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WO2013013361A1 - Wind turbine blade fully made of honeycomb board - Google Patents

Wind turbine blade fully made of honeycomb board Download PDF

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Publication number
WO2013013361A1
WO2013013361A1 PCT/CN2011/001904 CN2011001904W WO2013013361A1 WO 2013013361 A1 WO2013013361 A1 WO 2013013361A1 CN 2011001904 W CN2011001904 W CN 2011001904W WO 2013013361 A1 WO2013013361 A1 WO 2013013361A1
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WO
WIPO (PCT)
Prior art keywords
honeycomb
panel
honeycomb panel
wind turbine
profile
Prior art date
Application number
PCT/CN2011/001904
Other languages
French (fr)
Chinese (zh)
Inventor
周阳
Original Assignee
上海庆华蜂巢建材有限公司
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Application filed by 上海庆华蜂巢建材有限公司 filed Critical 上海庆华蜂巢建材有限公司
Publication of WO2013013361A1 publication Critical patent/WO2013013361A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • F03D1/065Rotors characterised by their construction elements
    • F03D1/0675Rotors characterised by their construction elements of the blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/20Geometry three-dimensional
    • F05B2250/28Geometry three-dimensional patterned
    • F05B2250/283Honeycomb
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

Definitions

  • the present invention relates to a wind turbine blade, and more particularly to a wind turbine blade made of a full honeycomb panel. Background technique
  • a full honeycomb panel wind turbine wind turbine blade comprising a casing and an inner support structure, the casing being mainly composed of an upper half shell and a lower half shell, wherein the inner support structure is placed in the shell and The support portions of the upper half shell and the lower half shell are respectively connected, wherein the upper half shell is formed by bending of a first honeycomb panel, and the lower half shell is formed by bending of a second honeycomb panel, the inner support structure a longitudinal support plate, the longitudinal support plate is formed by an upright honeycomb plate, the longitudinal support plate and the casing have the same longitudinal cross-sectional shape at the support portion, and the size is matched, the first honeycomb plate and the second honeycomb
  • the plate and the upright honeycomb panel include an upper panel, a lower panel, and a honeycomb core material, wherein the honeycomb core material is placed on the lower panel and closely adheres to the lower panel, and the upper panel covers the The honeycomb core material is closely adhered to the honeycomb core material.
  • the full honeycomb plate wind turbine blade wherein the casing has a water droplet shape, and the water droplet tail is a spoiler angle of the wind turbine blade, and the spoiler angle is mainly a honeycomb panel and a second honeycomb panel;
  • the first honeycomb panel includes a first slope, the first slope forming a first acute angle and a first blunt on a cross section thereof An angle, the first acute angle corresponding to the first oblique cross section forming the spoiler angle
  • the second honeycomb panel comprising a second inclined surface, the second inclined surface forming a second acute angle and a cross section thereof a second obtuse angle, a side of the second acute angle shared by the second obtuse angle and a side of the first obtuse angle not shared by the first acute angle, and a vertex of the second acute angle and the first
  • the apex of the obtuse angle is in contact.
  • a polygonal profile that is divided into a left half and a right half in a centerline, the left half and the right half being symmetric about a centerline of the polygonal profile, the left half cross-sectional shape Matching the cross-sectional shape of the first channel profile, the right half cross-sectional shape matching the second channel profile cross-sectional shape, the left half of the polygonal profile extending into the first channel shape
  • the profile is connected thereto and the right half of the polygonal profile projects into and is connected to the second channel profile.

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

A wind turbine blade fully made of honeycomb boards comprises a housing and an internal support structure. The housing is mainly formed of an upper half housing and a lower half housing. The internal support structure is arranged in the housing, and connected to support portions of the upper half housing and the lower half housing respectively. The upper half housing is formed by bending a first honeycomb board (1). The lower half housing is formed by bending a second honeycomb board (2). The internal support structure is a longitudinal support board (3). The longitudinal support board is formed of a vertical honeycomb board (30). The longitudinal sections of the longitudinal support board and the housing at the support portions have the same shape and match in size. The blade structure reduces the weight of the wind turbine blade, increases the wind-to-power conversion efficiency of the wind turbine, simplifies the process of using the honeycomb boards to manufacture the wind turbine blade, and reduces the manufacturing costs.

Description

全蜂巢板风力发电机风轮叶片  Full honeycomb panel wind turbine blade
技术领域 Technical field
本发明涉及一种风力发电机风轮叶片,尤其是一种全蜂巢板制成的风力发电机风轮叶 片。 背景技术  The present invention relates to a wind turbine blade, and more particularly to a wind turbine blade made of a full honeycomb panel. Background technique
公知的风力发电机风轮叶片一般由玻璃纤维与树脂混合制成,由于该种方式制成的风 轮叶片存在重量大、脆性大、生产时会释放有害气体等问题, 所以发展比重轻且具有良好 疲劳强度和机械性能的风轮叶片成为风力发电机革新的重要问题, 蜂巢板由于其比重轻, 强度重量比大, 受力平均, 耐压力强, 抗震性好及不变形等特点是制造风力发电力风轮叶 片的优良材料, 但是由于蜂巢板的结构特点, 导致其加工、组合成风轮风叶的形状存在相 当难度, 使得以蜂巢板制造风力发电机风轮叶片无法推广。 发明内容  The known wind turbine blade is generally made of glass fiber and resin. Because the wind turbine blade made by this method has the problems of large weight, large brittleness, and release of harmful gas during production, the development is light and has a light weight. Wind turbine blades with good fatigue strength and mechanical properties have become an important issue in the innovation of wind turbines. Due to their light weight, high strength-to-weight ratio, average force, high pressure resistance, good shock resistance and no deformation, honeycomb panels are used to manufacture wind power. The excellent material of the electric wind turbine blades, but due to the structural characteristics of the honeycomb panels, the shape of the wind turbine blades processed and combined into the wind turbine is quite difficult, so that the wind turbine blades manufactured by the honeycomb panels cannot be promoted. Summary of the invention
针对现有风力发电机风轮叶片存在的上述问题,本发明提供一种全蜂巢板制成的风力 发电机风轮叶片。  In view of the above problems with existing wind turbine blades, the present invention provides a wind turbine blade made of a full honeycomb panel.
本发明解决技术问题所采用的技术方案为:  The technical solution adopted by the present invention to solve the technical problem is:
一种全蜂巢板风力发电机风轮叶片,包括壳体和内部支撑结构,所述壳体主要由上半 壳与下半壳组合而成,所述内部支撑结构置于所述壳体内并与所述上半壳及所述下半壳的 支撑部位分别连接, 其中, 所述上半壳由第一蜂巢板弯曲形成, 所述下半壳由第二蜂巢板 弯曲形成, 所述内部支撑结构为纵向支撑板, 所述纵向支撑板由直立蜂巢板形成, 所述纵 向支撑板与所述壳体于所述支撑部位的纵向截面形状相同且大小匹配, 所述第一蜂巢板、 第二蜂巢板及所述直立蜂巢板包括上面板、下面板、蜂巢状芯材, 所述蜂巢状芯材置于所 述下面板上并与所述下面板紧密贴合,所述上面板覆于所述蜂巢状芯材上,并与所述蜂巢 状芯材紧密贴合。  A full honeycomb panel wind turbine wind turbine blade comprising a casing and an inner support structure, the casing being mainly composed of an upper half shell and a lower half shell, wherein the inner support structure is placed in the shell and The support portions of the upper half shell and the lower half shell are respectively connected, wherein the upper half shell is formed by bending of a first honeycomb panel, and the lower half shell is formed by bending of a second honeycomb panel, the inner support structure a longitudinal support plate, the longitudinal support plate is formed by an upright honeycomb plate, the longitudinal support plate and the casing have the same longitudinal cross-sectional shape at the support portion, and the size is matched, the first honeycomb plate and the second honeycomb The plate and the upright honeycomb panel include an upper panel, a lower panel, and a honeycomb core material, wherein the honeycomb core material is placed on the lower panel and closely adheres to the lower panel, and the upper panel covers the The honeycomb core material is closely adhered to the honeycomb core material.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述壳体横截面为水滴形, 所述水滴形尾 部为所述风力发电机风轮叶片的扰流角,所述扰流角主要由第一蜂巢板和第二蜂巢板组合 而成;所述第一蜂巢板包括第一斜面,所述第一斜面于其横截面上形成第一锐角和第一钝 角,所述第一斜面横截面对应的所述第一锐角形成所述扰流角,所述第二蜂巢板包括第二 斜面,所述第二斜面于其横截面上形成第二锐角和第二钝角,所述第二锐角与所述第二钝 角共用的一边与所述第一钝角不与所述第一锐角共用的一边贴合并连接,且所述第二锐角 的顶点与所述第一钝角的顶点接触。 The full honeycomb plate wind turbine blade, wherein the casing has a water droplet shape, and the water droplet tail is a spoiler angle of the wind turbine blade, and the spoiler angle is mainly a honeycomb panel and a second honeycomb panel; the first honeycomb panel includes a first slope, the first slope forming a first acute angle and a first blunt on a cross section thereof An angle, the first acute angle corresponding to the first oblique cross section forming the spoiler angle, the second honeycomb panel comprising a second inclined surface, the second inclined surface forming a second acute angle and a cross section thereof a second obtuse angle, a side of the second acute angle shared by the second obtuse angle and a side of the first obtuse angle not shared by the first acute angle, and a vertex of the second acute angle and the first The apex of the obtuse angle is in contact.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述壳体横截面为水滴形, 所述水滴形头 部为所述风力发电机风轮叶片的迎风端,所述迎风端包括第一蜂巢板和第二蜂巢板,所述 第一蜂巢板与所述第二蜂巢板厚度相同,所述第一蜂巢板与所述第二蜂巢板连接,其连接 部位形成所述迎风端,所述第一蜂巢板和第二蜂巢板之间有第一连接部件,所述第一连接 部件包括:  The above-mentioned full honeycomb panel wind turbine blade, wherein the casing has a teardrop shape in cross section, the teardrop head is a windward end of the wind turbine blade, and the windward end includes a first honeycomb a plate and a second honeycomb plate, wherein the first honeycomb plate has the same thickness as the second honeycomb plate, the first honeycomb plate is connected to the second honeycomb plate, and the connecting portion forms the windward end, the first A first connecting component is disposed between a honeycomb panel and the second honeycomb panel, and the first connecting component comprises:
第一槽形型材和第二槽形型材, 所述第一槽形型材和所述第二槽形型材形状相同; 所述第一槽形型材包括槽口和槽底,所述第一槽形型材槽口宽度小于所述第一蜂巢板 的厚度,所述第一槽形型材槽口向外与所述第一蜂巢板连接,且使所述第一槽形型材槽底 嵌入所述第一蜂巢板的上下面板之间并使所述第一槽形型材的槽口与所述第一蜂巢板板 边齐平;  a first channel profile and a second channel profile, the first channel profile and the second channel profile being identical in shape; the first channel profile comprising a slot and a slot bottom, the first slot shape The profile slot width is smaller than the thickness of the first honeycomb panel, the first slot profile slot is outwardly connected to the first honeycomb panel, and the first slot profile slot bottom is embedded in the first Between the upper and lower panels of the honeycomb panel and making the notch of the first channel profile flush with the edge of the first honeycomb panel;
所述第二槽形型材包括槽口和槽底,所述第二槽形型材槽口宽度小于所述第二蜂巢板 的厚度,所述第二槽形型材槽口向外与所述第二蜂巢板连接,且使所述第二槽形型材槽底 嵌入所述第二蜂巢板的上下面板之间并使所述第二槽形型材的槽口与所述第二蜂巢板板 边齐平;  The second channel profile includes a notch and a groove bottom, the second channel profile slot width is smaller than the thickness of the second honeycomb panel, and the second channel profile slot is outward and the second The honeycomb panels are connected, and the bottom of the second channel profile is embedded between the upper and lower panels of the second honeycomb panel and the notches of the second channel profile are flush with the edge of the second honeycomb panel ;
还包括多边形型材,所述多边形型材以其中线划分成左半部和右半部,所述左半部与 所述右半部关于所述多边形型材的中线对称,所述左半部横截面形状与所述第一槽形型材 横截面形状匹配,所述右半部横截面形状与所述第二槽形型材横截面形状匹配,所述多边 形型材的左半部伸入所述第一槽形型材并与其连接,所述多边形型材的右半部伸入所述第 二槽形型材并与其连接。  Also included is a polygonal profile that is divided into a left half and a right half in a centerline, the left half and the right half being symmetric about a centerline of the polygonal profile, the left half cross-sectional shape Matching the cross-sectional shape of the first channel profile, the right half cross-sectional shape matching the second channel profile cross-sectional shape, the left half of the polygonal profile extending into the first channel shape The profile is connected thereto and the right half of the polygonal profile projects into and is connected to the second channel profile.
上述全蜂巢板风力发电机风轮叶片,其中,形成所述纵向支撑板的直立蜂巢板与所述 第一蜂巢板和所述第二蜂巢板分别连接,所述直立蜂巢板与所述第一蜂巢板和所述第二蜂 巢板之间有一对第二连接部件, 所述一对第二连接部件为 u形型材, 所述 U形型材包括 凹槽、 两侧槽壁和槽底, 所述 u形型材的凹槽开口宽度大于所述直立蜂巢板的厚度, 所 述一对 U形型材其中之一的槽底与所述第一蜂巢板连接, 其中另一的槽底与所述第二蜂 巢板连接, 所述直立蜂巢板两端没有封边, 且分别插入所述一对 u形型材的凹槽中, 并 与所述 u形型材的两侧槽壁内侧及槽底保持一定距离以形成填充间隙, 所述填充间隙内 设有填充材料层, 所述填充材料层充满所述填充间隙及所述直立蜂巢板插入所述一对 u 形型材部分的蜂巢状芯材内部。 The above-mentioned full honeycomb panel wind turbine blade, wherein an upright honeycomb panel forming the longitudinal support plate is respectively connected to the first honeycomb panel and the second honeycomb panel, the upright honeycomb panel and the first a pair of second connecting members are disposed between the honeycomb panel and the second honeycomb panel, the pair of second connecting members are u-shaped profiles, and the U-shaped profiles include grooves, groove walls on both sides, and groove bottoms, The groove opening width of the u-shaped profile is greater than the thickness of the upright honeycomb panel, and the groove bottom of one of the pair of U-shaped profiles is connected to the first honeycomb panel, wherein the other groove bottom and the second groove The honeycomb panels are connected, and the two ends of the upright honeycomb panel are not edge-sealed, and are respectively inserted into the grooves of the pair of u-shaped profiles, and are kept at a distance from the inner side of the groove walls of the two sides of the u-shaped profile and the bottom of the groove. Forming a filling gap, the filling gap A layer of filler material is provided, the layer of filler material filling the fill gap and the interior of the honeycomb core of the pair of u-shaped profile portions inserted into the pair of u-shaped profiles.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述壳体由多段拼接组成, 以前段壳体的 所述第一蜂巢板为前段蜂巢板, 以后段壳体的所述第一蜂巢板为后蜂巢板,所述前蜂巢板 与所述后蜂巢板拼接,所述前蜂巢板的上面板与所述后蜂巢板的上面板拼合,所述前蜂巢 板的下面板与所述后蜂巢板的下面板拼合,所述前蜂巢板的蜂巢状芯材与所述后蜂巢板的 蜂巢状芯材于拼接部位贴合,所述前蜂巢板和所述后蜂巢板之间有第三连接部件,所述第 三连接部件为上部连接板和下部连接板,所述上部连接板覆盖所述前蜂巢板的上面板和所 述后蜂巢板的上面板的拼合接缝, 并与所述前蜂巢板上面板和所述后蜂巢板上面板连接, 所述下部连接板覆盖所述前蜂巢板的下面板和所述后蜂巢板的下面板的拼合接缝,并与所 述前蜂巢板下面板和所述后蜂巢板下面板连接,两段壳体的所述第二蜂巢板之间的连接方 式与两段壳体的所述第一蜂巢板的连接方式相同。  The above-mentioned full honeycomb panel wind turbine blade, wherein the casing is composed of a plurality of segments, the first honeycomb plate of the previous casing is a front honeycomb plate, and the first honeycomb plate of the subsequent casing is a rear honeycomb panel, the front honeycomb panel is spliced with the rear honeycomb panel, an upper panel of the front honeycomb panel is assembled with an upper panel of the rear honeycomb panel, and a lower panel of the front honeycomb panel and the rear honeycomb panel The bottom plate of the front honeycomb panel is joined to the honeycomb core material of the rear honeycomb panel at a splicing portion, and a third connecting member is disposed between the front honeycomb panel and the rear honeycomb panel The third connecting member is an upper connecting plate and a lower connecting plate, the upper connecting plate covering the split seam of the upper panel of the front honeycomb panel and the upper panel of the rear honeycomb panel, and the front honeycomb The upper panel is connected to the rear honeycomb panel, the lower connecting panel covers the split seam of the lower panel of the front honeycomb panel and the lower panel of the rear honeycomb panel, and the front panel of the honeycomb panel Connected to the lower panel of the honeycomb panel The connection between the second honeycomb panels of the two-stage housing is the same as the connection of the first honeycomb panels of the two-segment housing.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一锐角和所述第二锐角共同形成所 述扰流角,所述第二锐角与所述第二钝角共用的边与所述第一锐角与所述第一钝角共用的 边贴合并连接,且第二锐角的顶点与所述第一锐角的顶点接触,所述第二钝角的顶点与所 述第一钝角的顶点接触。  The full honeycomb panel wind turbine blade, wherein the first acute angle and the second acute angle together form the spoiler angle, and the second acute angle and the second obtuse angle share an edge An edge of the acute angle that is common to the first obtuse angle is joined, and a vertex of the second acute angle is in contact with an apex of the first acute angle, and a vertex of the second obtuse angle is in contact with an apex of the first obtuse angle.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一蜂巢板和所述第二蜂巢板的连接 方式为紧固件连接。  The above-mentioned full honeycomb panel wind turbine blade, wherein the first honeycomb panel and the second honeycomb panel are connected by a fastener.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一槽形型材与所述第一蜂巢板之间 有填充材料层, 所述第二槽形型材与所述第二蜂巢板之间有填充材料层。  The full honeycomb panel wind turbine blade, wherein a filler material layer is disposed between the first channel profile and the first honeycomb panel, and the second channel profile and the second honeycomb panel are There is a layer of filler material.
上述全蜂巢板风力发电机风轮叶片,其中,所述多边形型材与所述第一槽形型材及所 述第二槽形型材之间有填充材料层。  The full honeycomb panel wind turbine blade, wherein the polygonal profile and the first channel profile and the second channel profile have a layer of filler material.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述第一槽形型材包括两侧槽壁, 一对沉 孔分别穿透所述第一蜂巢板的上下面板及所述第一槽形型材的两侧槽壁,并通过一对穿过 该对沉孔的紧固件将所述第一蜂巢板、所述第一槽形型材和所述多边形型材的左半部连接 在一起。  The full honeycomb panel wind turbine blade, wherein the first channel profile comprises two side groove walls, and the pair of counter holes penetrate the upper and lower panels of the first honeycomb panel and the first channel profile The groove walls on both sides and the first honeycomb panel, the first channel profile and the left half of the polygonal profile are joined together by a pair of fasteners passing through the pair of counterbore.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述第二槽形型材包括两侧槽壁, 一对沉 孔分别穿透所述第二蜂巢板的上下面板及所述第二槽形型材的两侧槽壁,并通过一对穿过 该对沉孔的紧固件将所述第二蜂巢板、所述第二槽形型材和所述多边形型材的右半部连接 在一起。 上述全蜂巢板风力发电机风轮叶片, 其中, 所述直立蜂巢板由多段连接而成, 以前段 的所述直立蜂巢板为前直立蜂巢板, 以后段的所述直立蜂巢板为后直立蜂巢板,所述前直 立蜂巢板边缘与所述后直立蜂巢板边缘连接,且所述前直立蜂巢板与所述后直立蜂巢板在 同一平面内,所述前直立蜂巢板和所述后直立蜂巢板相互连接的一侧没有封边,所述前直 立蜂巢板与所述后直立蜂巢板之间有第四连接部件, 所述第四连接部件为 H形型材, 所 述 H形型材包括第一槽口和第二槽口, 所述第一槽口和第二槽口分别包括两侧槽壁和槽 底, 所述前直立蜂巢板插入所述第一槽口且与所述 H形型材连接, 所述后直立蜂巢板插 入所述第二槽口且与所述 H形型材连接, 所述前直立蜂巢板与所述第一槽口的两侧槽壁 内侧及槽底保持一定距离,形成第一填充间隙,所述后直立蜂巢板与所述第二槽口的两侧 槽壁内侧及槽底保持一定距离,形成第二填充空间,所述第一填充空间及所述第二填充空 间内设有填充材料层。 The full honeycomb panel wind turbine blade, wherein the second channel profile comprises two side groove walls, and the pair of counter holes penetrate the upper and lower panels of the second honeycomb panel and the second channel profile respectively The groove walls on both sides and the second honeycomb panel, the second channel profile and the right half of the polygonal profile are joined together by a pair of fasteners passing through the pair of counterbore. The above-mentioned full honeycomb plate wind turbine blade, wherein the upright honeycomb plate is connected by a plurality of segments, the upright honeycomb plate of the previous segment is a front upright honeycomb plate, and the upright honeycomb plate of the later segment is a rear upright honeycomb a plate, the edge of the front upright honeycomb panel is joined to the edge of the rear upright honeycomb panel, and the front upright honeycomb panel is in the same plane as the rear upright honeycomb panel, the front upright honeycomb panel and the rear upright honeycomb The side of the board that is connected to each other has no edge sealing, and there is a fourth connecting part between the front upright honeycomb board and the rear upright honeycomb board, the fourth connecting part is an H-shaped profile, and the H-shaped profile includes the first a notch and a second notch, the first notch and the second notch respectively comprise two side groove walls and a groove bottom, and the front upright honeycomb plate is inserted into the first notch and connected to the H-shaped profile The rear upright honeycomb panel is inserted into the second slot and connected to the H-shaped profile, and the front upright honeycomb panel is kept at a certain distance from the inner side of the groove wall and the groove bottom of the first slot. First filling gap, the rear erect Nest plate and holding the second slot on both sides of the inner groove wall and the groove bottom at a distance, forming a second space filling, filling the first space and the second space is filled with a filling material layer features.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述一对 U形型材分别与所述第一蜂巢 板和第二蜂巢板之间有填充材料层。  The above-mentioned full honeycomb panel wind turbine blade, wherein the pair of U-shaped profiles respectively have a filling material layer between the first honeycomb panel and the second honeycomb panel.
上述全蜂巢板风力发电机风轮叶片,其中,所述上部连接板覆盖所述前蜂巢板的上面 板和所述后蜂巢板的上面板的拼合接缝朝向所述蜂巢状芯材的一面,所述下部连接板覆盖 所述前蜂巢板的下面板和所述后蜂巢板的下面板的拼合接缝朝向所述蜂巢状芯材的一面。  The above-mentioned full honeycomb panel wind turbine blade, wherein the upper connecting plate covers the joint seam of the upper panel of the front honeycomb panel and the upper panel of the rear honeycomb panel toward one side of the honeycomb core material, The lower connecting plate covers a split seam of the lower panel of the front honeycomb panel and the lower panel of the rear honeycomb panel toward one side of the honeycomb core.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述上部连接板有多块, 所述多块上部连 接板为长条形并相互以一定间隔连接所述前蜂巢板上面板和所述后蜂巢板上面板,所述下 部连接板有多块,所述多块下部连接板为长条形并相互以一定间隔连接所述前蜂巢板下面 板和所述后蜂巢板下面板。  The above-mentioned full honeycomb panel wind turbine blade, wherein the upper connecting plate has a plurality of pieces, and the plurality of upper connecting plates are elongated and connected to the front honeycomb panel and the rear portion at intervals The honeycomb panel has a plurality of lower connecting plates, and the plurality of lower connecting plates are elongated and connected to the front honeycomb panel lower panel and the rear honeycomb panel lower panel at a certain interval.
上述全蜂巢板风力发电机风轮叶片,其中,所述上部连接板与所述前蜂巢板的上面板 和所述后蜂巢板的上面板的连接方式为粘接,所述下部连接板与所述前蜂巢板的下面板和 所述后蜂巢板的下面板的连接方式为粘接。  The full honeycomb panel wind turbine blade, wherein the upper connecting plate is bonded to the upper panel of the front honeycomb panel and the upper panel of the rear honeycomb panel, and the lower connecting panel is The connection between the lower panel of the front honeycomb panel and the lower panel of the rear honeycomb panel is bonding.
上述全蜂巢板风力发电机风轮叶片, 其中, 还包括 V形连接部件, 所述 V形连接部 件包括第一平面、第二平面和顶角, 所述顶角顶住所述扰流角内侧, 所述第一平面与所述 第一蜂巢板贴合并连接, 所述第二平面与所述第二蜂巢板贴合并连接。  The full honeycomb panel wind turbine blade, further comprising a V-shaped connecting member, the V-shaped connecting member comprising a first plane, a second plane and a vertex, the vertex supporting the inside of the spoiler The first plane is attached to the first honeycomb panel, and the second plane is connected to the second honeycomb panel.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一槽形型材和所述第二槽形型材为 C形型材, 所述多边形型材为矩形型材。  The full honeycomb panel wind turbine blade, wherein the first channel profile and the second channel profile are C-shaped profiles, and the polygonal profile is a rectangular profile.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一槽形型材和所述第二槽形型材为 V形型材, 所述多边形型材为菱形型材。 上述全蜂巢板风力发电机风轮叶片, 其中, 所述前直立蜂巢板与所述 H形型材的连 接方式为所述前直立蜂巢板的上下面板与所述 H形型材的第一槽口的两侧槽壁通过紧固 件连接, 所述后直立蜂巢板与所述 H形型材的连接方式为所述后直立蜂巢板的上下面板 与所述 H形型材的第二槽口的两侧槽壁通过紧固件连接。 The full honeycomb panel wind turbine blade, wherein the first channel profile and the second channel profile are V-shaped profiles, and the polygonal profile is a diamond profile. The full honeycomb panel wind turbine blade, wherein the front vertical honeycomb panel and the H-shaped profile are connected by the upper and lower panels of the front upright honeycomb panel and the first slot of the H-shaped profile The groove walls of the two sides are connected by fasteners, and the connection manner of the rear upright honeycomb panel and the H-shaped profile is the upper and lower panels of the rear upright honeycomb panel and the slots on the two sides of the second slot of the H-shaped profile The walls are connected by fasteners.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述一对 U形型材的槽底分别与所述第 一蜂巢板和所述第二蜂巢板粘接。  The above-mentioned full honeycomb panel wind turbine blade, wherein the groove bottoms of the pair of U-shaped profiles are respectively bonded to the first honeycomb panel and the second honeycomb panel.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述一对 U形型材的槽底与所述第一蜂 巢板和所述第二蜂巢板之间分别设有沉孔且有紧固件通过该沉孔分别将所述第一蜂巢板 和所述一对 U形型材其中之一以及第二蜂巢板和所述一对 U形型材其中另一连接在一起。  The full honeycomb panel wind turbine blade, wherein the groove bottom of the pair of U-shaped profiles and the first honeycomb panel and the second honeycomb panel are respectively provided with countersunk holes and fasteners are passed through The counterbore connects the first honeycomb panel and one of the pair of U-shaped profiles and the second honeycomb panel and the other of the pair of U-shaped profiles, respectively.
上述全蜂巢板风力发电机风轮叶片,其中,所述上部连接板伸入所述前蜂巢板上面板 和所述蜂巢状芯材之间的长度与其伸入所述后蜂巢板上面板和所述蜂巢状芯材之间的长 度相等,所述下部连接板伸入所述前蜂巢板下面板和所述蜂巢状芯材之间的长度与其伸入 所述后蜂巢板下面板和所述蜂巢状芯材之间的长度相等。  The above-mentioned full honeycomb panel wind turbine blade, wherein the upper connecting plate extends into a length between the front honeycomb panel and the honeycomb core and extends into the rear honeycomb panel and the The length between the honeycomb core materials is equal, the lower connecting plate extends into the length between the lower panel of the front honeycomb panel and the honeycomb core material and extends into the lower panel of the honeycomb panel and the honeycomb The length between the core materials is equal.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一蜂巢板和所述第二蜂巢板与所述 V形连接部件连接处有沉孔, 有紧固件通过所述第一蜂巢板上的沉孔与所述 V形连接部 件的第一平面连接, 有紧固件通过所述第二蜂巢板上的沉孔与所述 V形连接部件的第二 平面连接。  The full honeycomb panel wind turbine blade, wherein the first honeycomb panel and the second honeycomb panel have a counterbore at the junction with the V-shaped connecting member, and the fastener passes through the first honeycomb panel The upper counterbore is coupled to the first plane of the V-shaped connecting member, and the fastener is coupled to the second plane of the V-shaped connecting member through a counterbore on the second honeycomb panel.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一斜面处的所述蜂巢状芯材高度随 斜面均匀变化, 所述第二斜面处蜂巢状芯材高度随斜面均匀变化。  In the above-mentioned full honeycomb panel wind turbine blade, the height of the honeycomb core at the first slope is uniformly changed with the slope, and the height of the honeycomb core at the second slope is uniformly changed with the slope.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述蜂巢状新材包括多个六角形腔体, 所 述第一斜面处蜂巢状芯材的六角形腔体内和所述第二斜面处蜂巢状芯材的六角形腔体内 有硬质弹性填充材料。  The above-mentioned full honeycomb panel wind turbine blade, wherein the honeycomb-shaped new material comprises a plurality of hexagonal cavities, a hexagonal cavity of the honeycomb core at the first bevel and a honeycomb at the second bevel The hexagonal cavity of the core material has a hard elastic filling material.
上述全蜂巢板风力发电机风轮叶片,其中,将开设所述沉孔的蜂巢板称为待连接蜂巢 板,将需与所述待连接蜂巢板连接的型材称为连接件,所述带连接蜂巢板包括待连接上面 板、待连接下面板和待连接蜂巢状芯材, 所述待连接蜂巢状芯材包括多个六角形腔室, 所 述沉孔包括连接结构,所述连接结构包括加固层和通孔,所述加固层主要由所述待连接蜂 巢状芯材和所述六角形腔室内的加固填充材料层组成,所述加固填充材料层充满所述六角 形腔室,所述加固填充材料层为硬质弹性填充材料层,所述加固层面积小于所述待连接蜂 巢板的面积, 所述加固层面积大于所述连接件与所述待连接蜂巢板连接部位的接触面积, 所述通孔穿透所述待连接上面板、待连接下面板及所述加固层, 所述通孔包括台阶, 所述 台阶位于所述待连接蜂巢板不与所述连接件连接的一侧。 The above-mentioned full honeycomb panel wind turbine blade, wherein the honeycomb panel in which the counterbore is opened is referred to as a honeycomb panel to be connected, and the profile to be connected to the honeycomb panel to be connected is referred to as a connector, and the strap is connected. The honeycomb panel includes an upper panel to be connected, a lower panel to be connected, and a honeycomb core to be connected, the honeycomb core to be connected includes a plurality of hexagonal chambers, the counterbore includes a connection structure, and the connection structure includes reinforcement a layer and a through hole, the reinforcing layer mainly consisting of the honeycomb core material to be connected and a layer of reinforcing filler material in the hexagonal cavity, the layer of reinforcing filler material filling the hexagonal cavity, the reinforcement The filler material layer is a hard elastic filler material layer, the reinforcement layer area is smaller than the area of the honeycomb panel to be connected, and the reinforcement layer area is larger than the contact area of the connecting member and the connection portion of the honeycomb panel to be connected. The through hole penetrates the upper panel to be connected, the lower panel to be connected, and the reinforcement layer, and the through hole includes a step, The step is located on a side where the honeycomb panel to be connected is not connected to the connecting member.
上述全蜂巢板风力发电机风轮叶片,其中,所述第一蜂巢板和所述第二蜂巢板为铝蜂 巢板。  The above-described full honeycomb panel wind turbine blade, wherein the first honeycomb plate and the second honeycomb plate are aluminum honeycomb plates.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述壳体外侧包覆保护涂层。  The above-mentioned full honeycomb panel wind turbine blade, wherein the outer side of the casing is covered with a protective coating.
上述全蜂巢板风力发电机风轮叶片, 其中, 所述保护涂层为环氧树脂涂层。  The above-mentioned full honeycomb panel wind turbine blade, wherein the protective coating is an epoxy resin coating.
本发明的有益效果是:  The beneficial effects of the invention are:
有效减轻了风力发电机风轮叶片的重量,提高了风力发电机的风电转换效率, 同时简 化了蜂巢板制造风力发电机风轮叶片的工艺, 降低了制造成本。 附图说明  The weight of the wind turbine blade is effectively reduced, the wind power conversion efficiency of the wind power generator is improved, and the process of manufacturing the wind turbine blade of the wind turbine by the honeycomb plate is simplified, and the manufacturing cost is reduced. DRAWINGS
图 1是本发明全蜂巢板风力发电机风轮叶片的正视图;  Figure 1 is a front elevational view of a full honeycomb panel wind turbine blade of the present invention;
图 2是本发明全蜂巢板风力发电机风轮叶片的侧视图;  Figure 2 is a side view of the full honeycomb panel wind turbine blade of the present invention;
图 3是本发明全蜂巢板风力发电机风轮叶片的纵向支撑板的正视图;  Figure 3 is a front elevational view of the longitudinal support plate of the full honeycomb panel wind turbine blade of the present invention;
图 4是本发明全蜂巢板风力发电机风轮叶片的剖面图;  Figure 4 is a cross-sectional view of a full honeycomb panel wind turbine blade of the present invention;
图 5是本发明全蜂巢板风力发电机风轮叶片的扰流角结构示意图;  Figure 5 is a schematic view showing the structure of the spoiler angle of the wind turbine blade of the full honeycomb panel of the present invention;
图 6是本发明全蜂巢板风力发电机风轮叶片的扰流角另一种实施方式的结构示意图; 图 7是本发明全蜂巢板风力发电机风轮叶片的扰流角的 V型连接部件的结构示意图; 图 8是本发明全蜂巢板风力发电机风轮叶片的迎风端的结构示意图;  6 is a schematic structural view showing another embodiment of the spoiler angle of the full honeycomb panel wind turbine blade of the present invention; FIG. 7 is a V-shaped connecting member of the spoiler angle of the full honeycomb panel wind turbine blade of the present invention; Figure 8 is a schematic view showing the structure of the windward end of the wind turbine blade of the full honeycomb panel of the present invention;
图 9是本发明全蜂巢板风力发电机风轮叶片的迎风端的 C形型材的结构示意图; 图 10是本发明全蜂巢板风力发电机风轮叶片的迎风端的矩形型材的结构示意图; 图 11是本发明全蜂巢板风力发电机风轮叶片的纵向支撑板与上下半壳连接处的结构 示意图;  9 is a schematic structural view of a C-shaped profile of the windward end of the full honeycomb panel wind turbine blade of the present invention; FIG. 10 is a schematic structural view of a rectangular profile of the windward end of the full honeycomb panel wind turbine blade of the present invention; The structural schematic diagram of the joint between the longitudinal support plate and the upper and lower half shells of the full honeycomb panel wind turbine blade of the present invention;
图 12是本发明全蜂巢板风力发电机风轮叶片分段安装时外壳拼接处的结构示意图; 图 13是本发明全蜂巢板风力发电机风轮叶片分段安装时外壳拼接处另一种实施方式 的结构示意图;  12 is a schematic structural view of a splicing portion of a casing of a full honeycomb panel wind turbine generator according to the present invention; FIG. 13 is another embodiment of a splicing portion of a casing of a full honeycomb panel wind turbine generator according to the present invention. Schematic diagram of the mode;
图 14是本发明全蜂巢板风力发电机风轮叶片分段安装时纵向支撑板的拼接结构示意 图;  Figure 14 is a schematic view showing the splicing structure of the longitudinal support plate when the wind turbine blades of the whole honeycomb panel of the present invention are installed in sections;
图 15是本发明全蜂巢板风力发电机风轮叶片的沉孔的结构示意图。 具体实施方式 下面结合附图和具体实施例对本发明作进一步说明, 但不作为本发明的限定。 Fig. 15 is a structural schematic view showing the counterbore of the wind turbine blade of the full honeycomb panel wind turbine of the present invention. detailed description The invention is further described below in conjunction with the drawings and specific embodiments, but is not to be construed as limiting.
如图 1、 图 2、 图 3和图 4所示, 本发明全蜂巢板风轮叶片包括壳体和内部支撑结构, 壳体主要由上半壳与下半壳组合而成,内部支撑结构置于壳体内并与上半壳及所述下半壳 的支撑部位分别连接, 其中, 上半壳由第一蜂巢板 1 弯曲形成, 下半壳由第二蜂巢板 2 弯曲形成, 内部支撑结构为纵向支撑板 3, 纵向支撑板由直立蜂巢板形成, 纵向支撑板 3 与壳体于支撑部位的纵向截面形状相同且大小匹配, 第一蜂巢板 1、第二蜂巢板 2及直立 蜂巢板包括上面板、下面板、蜂巢状芯材,蜂巢状芯材置于下面板上并与下面板紧密贴合, 上面板覆于蜂巢状芯材上,并与蜂巢状芯材紧密贴合。以纵向支撑板 3代替传统的肋骨桁 架结构可以降低内部支撑结构的重量,且由于蜂巢板本身的结构特点, 以其制成纵向支撑 板可以很好的代替传统的肋骨桁架结构。纵向支撑板 3可以根据风轮叶片的宽度选择设置 一块或多块,如设置多块纵向支撑板只需使各纵向支撑板之间保持平行即可,设置多块纵 向支撑板可以适应更大尺寸的风轮叶片。  As shown in FIG. 1, FIG. 2, FIG. 3 and FIG. 4, the full honeycomb panel wind turbine blade of the present invention comprises a casing and an internal support structure, and the casing is mainly composed of an upper half shell and a lower half shell, and the inner support structure is arranged. And being connected to the support portions of the upper half shell and the lower half shell respectively, wherein the upper half shell is formed by bending of the first honeycomb panel 1 and the lower half shell is formed by bending of the second honeycomb panel 2, and the inner support structure is The longitudinal support plate 3, the longitudinal support plate is formed by an upright honeycomb plate, the longitudinal support plate 3 and the casing have the same longitudinal cross-sectional shape at the support portion, and the first honeycomb plate 1, the second honeycomb plate 2 and the upright honeycomb plate are included The panel, the lower panel, the honeycomb core material, the honeycomb core material are placed on the lower panel and closely adhered to the lower panel, and the upper panel is covered on the honeycomb core material and closely adheres to the honeycomb core material. Replacing the conventional rib cage structure with the longitudinal support plate 3 can reduce the weight of the internal support structure, and due to the structural characteristics of the honeycomb panel itself, the longitudinal support plate can be used to replace the conventional rib truss structure. The longitudinal support plate 3 can be selected according to the width of the wind turbine blade. One or more blocks can be selected according to the width of the wind turbine blade. For example, if a plurality of longitudinal support plates are arranged, only the longitudinal support plates should be kept parallel, and a plurality of longitudinal support plates can be arranged to accommodate larger sizes. Wind turbine blades.
进一步的, 壳体横截面为水滴形, 水滴形尾部为风力发电机风轮叶片的扰流角 4, 如 图 5所示,扰流角 4主要由第一蜂巢板 1和第二蜂巢板 2组合而成;第一蜂巢板 1包括第 一斜面 411,第一斜面 411于其横截面上形成第一锐角 412和第一钝角 413 ,第一斜面 411 横截面对应的第一锐角 412形成扰流角 4,第二蜂巢板 2包括第二斜面 421,第二斜面 421 于其横截面上形成第二锐角 422和第二钝角 423 ,第二锐角 422与第二钝角 423共用的一 边与第一钝角 413不与第一锐角 412共用的一边贴合并连接,且第二锐角 422的顶点与第 一钝角 413的顶点接触,第一蜂巢板 1和第二蜂巢板 2的连接方式为紧固件连接,如铆钉 铆接,铆钉可以选择铝制铆钉。以带斜面的蜂巢板的斜面形成风轮叶片的扰流角解决了蜂 巢板制成风力发电机风轮叶片时需使用额外的配件或者工艺形成扰流角缺点,既简化了蜂 巢板制成风轮叶片的工艺又降低了蜂巢板制成风轮叶片的成本。在此基础上扰流角还可以 以下形式实施:  Further, the cross section of the casing is a teardrop shape, and the drop shape tail is a spoiler angle 4 of the wind turbine blade. As shown in FIG. 5, the spoiler angle 4 is mainly composed of the first honeycomb plate 1 and the second honeycomb plate 2 The first honeycomb panel 1 includes a first inclined surface 411. The first inclined surface 411 forms a first acute angle 412 and a first obtuse angle 413 on a cross section thereof, and the first acute angle 412 corresponding to the cross section of the first inclined surface 411 forms a spoiler. The second honeycomb plate 2 includes a second inclined surface 421. The second inclined surface 421 forms a second acute angle 422 and a second obtuse angle 423 on the cross section thereof. The second acute angle 422 and the second obtuse angle 423 share a side and a first obtuse angle. 413 is not attached to the side shared by the first acute angle 412, and the apex of the second acute angle 422 is in contact with the apex of the first obtuse angle 413, and the connection manner of the first honeycomb panel 1 and the second honeycomb panel 2 is a fastener connection. If the rivet is riveted, the rivet can be made of aluminum rivets. The turbulent angle of the wind turbine blade formed by the inclined surface of the beveled bevel plate solves the disadvantage that the honeycomb plate is made into a wind turbine blade, which requires additional fittings or processes to form a spoiler angle, which simplifies the formation of the honeycomb plate. The process of the wheel blades in turn reduces the cost of the honeycomb blades to make the rotor blades. On this basis, the spoiler angle can also be implemented in the following form:
如图 6所示,第一锐角 412和第二锐角 422共同形成扰流角,第二锐角 422与第二钝 角 423共用的边与第一锐角 412与第一钝角 413共用的边贴合并连接, 且第二锐角 422 的顶点与第一锐角 412的顶点接触,第二钝角 423的顶点与第一钝角 413的顶点接触,第 一蜂巢板 1和第二蜂巢板 2的连接方式为紧固件连接,如铆钉铆接,铆钉可以选择铝制铆 钉。此实施方式是在前述实施方式基础上的改进。此实施方式的主要优点是可以增加扰流 角尖端的强度。  As shown in FIG. 6 , the first acute angle 412 and the second acute angle 422 together form a spoiler angle, and the edge shared by the second acute angle 422 and the second obtuse angle 423 and the edge of the first acute angle 412 and the first obtuse angle 413 are connected and connected. And the apex of the second acute angle 422 is in contact with the apex of the first acute angle 412, the apex of the second obtuse angle 423 is in contact with the apex of the first obtuse angle 413, and the connection manner of the first honeycomb panel 1 and the second honeycomb panel 2 is a fastener connection. For example, rivets are riveted, and rivets can be selected from aluminum rivets. This embodiment is an improvement based on the foregoing embodiment. The main advantage of this embodiment is that the strength of the spoiler tip can be increased.
进一步的如图 5、 图 6和图 7所示, 还包括 V形连接部件 43, V形连接部件 43包括 第一平面 431、 第二平面 432和顶角 433, 顶角 433顶住扰流角内侧, 第一平面 431与第 一蜂巢板 1贴合并连接, 第二平面 432与第二蜂巢板 2贴合并连接。 增加了 V形连接部 件可以是扰流角获得支撑, 增加了扰流角的强度, 同时可以防止扰流角变形。 V形连接部 件 43可以是 V形铝型材, 第一平面 431与第一蜂巢板 1的连接方式可以是铆钉铆接, 第 二平面 432与第二蜂巢板 2的连接方式可以是紧固件连接, 如铆钉铆接。在此基础上, 第 一蜂巢板 1和第二蜂巢板 2与 V形连接部件 43连接处有沉孔,有紧固件通过第一蜂巢板 上 1的沉孔与 V形连接部件 43的第一平面 431连接,有紧固件通过第二蜂巢板 2上的沉 孔与 V形连接部件 43的第二平面 432连接。 Further, as shown in FIG. 5, FIG. 6, and FIG. 7, a V-shaped connecting member 43 is further included, and the V-shaped connecting member 43 includes The first plane 431, the second plane 432 and the apex angle 433, the apex angle 433 is opposite to the inner side of the spoiler angle, the first plane 431 is attached to the first honeycomb panel 1 and the second plane 432 is pasted with the second honeycomb panel 2 connection. The addition of the V-shaped connecting member can be supported by the spoiler angle, which increases the intensity of the spoiler angle and prevents the spoiler angle from being deformed. The V-shaped connecting member 43 may be a V-shaped aluminum profile, and the first plane 431 may be connected to the first honeycomb panel 1 by rivet riveting, and the second plane 432 and the second honeycomb panel 2 may be connected by fasteners. Such as rivet riveting. On the basis of this, the first honeycomb plate 1 and the second honeycomb plate 2 are connected with the V-shaped connecting member 43 with a counterbore, and the fastener passes through the counterbore of the first honeycomb plate 1 and the V-shaped connecting member 43 A flat surface 431 is connected and a fastener is connected to the second flat surface 432 of the V-shaped connecting member 43 through a counterbore on the second honeycomb panel 2.
进一步的,第一斜面处 411的蜂巢状芯材高度随斜面均匀变化,第二斜面 412处蜂巢 状芯材高度随斜面均匀变化,蜂巢状新材包括多个六角形腔体,第一斜面 411处蜂巢状芯 材的六角形腔体内和第二斜面 412处蜂巢状芯材的六角形腔体内有硬质弹性填充材料。蜂 巢状芯材高度随斜面均匀变化使斜面处面板与芯材间无空隙,使蜂巢板于斜面处强度得以 维持,同时在蜂巢状芯材中灌注硬质弹性填充材料可提高蜂巢板与斜面处的强度及抗变形 能力, 进而提高风力发电机风轮叶片扰流角 4的强度及抗变形能力。  Further, the height of the honeycomb core material at the first inclined surface 411 is uniformly changed with the inclined surface, and the height of the honeycomb core material at the second inclined surface 412 is uniformly changed with the inclined surface, and the honeycomb-shaped new material includes a plurality of hexagonal cavities, and the first inclined surface 411 The hexagonal cavity of the honeycomb core at the honeycomb core and the hexagonal cavity of the honeycomb core at the second slope 412 have a hard elastic filling material. The height of the honeycomb core material changes uniformly with the inclined surface so that there is no gap between the panel and the core material at the inclined surface, so that the strength of the honeycomb panel at the inclined surface is maintained, and the hard elastic filling material is filled in the honeycomb core material to improve the honeycomb panel and the inclined surface. The strength and resistance to deformation, thereby improving the strength and resistance to deformation of the wind turbine blade spoiler angle 4.
进一步的, 如图 4和图 8所示, 壳体横截面为水滴形, 水滴形头部为风力发电机风轮 叶片的迎风端 5, 迎风端 5包括第一蜂巢板 1和第二蜂巢板 2, 第一蜂巢板 1与第二蜂巢 板 2厚度相同, 第一蜂巢板 1与第二蜂巢板 2连接, 其连接部位形成迎风端 5, 第一蜂巢 板 1和第二蜂巢板 2之间有第一连接部件, 第一连接部件包括:  Further, as shown in FIG. 4 and FIG. 8, the housing has a teardrop shape in cross section, the teardrop shaped head is the windward end 5 of the wind turbine blade, and the windward end 5 includes the first honeycomb panel 1 and the second honeycomb panel. 2, the first honeycomb panel 1 is the same thickness as the second honeycomb panel 2, the first honeycomb panel 1 is connected to the second honeycomb panel 2, and the connecting portion forms a windward end 5, between the first honeycomb panel 1 and the second honeycomb panel 2 There is a first connecting component, and the first connecting component comprises:
第一槽形型材 531和第二槽形型材 532,第一槽形型材 531和第二槽形型材 532形状 相同;  The first channel profile 531 and the second channel profile 532, the first channel profile 531 and the second profile profile 532 are identical in shape;
由于第一槽形型材 531与第一蜂巢板 1的连接方式同第二槽形型材 532与第二蜂巢板 1的连接方式完全相同, 故此处以第一槽形型材 531举例说明, 如图 8和图 9, 第一槽形 型材 531包括槽口 531 1和槽底 5312,第一槽形型材 531槽口 531 1宽度小于第一蜂巢板 1 的厚度, 第一槽形型材 531槽口 5311向外与第一蜂巢板 1连接, 且使第一槽形型材 531 槽底 5312嵌入第一蜂巢板 1的上面板 1 1和下面板 12之间并使第一槽形型材 531的槽口 5311与第一蜂巢板 1板边齐平;  Since the first slot profile 531 is connected to the first honeycomb panel 1 in the same manner as the second slot profile 532 and the second honeycomb panel 1, the first slot profile 531 is illustrated here, as shown in FIG. 8 and 9, the first channel profile 531 includes a notch 531 1 and a groove bottom 5312. The width of the first channel profile 531 notch 531 1 is smaller than the thickness of the first honeycomb panel 1 , and the first channel profile 531 slot 5311 is outward. Connected to the first honeycomb panel 1 and the first channel profile 531 groove bottom 5312 is embedded between the upper panel 1 1 and the lower panel 12 of the first honeycomb panel 1 and the notch 5311 of the first channel profile 531 is a honeycomb panel 1 is flush with the board edge;
如图 10所示, 还包括多边形型材 533, 多边形型材 533以其中线 5330划分成左半部 5331和右半部 5332, 左半部 5331与右半部 5332关于多边形型材 533的中线 5330对称, 左半部 5331横截面形状与第一槽形型材 531横截面形状匹配,右半部 5332横截面形状与 第二槽形型材 532横截面形状匹配,多边形型材 533的左半部 5331伸入第一槽形型材 531 并与其连接, 多边形型材 533的右半部 5332伸入第二槽形型材 532并与其连接; 该连接方式通过调整第一槽形型材 531和第二槽形型材 532嵌入第一蜂巢板 1和第二 蜂巢板 2的角度可以改变第一蜂巢板 1和第二蜂巢板 2连接处曲面的弧度,同时通过第一 槽形型材 531和第二槽形型材 532同多边形型材 533的连接可以使第一蜂巢板 1和第二蜂 巢板 2之间的连接得到加强。 As shown in FIG. 10, a polygonal profile 533 is further included. The polygonal profile 533 is divided into a left half 5331 and a right half 5332 by a center line 5330, and the left half 5331 and the right half 5332 are symmetric about a center line 5330 of the polygonal profile 533, left. The cross-sectional shape of the half portion 5331 matches the cross-sectional shape of the first channel-shaped profile 531, the cross-sectional shape of the right half portion 5332 matches the cross-sectional shape of the second channel-shaped profile 532, and the left half 5331 of the polygonal profile 533 extends into the first groove. Profile 531 And connected thereto, the right half 5332 of the polygonal profile 533 extends into and is connected to the second channel profile 532; the connection mode is embedded in the first honeycomb panel 1 by adjusting the first channel profile 531 and the second channel profile 532 The angle of the second honeycomb panel 2 can change the curvature of the curved surface of the joint between the first honeycomb panel 1 and the second honeycomb panel 2, and the first groove profile 531 and the second channel profile 532 can be connected to the polygonal profile 533 to make the first The connection between the honeycomb panel 1 and the second honeycomb panel 2 is reinforced.
进一步的, 第一槽形型材 531与第一蜂巢板 1之间有填充材料层 561, 第二槽形型材 532与第二蜂巢板 2之间有填充材料层 562。 填充材料层 561和 562起到填补第一槽形型 材 531和第二槽形型材 532与第一蜂巢板 1和第二蜂巢板 2之间缝隙的作用,尤其是在需 要通过调整第一槽形型材 531和第二槽形型材 532嵌入第一蜂巢板 1和第二蜂巢板 2的角 度以改变第一蜂巢板 1和第二蜂巢板 2连接处曲面的弧度时会在第一槽形型材 531和第一 蜂巢板 1之间或者第二槽形型材 532和第二蜂巢板 2之间产生较大的缝隙,此时即可通过 填充材料层 561和 562进行填补。  Further, a filler material layer 561 is disposed between the first channel profile 531 and the first honeycomb panel 1, and a filler material layer 562 is disposed between the second channel profile 532 and the second honeycomb panel 2. The filling material layers 561 and 562 serve to fill the gap between the first channel profile 531 and the second channel profile 532 and the first honeycomb panel 1 and the second honeycomb panel 2, in particular by adjusting the first slot shape The profile 531 and the second channel profile 532 are embedded in the angle of the first honeycomb panel 1 and the second honeycomb panel 2 to change the curvature of the curved surface of the junction of the first honeycomb panel 1 and the second honeycomb panel 2, which will be in the first channel profile 531. A large gap is created between the first honeycomb panel 1 and the second channel profile 532 and the second honeycomb panel 2, which can be filled by the filling material layers 561 and 562.
进一步的,多边形型材 533与第一槽形型材 531及第二槽形型材 532之间有填充材料 层 57。 填充材料层 57可以调节多边形型材 533与第一槽形型材 531及第二槽形型材 532 之间的缝隙,尤其是在需要通过调整第一槽形型材 531和第二槽形型材 532嵌入第一蜂巢 板 1和第二蜂巢板 2的角度以改变第一蜂巢板 1和第二蜂巢板 2连接处曲面的弧度时,第 一槽形型材 531及第二槽形型材 532与多边形型材 533之间可能产生较大的缝隙,此时即 可通过填充材料层 57进行填补  Further, a filler material layer 57 is interposed between the polygonal profile 533 and the first channel profile 531 and the second channel profile 532. The filling material layer 57 can adjust the gap between the polygonal profile 533 and the first channel profile 531 and the second channel profile 532, especially in the first step by adjusting the first channel profile 531 and the second channel profile 532. When the angles of the honeycomb panel 1 and the second honeycomb panel 2 are changed to change the curvature of the curved surface of the joint between the first honeycomb panel 1 and the second honeycomb panel 2, between the first channel profile 531 and the second groove profile 532 and the polygonal profile 533 A large gap may be generated, which can be filled by the filling material layer 57.
进一步的, 第一槽形型材 531包括两侧槽壁 5313和 5314, 一对沉孔 541分别穿透第 一蜂巢板 1的上面板 11、 下面板 12及第一槽形型材 531的两侧槽壁 5313和 5314, 并通 过一对穿过该对沉孔 541的紧固件 551将第一蜂巢板 1、第一槽形型材 531和多边形型材 533的左半部 5331连接在一起; 在此基础上, 第二槽形型材 532包括两侧槽壁, 一对沉 孔 542分别穿透第二蜂巢板 2的上面板 21、 下面板 22及第二槽形型材 532的两侧槽壁, 并通过一对穿过该对沉孔 542的紧固件 552将第二蜂巢板 2、第二槽形型材 532和多边形 型材 533的右半部 5332连接在一起。 通过沉孔 541和 542及紧固件 551及 552进行连接 可以使第一蜂巢板 1和第二蜂巢板 2的连接处表面平整,方便表面处理且不影响风轮叶片 迎风端的空气动力学性能。  Further, the first channel profile 531 includes two side groove walls 5313 and 5314, and the pair of counter holes 541 penetrate the upper panel 11, the lower plate 12 of the first honeycomb panel 1, and the groove on both sides of the first channel profile 531, respectively. Walls 5313 and 5314, and joining the first honeycomb panel 1, the first channel profile 531 and the left half 5331 of the polygonal profile 533 by a pair of fasteners 551 passing through the pair of counterbore 541; The second slotted profile 532 includes two side slot walls, and the pair of counterbore 542 respectively penetrates the slot walls of the upper panel 21, the lower panel 22 and the second slot profile 532 of the second honeycomb panel 2, and passes through A pair of fasteners 552 passing through the pair of counterbore 542 join the second honeycomb panel 2, the second channel profile 532, and the right half 5332 of the polygonal profile 533. The connection between the counterbore 541 and 542 and the fasteners 551 and 552 allows the surface of the joint between the first honeycomb panel 1 and the second honeycomb panel 2 to be flat, facilitating surface treatment without affecting the aerodynamic performance of the windward end of the rotor blade.
进一步的,第一槽形型材 531和第二槽形型材 532可以是 C形型材, 多边形型材 533 可以是矩形型材。 C形型材和矩形型材较易获得, 且 C形型材便于嵌入蜂巢板板边, 使 本发明加工难度降低。 作为改进的, 第一槽形型材 531和第二槽形型材 532可以是 V形型材, 多边形型材 533可以是菱形型材。 V形型材更便于调整嵌入蜂巢板的角度,可以实现多种弧度的曲面, V形型材嵌入蜂巢板板边时可将蜂巢板的蜂巢状芯材部分去处, 形成容纳 V形型材的沟 槽,在加工固定沉孔 541和 542时可在蜂巢状芯材的腔室内灌注填充材料以增加蜂巢状芯 材的强度。 Further, the first channel profile 531 and the second channel profile 532 may be C-shaped profiles, and the polygonal profile 533 may be a rectangular profile. C-shaped profiles and rectangular profiles are relatively easy to obtain, and the C-shaped profiles are easy to be embedded in the side of the honeycomb panel, which makes the processing of the invention less difficult. As an improvement, the first channel profile 531 and the second channel profile 532 may be V-shaped profiles and the polygonal profile 533 may be a diamond profile. The V-shaped profile is more convenient for adjusting the angle of the embedded honeycomb panel, and can realize a plurality of curved curved surfaces. When the V-shaped profile is embedded in the edge of the honeycomb panel, the honeycomb core portion of the honeycomb panel can be removed to form a groove for accommodating the V-shaped profile. Filler materials may be poured into the chamber of the honeycomb core to increase the strength of the honeycomb core when the fixed counterbore 541 and 542 are machined.
进一步的, 如图 4和图 1 1所示, 形成纵向支撑板 3的直立蜂巢板 30与第一蜂巢板 1 和所述第二蜂巢板 2分别连接, 直立蜂巢板 30与第一蜂巢板 1和第二蜂巢板 2之间有一 对第二连接部件, 一对第二连接部件为 U形型材 33, U形型材 33包括凹槽 331、 两侧槽 壁 332和槽底 333, U形型材 33的凹槽 331开口宽度大于直立蜂巢板 30的厚度, 一对 U 形型材 33其中之一的槽底 333与第一蜂巢板 1连接, 其中另一的槽底 333与第二蜂巢板 2连接, 其连接方式可以是利用粘合剂粘接, 直立蜂巢板 30两端没有封边, 且分别插入 一对 U形型材 33的凹槽 331中, 并与 U形型材 33的两侧槽壁 332内侧及槽底 333保持 一定距离以形成填充间隙, 填充间隙内设有填充材料层 34, 填充材料层 34充满填充间隙 及直立蜂巢板 30插入一对 U形型材 33部分的蜂巢状芯材内部。 以第一蜂巢板 1插入宽 度大于其厚度的 u形型材 333的凹槽 331中可以调第一整蜂巢板 1、第二蜂巢板 2与直立 蜂巢板 30之间的位置,使第一蜂巢板 1、第二蜂巢板 2与直立蜂巢板 30的连接配合更好, 填充材料层 34不仅起到加固直立蜂巢板 30与 U形型材 33连接的作用,且由于直立蜂巢 板 30插入一对 U形型材 33的两端没有封边,而且填充材料层 34同时充满了直立蜂巢板 30插入一对 U形型材 33部分的蜂巢状芯材内部, 使得直立蜂巢板 30插入一对 U形型材 33的部分也得到了加强。  Further, as shown in FIG. 4 and FIG. 11, the upright honeycomb panel 30 forming the longitudinal support plate 3 is connected to the first honeycomb panel 1 and the second honeycomb panel 2, respectively, and the vertical honeycomb panel 30 and the first honeycomb panel 1 are respectively There is a pair of second connecting members between the second honeycomb panel 2 and a pair of second connecting members. The U-shaped profile 33 includes a groove 331, a groove wall 332 on both sides and a groove bottom 333. The U-shaped profile 33 The groove 331 has an opening width larger than the thickness of the upright honeycomb panel 30, and the groove bottom 333 of one of the pair of U-shaped profiles 33 is connected to the first honeycomb panel 1, and the other groove bottom 333 is connected to the second honeycomb panel 2, The connection may be by adhesive bonding, the ends of the upright honeycomb panel 30 are not sealed, and are respectively inserted into the grooves 331 of the pair of U-shaped profiles 33, and the inside of the groove walls 332 on both sides of the U-shaped profile 33 The groove bottom 333 is maintained at a distance to form a filling gap, and a filling material layer 34 is provided in the filling gap. The filling material layer 34 fills the filling gap and the honeycomb body 30 is inserted into the honeycomb core portion of the pair of U-shaped profiles 33. The first honeycomb plate 1 is inserted into the groove 331 of the U-shaped profile 333 having a width greater than the thickness thereof, and the position between the first honeycomb plate 1, the second honeycomb plate 2 and the upright honeycomb plate 30 can be adjusted to make the first honeycomb plate 1. The connection between the second honeycomb panel 2 and the upright honeycomb panel 30 is better. The filler material layer 34 not only serves to strengthen the connection between the upright honeycomb panel 30 and the U-shaped profile 33, but also because the upright honeycomb panel 30 is inserted into a pair of U-shaped shapes. The ends of the profile 33 are not edge-sealed, and the layer of filler material 34 simultaneously fills the interior of the honeycomb core material in which the upright honeycomb panel 30 is inserted into a pair of U-shaped profiles 33, such that the upright honeycomb panel 30 is inserted into a portion of the pair of U-shaped profiles 33. Also strengthened.
进一步的, 一对 U形型材 33分别与第一蜂巢板 1和第二蜂巢板 2之间有填充材料层 (未在图中标出)。 此填充层材料层可以调整 U形型材 33与第一蜂巢板 1和第二蜂巢板 2 之间的间隙, 以使 U形型材 33与第一蜂巢板 1和第二蜂巢板 2之间连接配合更好, 同时 又可以防止 U形型材 33与第一蜂巢板 1和第二蜂巢板 2连接处的液体渗漏, 以达到防止 雨水渗入风力发电机风轮叶片内部的目的。  Further, a pair of U-shaped profiles 33 have a layer of filler material (not shown) between the first honeycomb panel 1 and the second honeycomb panel 2, respectively. The layer of filling layer material can adjust the gap between the U-shaped profile 33 and the first honeycomb panel 1 and the second honeycomb panel 2 to connect the U-shaped profile 33 with the first honeycomb panel 1 and the second honeycomb panel 2 More preferably, at the same time, liquid leakage at the junction of the U-shaped profile 33 with the first honeycomb panel 1 and the second honeycomb panel 2 can be prevented to prevent the rainwater from penetrating into the interior of the wind turbine blade.
迸一步的,一对 U形型材 33的槽底 333与第一蜂巢板 1和第二蜂巢板 2之间分别设 有沉孔且有紧固件通过该沉孔分别将第一蜂巢板 1和一对 U形型材 33其中之一以及第二 蜂巢板 2和一对 U形型材 33其中另一连接在一起。采用沉孔和紧固件连接可以使风力发 电机风轮叶片表面平整, 既可保证空气动力学性能又便于进行表面处理。  Further, a groove bottom 333 of the pair of U-shaped profiles 33 is respectively provided with a counterbore between the first honeycomb plate 1 and the second honeycomb plate 2, and a fastener passes through the counterbore respectively to respectively the first honeycomb plate 1 and One of the pair of U-shaped profiles 33 and the second honeycomb panel 2 and a pair of U-shaped profiles 33 are joined together. The use of countersinks and fastener connections allows the surface of the wind turbine rotor blades to be flat, ensuring aerodynamic performance and surface treatment.
进一步的, 壳体可以由多段拼接组成, 如图 12所示, 以前段壳体的第一蜂巢板为前 段蜂巢板 61, 以后段壳体的第一蜂巢板为后蜂巢板 62,前蜂巢板 61与后蜂巢板 62拼接, 前蜂巢板 61的上面板 61 1与后蜂巢板 62的上面板 621拼合, 前蜂巢板 61的下面板 612 与后蜂巢板 62的下面板 622拼合, 前蜂巢板 61的蜂巢状芯材 613与后蜂巢板 62的蜂巢 状芯材 623于拼接部位贴合,前蜂巢板 61和后蜂巢板 62之间有第三连接部件,第三连接 部件为上部连接板 631和下部连接板 632,上部连接板 631覆盖前蜂巢板 61的上面板 611 和后蜂巢板 62的上面板 621的拼合接缝, 并与前蜂巢板 61上面板 61 1和后蜂巢板 62上 面板 621连接, 下部连接板 632覆盖前蜂巢板 61的下面板 612和后蜂巢板 62的下面板 622的拼合接缝, 并与前蜂巢板 61下面板 612和后蜂巢板 62下面板 622连接, 两段壳体 的第二蜂巢板之间的连接方式与两段壳体的第一蜂巢板的连接方式相同。上部连接板 631 与前蜂巢板 61的上面板 61 1和后蜂巢板 62的上面板 621的连接方式为粘接,上部连接板 631与前蜂巢板 61的上面板 61 1和后蜂巢板 62的上面板 621的连接部位有粘接剂层 641, 下部连接板 632与前蜂巢板 61的下面板 612和后蜂巢板 62的下面板 622的连接方式为粘 接,下部连接板 632与前蜂巢板 61的下面板 612和后蜂巢板 62的下面板 622的连接部位 有粘接剂层 642。 此拼接方式的优点是, 当前蜂巢板 61与后蜂巢板 62拼接时不可避免的 会存在缝隙,而上部连接板 631与下部连接板 632可将前蜂巢板 61与后蜂巢板 62拼接时 产生的缝隙覆盖, 同时由于粘接剂层 641和 642在涂覆时能渗入前蜂巢板 61与后蜂巢板 62拼接时产生的缝隙中,并流入于拼接位置的前蜂巢板 61的蜂巢状芯材 613和后蜂巢板 62的蜂巢状芯材 623中,随着粘接剂固化使前蜂巢板 61的蜂巢状芯材 613与后蜂巢板 62 的蜂巢状芯材 623之间产生牢固的连接,并将前蜂巢板 61与后蜂巢板 62拼合时产生的缝 隙填满, 进而使前蜂巢板 61与后蜂巢板 62的拼接更牢固。 Further, the housing may be composed of a plurality of segments, as shown in FIG. 12, the first honeycomb panel of the previous housing is front. The segment honeycomb plate 61, the first honeycomb plate of the later casing is the rear honeycomb plate 62, the front honeycomb plate 61 and the rear honeycomb plate 62 are spliced, and the upper panel 61 1 of the front honeycomb panel 61 and the upper panel 621 of the rear honeycomb panel 62 are joined together. The lower panel 612 of the front honeycomb panel 61 is joined to the lower panel 622 of the rear honeycomb panel 62. The honeycomb core material 613 of the front honeycomb panel 61 and the honeycomb core material 623 of the rear honeycomb panel 62 are attached to the splicing portion, and the front honeycomb panel is attached. There is a third connecting member between the 61 and the rear honeycomb panel 62. The third connecting member is an upper connecting plate 631 and a lower connecting plate 632. The upper connecting plate 631 covers the upper panel 611 of the front honeycomb panel 61 and the upper panel of the rear honeycomb panel 62. The split seam of 621 is connected to the upper honeycomb panel 61 upper panel 61 1 and the rear honeycomb panel 62 upper panel 621, and the lower connecting panel 632 covers the lower panel 612 of the front honeycomb panel 61 and the lower panel 622 of the rear honeycomb panel 62. The seam is connected to the lower panel 612 of the front honeycomb panel 61 and the lower panel 622 of the rear honeycomb panel 62. The connection between the second honeycomb panels of the two-stage housing is the same as that of the first honeycomb panel of the two-segment housing. . The upper connecting plate 631 is bonded to the upper panel 61 1 of the front honeycomb panel 61 and the upper panel 621 of the rear honeycomb panel 62, and the upper connecting panel 631 and the upper panel 61 1 of the front honeycomb panel 61 and the rear honeycomb panel 62 are bonded. The connecting portion of the upper panel 621 has an adhesive layer 641. The lower connecting plate 632 is bonded to the lower panel 612 of the front honeycomb panel 61 and the lower panel 622 of the rear honeycomb panel 62. The lower connecting panel 632 and the front honeycomb panel are attached. An adhesive layer 642 is formed at a joint portion of the lower panel 612 of the 61 and the lower panel 622 of the rear honeycomb panel 62. The advantage of this splicing method is that there is inevitably a gap between the current honeycomb panel 61 and the rear honeycomb panel 62, and the upper connecting panel 631 and the lower connecting panel 632 can be combined with the front honeycomb panel 61 and the rear honeycomb panel 62. The gap covers, and at the same time, the adhesive layers 641 and 642 can penetrate into the gap formed when the front honeycomb plate 61 and the rear honeycomb plate 62 are spliced at the time of coating, and flow into the honeycomb core member 613 of the front honeycomb plate 61 at the splicing position. And the honeycomb core material 623 of the rear honeycomb plate 62, a solid connection between the honeycomb core material 613 of the front honeycomb plate 61 and the honeycomb core material 623 of the rear honeycomb plate 62 is formed as the adhesive is solidified, and The gap formed when the front honeycomb panel 61 and the rear honeycomb panel 62 are joined together is filled, thereby further splicing the front honeycomb panel 61 and the rear honeycomb panel 62.
进一步的,如图 13所示,上部连接板 631覆盖前蜂巢板 61的上面板 611和后蜂巢板 62的上面板 621的拼合接缝朝向蜂巢状芯材 613和 623的一面, 下部连接板 632覆盖前 蜂巢板 61的下面板 612和后蜂巢板 62的下面板 622的拼合接缝朝向蜂巢状芯材 613和 623的一面。 此种拼接形式可以使第一蜂巢板 1和第二蜂巢板 2的拼接部位表面平整, 对 风力发电机风轮叶片而言, 既不影响工件整体的空气动力学性能, 又便于进行表面处理。 在此基础上, 上部连接板 631伸入前蜂巢板 61上面板 611和蜂巢状芯材 613之间的长度 与其伸入后蜂巢板 62上面板 621和蜂巢状芯材 623之间的长度相等, 下部连接板 632伸 入前蜂巢板 61下面板 612和蜂巢状芯材 613之间的长度与其伸入后蜂巢板 62下面板 622 和蜂巢状芯材 623之间的长度相等。 此形式的拼接使上部连接板 631 和下部连接板 632 受力均勾, 可防止上部连接板 631和下部连接板 632出现变形。 进一步的,上部连接板 631可以有多块,多块上部连接板 631为长条形并相互以一定 间隔连接前蜂巢板 61上面板 611和后蜂巢板 62上面板 621。下部连接板 632可以有多块, 下部连接板 632为长条形并相互以一定间隔连接前蜂巢板 61下面板 612和后蜂巢板 62 下面板 622。 通过选择粘接强度较强的粘接剂可以减小上部连接板 631和下部连接板 632 的粘接面积, 即可减小上部连接板 631和下部连接板 632的尺寸,如此不但能减轻工件的 整体重量,而且在上部连接板 631和下部连接板 632朝向蜂巢状芯材 613和 623的实施方 式中, 宽度较小的上部连接板 631和下部连接板 632更容易压入蜂巢状芯材 613和 623 中, 简化了生产工艺。 Further, as shown in FIG. 13, the upper connecting plate 631 covers the split joint of the upper panel 611 of the front honeycomb panel 61 and the upper panel 621 of the rear honeycomb panel 62 toward the side of the honeycomb core members 613 and 623, and the lower connecting panel 632. The split seam covering the lower panel 612 of the front honeycomb panel 61 and the lower panel 622 of the rear honeycomb panel 62 faces one side of the honeycomb core members 613 and 623. The splicing form can make the surface of the splicing part of the first honeycomb board 1 and the second honeycomb board 2 flat, and the wind turbine blade does not affect the overall aerodynamic performance of the workpiece, and is convenient for surface treatment. On the basis of this, the length of the upper connecting plate 631 extending into the upper honeycomb panel 61 upper panel 611 and the honeycomb core 613 is equal to the length between the upper panel 621 and the honeycomb core 623 of the honeycomb panel 62. The length of the lower web 632 extending between the lower panel 612 of the front honeycomb panel 61 and the honeycomb core 613 is equal to the length between the lower panel 622 and the honeycomb core 623 of the honeycomb panel 62. This form of splicing forces the upper connecting plate 631 and the lower connecting plate 632 to be evenly hooked to prevent deformation of the upper connecting plate 631 and the lower connecting plate 632. Further, the upper connecting plate 631 may have a plurality of pieces, and the plurality of upper connecting plates 631 are elongated and connected to the front honeycomb panel 61 upper panel 611 and the rear honeycomb panel 62 upper panel 621 at a certain interval. The lower connecting plate 632 may have a plurality of pieces, and the lower connecting plate 632 has an elongated shape and is connected to the front honeycomb plate 61 lower panel 612 and the rear honeycomb plate 62 lower plate 622 at intervals. By selecting an adhesive having a strong bonding strength, the bonding area of the upper connecting plate 631 and the lower connecting plate 632 can be reduced, and the size of the upper connecting plate 631 and the lower connecting plate 632 can be reduced, so that the workpiece can be lightened. The overall weight, and in the embodiment in which the upper connecting plate 631 and the lower connecting plate 632 are oriented toward the honeycomb core members 613 and 623, the upper connecting plate 631 and the lower connecting plate 632 having a smaller width are more easily pressed into the honeycomb core member 613 and In 623, the production process is simplified.
进一步的, 如图 14所示, 直立蜂巢板由多段连接而成, 以前段的直立蜂巢板为前直 立蜂巢板 71, 以后段的直立蜂巢板为后直立蜂巢板 72,前直立蜂巢板 71边缘与后直立蜂 巢板 72边缘连接, 且前直立蜂巢板 71与后直立蜂巢板 72在同一平面内, 前直立蜂巢板 71和后直立蜂巢板 72相互连接的一侧没有封边,前直立蜂巢板 71与后直立蜂巢板 72之 间有第四连接部件,第四连接部件为 H形型材 73, H形型材包括第一槽口 731和第二槽 口 732, 第一槽口 731和第二槽口 732分别包括两侧槽壁 731 1、 7321和槽底 7312、 7322, 前直立蜂巢板 71插入第一槽口 731且与 H形型材 73连接,后直立蜂巢板 72插入第二槽 口 732且与 H形型材 73连接,前直立蜂巢板 71与第一槽口 731的两侧槽壁 7311内侧及 槽底 7312保持一定距离, 形成第一填充间隙 741, 后直立蜂巢板 72与第二槽口 732的两 侧槽壁 7321内侧及槽底 7322保持一定距离, 形成第二填充空间 742, 第一填充空间 741 及第二填充空间 742内设有填充材料层, 填充材料层充满前直立蜂巢板 71插入第一槽口 731部分的蜂巢状芯材内及后直立蜂巢板 72插入第二槽口 732部分的蜂巢状芯材内。 H 形型材 73的第一槽口 731和第二槽口 732的开口宽度大于前直立蜂巢板 71和后直立蜂巢 板 72的厚度, 此种连接形式在连接安装时可以调整前直立蜂巢板 71和后直立蜂巢板 72 之间的位置, 尤其是在长度尺寸较大的工件分成多段加工, 需组合连接时, 由于各段之间 可能存在一定误差或者组合时存在一定间隙, 通过 H形型材 73即可调整误差或者间隙。 前直立蜂巢板 71及后直立蜂巢板 72的上下面板与 H形型材 73的第一槽口 731的槽壁 731 1及第二槽口 732的槽壁 7321通过紧固件 751、 752连接, 填充材料层对前直立蜂巢 板 71及后直立蜂巢板 72与 H形型材的连接部位进行加固, 同时由于填充材料层充满前 直立蜂巢板 71插入第一槽口 731部分的蜂巢状芯材内及后直立蜂巢板 72插入第二槽口 732部分的蜂巢状芯材内, 使前直立蜂巢板 71插入第一槽口 731部分和后直立蜂巢板 72 插入第二槽口 732部分的强度得到加强, 可防止连接后连接部位出现受力变形。 进一步的, 如图 15所示, 在此对前文提到的沉孔作出说明, 将开设沉孔的蜂巢板称 为待连接蜂巢板, 将需与待连接蜂巢板连接的型材称为连接件 82, 带连接蜂巢板包括待 连接上面板 811、 待连接下面板 812和待连接蜂巢状芯材 813, 待连接蜂巢状芯材 813包 括多个六角形腔室,沉孔包括连接结构,连接结构包括加固层 831和通孔 832,加固层 831 主要由待连接蜂巢状芯材 813和六角形腔室内的加固填充材料层组成,加固填充材料层充 满六角形腔室,加固填充材料层为硬质弹性填充材料层,加固层 831面积小于待连接蜂巢 板的面积,加固层 831面积大于连接件 82与待连接蜂巢板连接部位的接触面积,通孔 832 穿透待连接上面板 81 1、 待连接下面 812板及加固层 831, 通孔 832包括台阶 8321, 台阶 8321位于待连接蜂巢板不与连接件 82连接的一侧, 可用一紧固件 84穿过通孔 832将待 连接蜂巢板和连接件 82连接。 由于蜂巢板的蜂巢状芯材一般为薄壁多孔材料, 很难采用 传统紧固件进行连接, 所以现有的蜂巢板连接结构一般是以上下面板同连接件进行连接, 这种形式的连接结构由于只连接蜂巢板的上下面板很容易在上下面板的连接部位产生变 形。本发明描述的沉孔釆用填充材料层将蜂巢板上一定区域内的蜂巢状芯材的六角形腔体 填满形成加固层,使该区域的蜂巢状芯材强度增加,易于实现采用传统紧固件与连接部件 进行连接的连接方式,这样就减少了蜂巢板与连接件的连接部位出现变形的可能,优选的, 填充材料层可以是硬质弹性填充材料层,这样可以进一步降低蜂巢板与连接件的连接部位 出现变形的可能。在此基础上,加固层面积可以大于连接件与蜂巢板连接部位的接触面积, 这样可以提高蜂巢板与连接件连接部位的强度。 Further, as shown in FIG. 14, the erect honeycomb panels are connected by a plurality of segments. The erect honeycomb panels of the previous section are the front erect honeycomb panels 71, and the erect honeycomb panels of the later section are the rear erect honeycomb panels 72, and the front erect honeycomb panels 71. Connected to the edge of the rear upright honeycomb panel 72, and the front upright honeycomb panel 71 and the rear upright honeycomb panel 72 are in the same plane, the front side of the front upright honeycomb panel 71 and the rear upright honeycomb panel 72 are not sealed, and the front upright honeycomb panel There is a fourth connecting member between the 71 and the rear upright honeycomb panel 72. The fourth connecting member is an H-shaped profile 73. The H-shaped profile includes a first notch 731 and a second notch 732, a first notch 731 and a second groove. The ports 732 respectively include two side groove walls 731 1 and 7321 and groove bottoms 7312 and 7322. The front upright honeycomb plate 71 is inserted into the first notch 731 and connected to the H-shaped profile 73, and the rear upright honeycomb plate 72 is inserted into the second notch 732 and The H-shaped profile 73 is connected, and the front upright honeycomb panel 71 is spaced apart from the inner side of the groove wall 7311 of the first notch 731 and the groove bottom 7312 to form a first filling gap 741, and the rear vertical honeycomb panel 72 and the second notch. 732 has a groove wall 7321 on both sides and a groove bottom 7322 to maintain a a second filling space 742 is formed. The first filling space 741 and the second filling space 742 are provided with a filling material layer. The filling material layer is filled with the front vertical honeycomb panel 71 inserted into the honeycomb core of the first notch 731 portion and The rear upright honeycomb panel 72 is inserted into the honeycomb core of the second slot 732 portion. The opening width of the first notch 731 and the second notch 732 of the H-shaped profile 73 is greater than the thickness of the front upright honeycomb panel 71 and the rear upright honeycomb panel 72, and this connection form can adjust the front upright honeycomb panel 71 and the connection installation. The position between the upright honeycomb panels 72, especially in the case of a workpiece having a large length, is divided into a plurality of sections. When a combination is required, there may be a certain error between the segments or a certain gap when combined, and the H-shaped profile 73 is The error or gap can be adjusted. The upper and lower panels of the front upright honeycomb panel 71 and the rear upright honeycomb panel 72 and the slot wall 731 1 of the first slot 731 of the H-shaped profile 73 and the slot wall 7321 of the second slot 732 are connected by fasteners 751, 752, and filled. The material layer reinforces the joint portion of the front upright honeycomb panel 71 and the rear upright honeycomb panel 72 and the H-shaped profile, and at the same time, the filler material layer is filled with the front upright honeycomb panel 71 inserted into the honeycomb core of the first notch 731 portion and thereafter. The upright honeycomb panel 72 is inserted into the honeycomb core of the second slot 732 portion, and the strength of the portion of the front upright honeycomb panel 71 inserted into the first slot 731 and the rear upright honeycomb panel 72 inserted into the second slot 732 is enhanced. Prevent the joint deformation of the joint after the connection. Further, as shown in FIG. 15, the above-mentioned counterbore is described. The honeycomb panel in which the counterbore is opened is referred to as the honeycomb panel to be connected, and the profile to be connected to the honeycomb panel to be connected is referred to as a connector 82. The connection honeycomb panel includes an upper panel 811 to be connected, a lower panel 812 to be connected, and a honeycomb core 813 to be connected. The honeycomb core 813 to be connected includes a plurality of hexagonal chambers, and the counterbore includes a connection structure, and the connection structure includes The reinforcing layer 831 and the through hole 832, the reinforcing layer 831 is mainly composed of a honeycomb core material 813 to be connected and a reinforcing filling material layer in the hexagonal cavity, the reinforcing filling material layer is filled with the hexagonal cavity, and the reinforcing filling material layer is hard elastic. The area of the filling material layer, the area of the reinforcing layer 831 is smaller than the area of the honeycomb board to be connected, the area of the reinforcing layer 831 is larger than the contact area of the connecting part of the connecting piece 82 and the honeycomb board to be connected, and the through hole 832 penetrates the upper panel 81 1 to be connected, to be connected below. The 812 plate and the reinforcing layer 831, the through hole 832 includes a step 8321, and the step 8321 is located on a side where the honeycomb plate to be connected is not connected to the connecting member 82, and a fastener 84 is passed through the through hole 832 to be connected. Nest plate 82 and the connecting member is connected. Since the honeycomb core material of the honeycomb panel is generally a thin-walled porous material, it is difficult to connect with a conventional fastener, so the existing honeycomb panel connection structure is generally that the upper lower panel is connected with the connecting member, and the connection structure of this form is adopted. Since only the upper and lower panels of the honeycomb panel are connected, it is easy to deform at the joint portion of the upper and lower panels. The counterbore filling material layer described in the present invention fills the hexagonal cavity of the honeycomb core material in a certain area on the honeycomb panel to form a reinforcing layer, so that the strength of the honeycomb core material in the region is increased, and the traditional tightness is easily realized. The connection manner of the firmware and the connecting component, thereby reducing the possibility of deformation of the connection portion between the honeycomb panel and the connecting member. Preferably, the filling material layer may be a hard elastic filling material layer, which can further reduce the honeycomb panel and The connection portion of the connector may be deformed. On the basis of this, the area of the reinforcing layer can be larger than the contact area of the connecting part of the connecting piece and the honeycomb board, so that the strength of the joint portion of the honeycomb board and the connecting piece can be improved.
进一步的第一蜂巢板 1和所述第二蜂巢板 2可以是铝蜂巢板。铝蜂巢板质轻耐压力强, 是制造风力发电机风轮叶片的优选材料。  Further first honeycomb panels 1 and said second honeycomb panels 2 may be aluminum honeycomb panels. The aluminum honeycomb panel is light and resistant to pressure and is the preferred material for the manufacture of wind turbine blades.
进一步的, 壳体外侧包覆保护涂层, 包覆保护涂层可防止风力发电机风轮叶片老化、 腐蚀。 优选的, 保护涂层可以是环氧树脂涂层。 环氧树脂附着力强, 固化收缩率小, 稳定 性好,抗化学药品性优良, 同时又不错的耐热性适合作为风力发电机风轮叶片外层保护涂 层材料。  Further, the outer side of the casing is covered with a protective coating, and the protective coating is coated to prevent aging and corrosion of the wind turbine blade. Preferably, the protective coating may be an epoxy coating. Epoxy resin has strong adhesion, low cure shrinkage, good stability, excellent chemical resistance, and good heat resistance. It is suitable as the outer layer protective coating material for wind turbine blades.
以上所述仅为本发明较佳的实施例,并非因此限制本发明的申请专利范围,所以凡运 用本发明说明书及图示内容所作出的等效结构变化, 均包含在本发明的保护范围内。  The above is only the preferred embodiment of the present invention, and is not intended to limit the scope of the claims of the present invention. Therefore, equivalent structural changes made by using the specification and the description of the present invention are included in the scope of the present invention. .

Claims

权 利 要 求 书 Claim
1 . 一种全蜂巢板风力发电机风轮叶片, 包括壳体和内部支撑结构, 所述壳体主要由上半 壳与下半壳组合而成,所述内部支撑结构置于所述壳体内并与所述上半壳及所述下半壳的 支撑部位分别连接, 其特征在于, 所述上半壳由第一蜂巢板弯曲形成, 所述下半壳由第二 蜂巢板弯曲形成, 所述内部支撑结构为纵向支撑板, 所述纵向支撑板由直立蜂巢板形成, 所述纵向支撑板与所述壳体于所述支撑部位的纵向截面形状相同且大小匹配,所述第一蜂 巢板、第二蜂巢板及所述直立蜂巢板包括上面板、 下面板、 蜂巢状芯材, 所述蜂巢状芯材 置于所述下面板上并与所述下面板紧密贴合,所述上面板覆于所述蜂巢状芯材上,并与所 述蜂巢状芯材紧密贴合。 What is claimed is: 1. A fully honeycomb panel wind turbine blade comprising a housing and an inner support structure, the housing being mainly composed of an upper half shell and a lower half shell, the inner support structure being disposed in the shell And connecting to the support portions of the upper half shell and the lower half shell, respectively, wherein the upper half shell is formed by bending of a first honeycomb panel, and the lower half shell is formed by bending of a second honeycomb panel. The inner support structure is a longitudinal support plate, and the longitudinal support plate is formed by an upright honeycomb plate, and the longitudinal support plate and the casing have the same longitudinal cross-sectional shape at the support portion, and the size is matched, the first honeycomb plate The second honeycomb panel and the upright honeycomb panel comprise an upper panel, a lower panel, and a honeycomb core material, wherein the honeycomb core material is placed on the lower panel and closely adheres to the lower panel, the upper panel Covering the honeycomb core material and closely adhering to the honeycomb core material.
2. 如权利要求 1所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述壳体横截面为水 滴形,所述水滴形尾部为所述风力发电机风轮叶片的扰流角,所述扰流角主要由第一蜂巢 板和第二蜂巢板组合而成;所述第一蜂巢板包括第一斜面,所述第一斜面于其横截面上形 成第一锐角和第一钝角,所述第一斜面横截面对应的所述第一锐角形成所述扰流角,所述 第二蜂巢板包括第二斜面,所述第二斜面于其横截面上形成第二锐角和第二钝角,所述第 二锐角与所述第二钝角共用的一边与所述第一钝角不与所述第一锐角共用的一边贴合并 连接, 且所述第二锐角的顶点与所述第一钝角的顶点接触。 2. The full honeycomb panel wind turbine blade according to claim 1, wherein the casing has a teardrop shape in cross section, and the water droplet tail is a spoiler angle of the wind turbine blade The spoiler angle is mainly composed of a first honeycomb plate and a second honeycomb plate; the first honeycomb plate includes a first inclined surface, and the first inclined surface forms a first acute angle and a first obtuse angle on a cross section thereof The first acute angle corresponding to the first bevel cross section forms the spoiler angle, the second honeycomb panel includes a second inclined surface, the second inclined surface forms a second acute angle and a second cross section thereof An obtuse angle, a side of the second acute angle shared with the second obtuse angle and a side of the first obtuse angle not shared by the first acute angle, and a vertex of the second acute angle and the first obtuse angle The apex touch.
3. 如权利要求 1所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述壳体横截面为水 滴形,所述水滴形头部为所述风力发电机风轮叶片的迎风端,所述迎风端包括第一蜂巢板 和第二蜂巢板,所述第一蜂巢板与所述第二蜂巢板厚度相同,所述第一蜂巢板与所述第二 蜂巢板连接,其连接部位形成所述迎风端,所述第一蜂巢板和第二蜂巢板之间有第一连接 部件, 所述第一连接部件包括- 第一槽形型材和第二槽形型材, 所述第一槽形型材和所述第二槽形型材形状相同; 所述第一槽形型材包括槽口和槽底,所述第一槽形型材槽口宽度小于所述第一蜂巢板的厚 度,所述第一槽形型材槽口向外与所述第一蜂巢板连接,且使所述第一槽形型材槽底嵌入 所述第一蜂巢板的上下面板之间并使所述第一槽形型材的槽口与所述第一蜂巢板板边齐 所述第二槽形型材包括槽口和槽底,所述第二槽形型材槽口宽度小于所述第二蜂巢板的厚 度,所述第二槽形型材槽口向外与所述第二蜂巢板连接,且使所述第二槽形型材槽底嵌入 所述第二蜂巢板的上下面板之间并使所述第二槽形型材的槽口与所述第二蜂巢板板边齐 平; 3. The full honeycomb panel wind turbine blade according to claim 1, wherein the casing has a teardrop shape in cross section, and the teardrop shaped head is a windward end of the wind turbine blade. The windward end includes a first honeycomb plate and a second honeycomb plate, the first honeycomb plate and the second honeycomb plate have the same thickness, and the first honeycomb plate is connected to the second honeycomb plate, and the connecting portion thereof Forming the windward end, a first connecting member is disposed between the first honeycomb plate and the second honeycomb plate, and the first connecting member includes a first groove shape and a second groove shape, the first groove The profiled shape and the second channel profile are identical in shape; the first channel profile includes a slot and a slot bottom, the first slot profile slot width being less than a thickness of the first honeycomb panel, the first a slotted profile slot is outwardly coupled to the first honeycomb panel, and the first channel profile slot bottom is embedded between the upper and lower panels of the first honeycomb panel and the first channel profile is The slot is flush with the first honeycomb panel The second channel profile includes a notch and a groove bottom, the second channel profile slot width is smaller than the thickness of the second honeycomb panel, and the second channel profile slot is outward and the second The honeycomb panels are connected, and the bottom of the second channel profile is embedded between the upper and lower panels of the second honeycomb panel and the notches of the second channel profile are flush with the edge of the second honeycomb panel ;
还包括多边形型材,所述多边形型材以其中线划分成左半部和右半部,所述左半部与所述 右半部关于所述多边形型材的中线对称,所述左半部横截面形状与所述第一槽形型材横截 面形状匹配,所述右半部横截面形状与所述第二槽形型材横截面形状匹配,所述多边形型 材的左半部伸入所述第一槽形型材并与其连接,所述多边形型材的右半部伸入所述第二槽 形型材并与其连接。 Also included is a polygonal profile that is divided into a left half and a right half in a centerline, the left half and the right half being symmetric about a centerline of the polygonal profile, the left half cross-sectional shape Matching the cross-sectional shape of the first channel profile, the right half cross-sectional shape matching the second channel profile cross-sectional shape, the left half of the polygonal profile extending into the first channel shape The profile is connected thereto and the right half of the polygonal profile projects into and is connected to the second channel profile.
4. 如权利要求 1所述全蜂巢板风力发电机风轮叶片, 其特征在于, 形成所述纵向支撑板 的直立蜂巢板与所述第一蜂巢板和所述第二蜂巢板分别连接,所述直立蜂巢板与所述第一 蜂巢板和所述第二蜂巢板之间有一对第二连接部件,所述一对第二连接部件为 U形型材, 所述 U形型材包括凹槽、 两侧槽壁和槽底, 所述 U形型材的凹槽开口宽度大于所述直立 蜂巢板的厚度, 所述一对 U形型材其中之一的槽底与所述第一蜂巢板连接, 其中另一的 槽底与所述第二蜂巢板连接, 所述直立蜂巢板两端没有封边, 且分别插入所述一对 U形 型材的凹槽中, 并与所述 U形型材的两侧槽壁内侧及槽底保持一定距离以形成填充间隙, 所述填充间隙内设有填充材料层,所述填充材料层充满所述填充间隙及所述直立蜂巢板插 入所述一对 U形型材部分的蜂巢状芯材内部。 4. The full honeycomb panel wind turbine blade according to claim 1, wherein an upright honeycomb panel forming the longitudinal support panel is respectively connected to the first honeycomb panel and the second honeycomb panel, Between the upright honeycomb panel and the first honeycomb panel and the second honeycomb panel, there is a pair of second connecting members, the pair of second connecting members are U-shaped profiles, and the U-shaped profiles include grooves, two a side groove wall and a groove bottom, the groove opening width of the U-shaped profile is larger than the thickness of the upright honeycomb plate, and the groove bottom of one of the pair of U-shaped profiles is connected to the first honeycomb plate, wherein a groove bottom is connected to the second honeycomb plate, the two ends of the upright honeycomb plate are not sealed, and are respectively inserted into the grooves of the pair of U-shaped profiles, and the grooves on both sides of the U-shaped profile The inner side of the wall and the bottom of the groove are kept at a distance to form a filling gap, and the filling gap is provided with a filling material layer, the filling material layer filling the filling gap and the erect honeycomb panel being inserted into the pair of U-shaped profiles Honeycomb core inside.
5. 如权利要求 1所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述壳体由多段拼接 组成, 以前段壳体的所述第一蜂巢板为前段蜂巢板, 以后段壳体的所述第一蜂巢板为后蜂 巢板,所述前蜂巢板与所述后蜂巢板拼接,所述前蜂巢板的上面板与所述后蜂巢板的上面 板拼合,所述前蜂巢板的下面板与所述后蜂巢板的下面板拼合,所述前蜂巢板的蜂巢状芯 材与所述后蜂巢板的蜂巢状芯材于拼接部位贴合,所述前蜂巢板和所述后蜂巢板之间有第 三连接部件,所述第三连接部件为上部连接板和下部连接板,所述上部连接板覆盖所述前 蜂巢板的上面板和所述后蜂巢板的上面板的拼合接缝,并与所述前蜂巢板上面板和所述后 蜂巢板上面板连接,所述下部连接板覆盖所述前蜂巢板的下面板和所述后蜂巢板的下面板 的拼合接缝,并与所述前蜂巢板下面板和所述后蜂巢板下面板连接,两段壳体的所述第二 蜂巢板之间的连接方式与两段壳体的所述第一蜂巢板的连接方式相同。 5. The full honeycomb panel wind turbine blade according to claim 1, wherein the casing is composed of a plurality of segments, and the first honeycomb plate of the previous casing is a front honeycomb plate, and the rear casing is The first honeycomb panel of the body is a rear honeycomb panel, the front honeycomb panel is spliced with the rear honeycomb panel, and an upper panel of the front honeycomb panel is assembled with an upper panel of the rear honeycomb panel, the front honeycomb panel The lower panel is joined to the lower panel of the rear honeycomb panel, and the honeycomb core material of the front honeycomb panel and the honeycomb core material of the rear honeycomb panel are attached to the splicing portion, the front honeycomb panel and the rear honeycomb panel There is a third connecting component between the honeycomb panels, the third connecting component is an upper connecting plate and a lower connecting plate, and the upper connecting plate covers the upper panel of the front honeycomb panel and the upper panel of the rear honeycomb panel a seam and is connected to the front honeycomb panel and the rear honeycomb panel, the lower connector covering the split seam of the lower panel of the front honeycomb panel and the lower panel of the rear honeycomb panel, And with the front honeycomb panel lower panel and the rear Lower nest plate panels are connected, the same connection mode connection between the two housing plates and two second honeycomb housing a first honeycomb plate.
6. 如权利要求 2所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一锐角和所述 第二锐角共同形成所述扰流角,所述第二锐角与所述第二钝角共用的边与所述第一锐角与 所述第一钝角共用的边贴合并连接,且第二锐角的顶点与所述第一锐角的顶点接触,所述 第二钝角的顶点与所述第一钝角的顶点接触。 6. The full honeycomb panel wind turbine blade according to claim 2, wherein the first acute angle and the second acute angle together form the spoiler angle, the second acute angle and the first a side shared by the two obtuse angles is joined to the side edge of the first acute angle and the first obtuse angle, and a vertex of the second acute angle is in contact with an apex of the first acute angle, and a vertex of the second obtuse angle is The apex of the first obtuse angle contacts.
7. 如权利要求 2所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一蜂巢板和所 述第二蜂巢板的连接方式为紧固件连接。 7. The full honeycomb panel wind turbine blade according to claim 2, wherein the first honeycomb panel and the second honeycomb panel are connected by a fastener.
8. 如权利要求 3所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一槽形型材与 所述第一蜂巢板之间有填充材料层,所述第二槽形型材与所述第二蜂巢板之间有填充材料 层。 8. The full honeycomb panel wind turbine blade according to claim 3, wherein a filler material layer is disposed between the first channel profile and the first honeycomb panel, and the second channel profile There is a layer of filler material between the second honeycomb panel.
9. 如权利要求 3所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述多边形型材与所 述第一槽形型材及所述第二槽形型材之间有填充材料层。 9. The full honeycomb panel wind turbine blade according to claim 3, wherein a filler material layer is disposed between the polygonal profile and the first channel profile and the second channel profile.
10. 如权利要求 3所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一槽形型材包 括两侧槽壁,一对沉孔分别穿透所述第一蜂巢板的上下面板及所述第一槽形型材的两侧槽 壁,并通过一对穿过该对沉孔的紧固件将所述第一蜂巢板、所述第一槽形型材和所述多边 形型材的左半部连接在一起。 10. The full honeycomb panel wind turbine blade according to claim 3, wherein the first channel profile comprises two side groove walls, and a pair of counterbore holes respectively penetrate the upper and lower sides of the first honeycomb plate a panel and a groove wall on both sides of the first channel profile and passing the first honeycomb panel, the first channel profile and the polygonal profile by a pair of fasteners passing through the pair of counterbore The left half is connected together.
11 . 如权利要求 3所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第二槽形型材包 括两侧槽壁,一对沉孔分别穿透所述第二蜂巢板的上下面板及所述第二槽形型材的两侧槽 壁,并通过一对穿过该对沉孔的紧固件将所述第二蜂巢板、所述第二槽形型材和所述多边 形型材的右半部连接在一起。 11. The full honeycomb panel wind turbine blade according to claim 3, wherein the second channel profile comprises two side groove walls, and the pair of counter holes penetrate the upper and lower sides of the second honeycomb plate respectively a panel and a groove wall on both sides of the second channel profile, and passing the second honeycomb panel, the second channel profile and the polygonal profile by a pair of fasteners passing through the pair of counterbore The right half is connected together.
12. 如权利要求 4所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述直立蜂巢板由多 段连接而成, 以前段的所述直立蜂巢板为前直立蜂巢板, 以后段的所述直立蜂巢板为后直 立蜂巢板,所述前直立蜂巢板边缘与所述后直立蜂巢板边缘连接,且所述前直立蜂巢板与 所述后直立蜂巢板在同一平面内,所述前直立蜂巢板和所述后直立蜂巢板相互连接的一侧 没有封边,所述前直立蜂巢板与所述后直立蜂巢板之间有第四连接部件,所述第四连接部 件为 H形型材, 所述 H形型材包括第一槽口和第二槽口, 所述第一槽口和第二槽口分别 包括两侧槽壁和槽底, 所述前直立蜂巢板插入所述第一槽口且与所述 H形型材连接, 所 述后直立蜂巢板插入所述第二槽口且与所述 H形型材连接, 所述前直立蜂巢板与所述第 一槽口的两侧槽壁内侧及槽底保持一定距离,形成第一填充间隙,所述后直立蜂巢板与所 述第二槽口的两侧槽壁内侧及槽底保持一定距离,形成第二填充空间,所述第一填充空间 及所述第二填充空间内设有填充材料层。 12. The full honeycomb panel wind turbine blade according to claim 4, wherein the upright honeycomb panel is connected by a plurality of segments, and the erect honeycomb panel of the previous segment is a front erect honeycomb panel, and The upright honeycomb panel is a rear upright honeycomb panel, the front upright honeycomb panel edge is connected to the rear upright honeycomb panel edge, and the front upright honeycomb panel and the rear upright honeycomb panel are in the same plane, the front The side of the erect honeycomb panel and the rear upright honeycomb panel interconnected Without a seal, a fourth connecting member is disposed between the front upright honeycomb panel and the rear upright honeycomb panel, the fourth connecting member is an H-shaped profile, and the H-shaped profile includes a first slot and a second slot. The first notch and the second notch respectively comprise two side groove walls and a groove bottom, the front upright honeycomb plate is inserted into the first notch and connected with the H-shaped profile, the rear upright honeycomb Inserting the second slot into the second slot and connecting with the H-shaped profile, the front upright honeycomb panel and the inner side of the groove wall of the first slot and the bottom of the slot are kept at a certain distance to form a first filling gap. The rear vertical honeycomb panel and the inner side of the groove wall of the second slot and the bottom of the groove are spaced apart to form a second filling space, and the first filling space and the second filling space are provided with a filling material layer. .
13. 如权利要求 4所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述一对 U形型材 分别与所述第一蜂巢板和第二蜂巢板之间有填充材料层。 13. The full honeycomb panel wind turbine blade according to claim 4, wherein the pair of U-shaped profiles respectively have a filling material layer between the first honeycomb panel and the second honeycomb panel.
14. 如权利要求 5所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述上部连接板覆盖 所述前蜂巢板的上面板和所述后蜂巢板的上面板的拼合接缝朝向所述蜂巢状芯材的一面, 所述下部连接板覆盖所述前蜂巢板的下面板和所述后蜂巢板的下面板的拼合接缝朝向所 述蜂巢状芯材的一面。 14. The full honeycomb panel wind turbine blade according to claim 5, wherein the upper connecting plate covers the joint seam of the upper panel of the front honeycomb panel and the upper panel of the rear honeycomb panel One side of the honeycomb core material, the lower connecting plate covering a split seam of a lower panel of the front honeycomb panel and a lower panel of the rear honeycomb panel facing one side of the honeycomb core material.
15. 如权利要求 5所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述上部连接板有多 块,所述多块上部连接板为长条形并相互以一定间隔连接所述前蜂巢板上面板和所述后蜂 巢板上面板,所述下部连接板有多块,所述多块下部连接板为长条形并相互以一定间隔连 接所述前蜂巢板下面板和所述后蜂巢板下面板。 15. The full honeycomb panel wind turbine blade according to claim 5, wherein the upper connecting plate has a plurality of pieces, and the plurality of upper connecting plates are elongated and connected to each other at a certain interval. a front honeycomb panel and a rear honeycomb panel, the lower connecting panel has a plurality of blocks, the plurality of lower connecting plates are elongated and connected to the front honeycomb panel lower panel at intervals After the honeycomb panel is under the panel.
16. 如权利要求 5所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述上部连接板与所 述前蜂巢板的上面板和所述后蜂巢板的上面板的连接方式为粘接,所述下部连接板与所述 前蜂巢板的下面板和所述后蜂巢板的下面板的连接方式为粘接。 16. The full honeycomb panel wind turbine blade according to claim 5, wherein the upper connecting plate is connected to the upper panel of the front honeycomb panel and the upper panel of the rear honeycomb panel. The connection between the lower connecting plate and the lower panel of the front honeycomb panel and the lower panel of the rear honeycomb panel is bonding.
17. 如权利要求 2、 6或 7所述全蜂巢板风力发电机风轮叶片, 其特征在于, 还包括 V形 连接部件, 所述 V形连接部件包括第一平面、 第二平面和顶角, 所述顶角顶住所述扰流 角内侧,所述第一平面与所述第一蜂巢板贴合并连接,所述第二平面与所述第二蜂巢板贴 合并连接。 17. The full honeycomb panel wind turbine blade according to claim 2, 6 or 7, further comprising a V-shaped connecting member, the V-shaped connecting member comprising a first plane, a second plane and a vertex The top corner is opposite to the inner side of the spoiler angle, the first plane is pasted and connected with the first honeycomb panel, and the second plane is pasted and connected with the second honeycomb panel.
18. 如权利要求 8-11 中任一所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一 槽形型材和所述第二槽形型材为 C形型材, 所述多边形型材为矩形型材。 18. The full honeycomb panel wind turbine blade according to any one of claims 8-11, wherein the first channel profile and the second channel profile are C-shaped profiles, the polygon The profile is a rectangular profile.
19. 如权利要求 8-11 中任一所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一 槽形型材和所述第二槽形型材为 V形型材, 所述多边形型材为菱形型材。 19. The full honeycomb panel wind turbine blade according to any one of claims 8-11, wherein the first channel profile and the second channel profile are V-shaped profiles, the polygon The profile is a diamond profile.
20. 如权利要求 12所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述前直立蜂巢板 与所述 H形型材的连接方式为所述前直立蜂巢板的上下面板与所述 H形型材的第一槽口 的两侧槽壁通过紧固件连接, 所述后直立蜂巢板与所述 H形型材的连接方式为所述后直 立蜂巢板的上下面板与所述 H形型材的第二槽口的两侧槽壁通过紧固件连接。 The full honeycomb panel wind turbine blade according to claim 12, wherein the front vertical honeycomb panel and the H-shaped profile are connected to the upper and lower panels of the front upright honeycomb panel and the The groove walls on both sides of the first notch of the H-shaped profile are connected by fasteners, and the rear upright honeycomb panel is connected to the H-shaped profile by the upper and lower panels of the rear upright honeycomb panel and the H-shaped profile The groove walls on both sides of the second slot are connected by fasteners.
21. 如权利要求 13所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述一对 U形型材 的槽底分别与所述第一蜂巢板和所述第二蜂巢板粘接。 21. The full honeycomb panel wind turbine blade according to claim 13, wherein the groove bottoms of the pair of U-shaped profiles are bonded to the first honeycomb panel and the second honeycomb panel, respectively.
22. 如权利要求 13所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述一对 U形型材 的槽底与所述第一蜂巢板和所述第二蜂巢板之间分别设有沉孔且有紧固件通过该沉孔分 别将所述第一蜂巢板和所述一对 U形型材其中之一以及第二蜂巢板和所述一对 U形型材 其中另一连接在一起。 22. The full honeycomb panel wind turbine blade according to claim 13, wherein a groove bottom of the pair of U-shaped profiles is respectively disposed between the first honeycomb panel and the second honeycomb panel a counterbore having a fastener through which one of the first honeycomb panel and the pair of U-shaped profiles and the second honeycomb panel and the pair of U-shaped profiles are respectively joined together .
23. 如权利要求 14-16中任一所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述上部 连接板伸入所述前蜂巢板 0:面板和所述蜂巢状芯材之间的长度与其伸入所述后蜂巢板上 面板和所述蜂巢状芯材之间的长度相等,所述下部连接板伸入所述前蜂巢板下面板和所述 蜂巢状芯材之间的长度与其伸入所述后蜂巢板下面板和所述蜂巢状芯材之间的长度相等。 23. The full honeycomb panel wind turbine blade according to any one of claims 14-16, wherein the upper connecting plate extends into the front honeycomb panel 0: a panel and the honeycomb core material The length of the space is equal to the length between the rear honeycomb panel and the honeycomb core, and the lower web extends between the lower honeycomb panel and the honeycomb core The length is equal to the length between the lower panel of the honeycomb panel and the honeycomb core.
24. 如权利要求 17所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一蜂巢板和 所述第二蜂巢板与所述 V形连接部件连接处有沉孔, 有紧固件通过所述第一蜂巢板上的 沉孔与所述 V形连接部件的第一平面连接, 有紧固件通过所述第二蜂巢板上的沉孔与所 述 V形连接部件的第二平面连接。 24. The full honeycomb panel wind turbine blade according to claim 17, wherein the first honeycomb panel and the second honeycomb panel have a counterbore at the junction with the V-shaped connecting member, and are tight The firmware is coupled to the first plane of the V-shaped connecting member through a counterbore on the first honeycomb panel, and has a fastener passing through the counterbore on the second honeycomb panel and the V-shaped connecting member Two plane connections.
25. 如权利要求 17所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述第一斜面处的 所述蜂巢状芯材高度随斜面均匀变化, 所述第二斜面处蜂巢状芯材高度随斜面均勾变化。 25. The full honeycomb panel wind turbine blade according to claim 17, wherein: at the first slope The height of the honeycomb core material changes uniformly with the inclined surface, and the height of the honeycomb core material at the second inclined surface changes with the inclined surface.
26. 如权利要求 17所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述蜂巢状新材包 括多个六角形腔体,所述第一斜面处蜂巢状芯材的六角形腔体内和所述第二斜面处蜂巢状 芯材的六角形腔体内有硬质弹性填充材料。 26. The full honeycomb panel wind turbine blade according to claim 17, wherein the honeycomb-shaped new material comprises a plurality of hexagonal cavities, and the hexagonal cavity of the honeycomb core material at the first bevel A hard elastic filling material is formed in the hexagonal cavity of the honeycomb core material in the body and the second inclined surface.
27. 如权利要求 22所述全蜂巢板风力发电机风轮叶片, 其特征在于, 将开设所述沉孔的 蜂巢板称为待连接蜂巢板,将需与所述待连接蜂巢板连接的型材称为连接件,所述带连接 蜂巢板包括待连接上面板、待连接下面板和待连接蜂巢状芯材,所述待连接蜂巢状芯材包 括多个六角形腔室, 所述沉孔包括连接结构, 所述连接结构包括加固层和通孔, 所述加固 层主要由所述待连接蜂巢状芯材和所述六角形腔室内的加固填充材料层组成,所述加固填 充材料层充满所述六角形腔室,所述加固填充材料层为硬质弹性填充材料层,所述加固层 面积小于所述待连接蜂巢板的面积,所述加固层面积大于所述连接件与所述待连接蜂巢板 连接部位的接触面积, 所述通孔穿透所述待连接上面板、待连接下面板及所述加固层, 所 述通孔包括台阶, 所述台阶位于所述待连接蜂巢板不与所述连接件连接的一侧。 27. The full honeycomb panel wind turbine blade according to claim 22, wherein the honeycomb panel in which the counterbore is opened is referred to as a honeycomb panel to be connected, and a profile to be connected to the honeycomb panel to be connected Referring to the connecting member, the belt connecting honeycomb panel comprises an upper panel to be connected, a lower panel to be connected and a honeycomb core to be connected, the honeycomb core to be connected comprises a plurality of hexagonal chambers, and the counterbore comprises a connection structure, the connection structure includes a reinforcement layer and a through hole, the reinforcement layer is mainly composed of the honeycomb core material to be connected and a layer of a reinforcing filler material in the hexagonal cavity, the layer of the reinforcement filling material is filled a hexagonal chamber, the layer of reinforcing filler material is a layer of hard elastic filling material, the area of the reinforcing layer is smaller than the area of the honeycomb panel to be connected, and the area of the reinforcing layer is larger than the connecting member and the to-be-connected The contact area of the connection portion of the honeycomb board, the through hole penetrating the upper panel to be connected, the lower panel to be connected, and the reinforcement layer, the through hole includes a step, and the step is located at the A side member connected to the contact plate not connected to the honeycomb.
28. 如权利要求 24所述全蜂巢板风力发电机风轮叶片, 其特征在于, 将开设所述沉孔的 蜂巢板称为待连接蜂巢板,将需与所述待连接蜂巢板连接的型材称为连接件,所述带连接 蜂巢板包括待连接上面板、待连接下面板和待连接蜂巢状芯材,所述待连接蜂巢状芯材包 括多个六角形腔室, 所述沉孔包括连接结构, 所述连接结构包括加固层和通孔, 所述加固 层主要由所述待连接蜂巢状芯材和所述六角形腔室内的加固填充材料层组成,所述加固填 充材料层充满所述六角形腔室,所述加固填充材料层为硬质弹性填充材料层,所述加固层 面积小于所述待连接蜂巢板的面积,所述加固层面积大于所述连接件与所述待连接蜂巢板 连接部位的接触面积, 所述通孔穿透所述待连接上面板、待连接下面板及所述加固层, 所 述通孔包括台阶, 所述台阶位于所述待连接蜂巢板不与所述连接件连接的一侧。 28. The full honeycomb panel wind turbine blade according to claim 24, wherein the honeycomb panel in which the counterbore is opened is referred to as a honeycomb panel to be connected, and a profile to be connected to the honeycomb panel to be connected Referring to the connecting member, the belt connecting honeycomb panel comprises an upper panel to be connected, a lower panel to be connected and a honeycomb core to be connected, the honeycomb core to be connected comprises a plurality of hexagonal chambers, and the counterbore comprises a connection structure, the connection structure includes a reinforcement layer and a through hole, the reinforcement layer is mainly composed of the honeycomb core material to be connected and a layer of a reinforcing filler material in the hexagonal cavity, the layer of the reinforcement filling material is filled a hexagonal chamber, the layer of reinforcing filler material is a layer of hard elastic filling material, the area of the reinforcing layer is smaller than the area of the honeycomb panel to be connected, and the area of the reinforcing layer is larger than the connecting member and the to-be-connected The contact area of the connection portion of the honeycomb board, the through hole penetrating the upper panel to be connected, the lower panel to be connected, and the reinforcement layer, the through hole includes a step, and the step is located at the A side member connected to the contact plate not connected to the honeycomb.
29. 如权利要求 1-16、 20、 21、 22以及 27中任一所述全蜂巢板风力发电机风轮叶片, 其 特征在于, 所述第一蜂巢板和所述第二蜂巢板为铝蜂巢板。 29. The full honeycomb panel wind turbine blade according to any one of claims 1 to 16, 20, 21, 22 and 27, wherein the first honeycomb panel and the second honeycomb panel are aluminum Honeycomb board.
30. 如权利要求 1-16、 20、 21、 22以及 27中任一所述全蜂巢板风力发电机风轮叶片, 其 特征在于, 所述壳体外侧包覆保护涂层。 30. The full honeycomb panel wind turbine blade according to any one of claims 1 to 16, 20, 21, 22 and 27, The feature is that the outer side of the casing is covered with a protective coating.
31 . 如权利要求 30所述全蜂巢板风力发电机风轮叶片, 其特征在于, 所述保护涂层为环 氧树脂涂层。 31. The full honeycomb panel wind turbine blade according to claim 30, wherein the protective coating is an epoxy resin coating.
PCT/CN2011/001904 2011-07-22 2011-11-14 Wind turbine blade fully made of honeycomb board WO2013013361A1 (en)

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