WO2018188188A1 - Upper cover of unmanned aerial vehicle and unmanned aerial vehicle - Google Patents
Upper cover of unmanned aerial vehicle and unmanned aerial vehicle Download PDFInfo
- Publication number
- WO2018188188A1 WO2018188188A1 PCT/CN2017/088336 CN2017088336W WO2018188188A1 WO 2018188188 A1 WO2018188188 A1 WO 2018188188A1 CN 2017088336 W CN2017088336 W CN 2017088336W WO 2018188188 A1 WO2018188188 A1 WO 2018188188A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- upper cover
- engaging members
- positioning member
- receiving cavity
- hole
- Prior art date
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/70—Constructional aspects of the UAV body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/90—Cooling
- B64U20/96—Cooling using air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
Definitions
- the invention relates to a drone technology, in particular to an upper cover and a drone of a drone.
- Embodiments of the present invention provide an upper cover and a drone of a drone.
- the upper cover of the embodiment of the present invention is mounted on the body of the drone, and the body is provided with a first positioning member and a plurality of first engaging members, and the upper cover comprises:
- the first positioning member is a groove or a through hole
- the second positioning member is a protrusion
- first engaging members a part of the first engaging members is a hook
- the plurality of first engaging members The remaining first engaging member is a card hole or a card slot
- a part of the plurality of second engaging members is a card hole or a card slot
- the plurality of second engaging members are The remaining second engaging members are hooks.
- the body is recessed inwardly to form a receiving cavity
- the front end of the receiving cavity is the front end wall
- the two sides of the receiving cavity are respectively formed with inclined portions
- the plurality of second cards The fitting is higher than the inclined portion
- each of the mounting posts being formed with a blind hole
- the upper cover being mounted on the body and cooperating with a plurality of the blind holes by a fastener to The upper cover is fixed to the body.
- the length of the plurality of mounting posts is greater than the depth of the receiving cavity.
- the body is provided with a first positioning member and a plurality of first engaging members;
- the upper cover according to any one of the preceding embodiments, wherein the upper cover is mounted on the body, the plurality of second engaging members are engaged with the plurality of first engaging members, and the second A positioning member is coupled to the first positioning member.
- the UAV and the upper cover of the embodiment of the present invention are matched with the first positioning member by the second positioning member.
- the plurality of second engaging members are engaged with the plurality of first engaging members to realize the mounting of the upper cover to the body. Since the method is easy to realize positioning and does not require fasteners, when the upper cover is mounted to the body
- the electronic component has less influence on the disassembly and assembly of the upper cover, and is convenient for the upper cover to be mounted on the body and detached from the body.
- FIG. 1 is a perspective view of an upper cover of a drone according to some embodiments of the present invention.
- FIG. 2 is a perspective view of an upper cover of a drone according to some embodiments of the present invention.
- Figure 5 is a plan view of the upper cover of the drone of some embodiments of the present invention.
- FIG. 6 is a schematic plan view of an upper cover of a drone according to some embodiments of the present invention.
- the first feature "on” or “under” the second feature may be a direct contact of the first and second features, or the first and second features may be indirectly through an intermediate medium, unless otherwise explicitly stated and defined. contact.
- the first feature "above”, “above” and “above” the second feature may be that the first feature is directly above or above the second feature, or merely that the first feature level is higher than the second feature.
- the first feature “below”, “below” and “below” the second feature may be the first feature Signed directly below or obliquely below the second feature, or simply indicates that the first feature level is less than the second feature.
- the upper cover 100 of the drone of the embodiment of the present invention is mounted on the body 200 of the drone, and the body 200 is provided with a first positioning member 202 and a plurality of first engaging members 204.
- the upper cover 100 includes a body 10, a second positioning member 20, and a plurality of second engaging members 30.
- the body 10 is formed with a front end wall 12 at one end of the nose of the drone.
- the second positioning member 20 is disposed on the front end wall 12, and the second positioning member 20 is engaged with the first positioning member 202.
- the plurality of second engaging members 30 are disposed on the body 10, and the plurality of second engaging members 30 are engaged with the plurality of first engaging members 204.
- the UAV and the upper cover 100 of the embodiment of the present invention cooperate with the first positioning member 202 through the second positioning member 20, and the plurality of second engaging members 30 are engaged with the plurality of first engaging members 204 to realize the upper cover.
- 100 is mounted on the body 200. Since the method is easy to realize positioning and no fastener is needed, when the upper cover 100 is mounted on the body 200, the electronic component has less influence on the disassembly and assembly of the upper cover 100, and the upper cover 100 is facilitated. It is mounted to and detached from the body 200.
- the upper cover 100 includes a body 10 , a second positioning member 20 , a plurality of second engaging members 30 , and a plurality of mounting posts 40 .
- the front end wall 12 of the body 10 is formed at one end of the nose of the drone 100, and the front end The wall 12 extends from the bottom surface 13 downward (in view of the flight of the drone), and the inclined portion 17 is formed obliquely downward from the intermediate position of the body 10 and extends outward.
- the inclined portion 17 is located on opposite sides of the receiving cavity 15, and the front end wall 12 is connected to the inclined portion 17 on the opposite sides of the receiving cavity 15, and the front end wall 12 and the inclined portion 17 are both part of the receiving cavity 15.
- each inclined portion 17 is recessed toward the top surface 11 to form a notch 172, and the center of the notch 172 is offset from the center of the inclined portion 17.
- each of the inclined portions 17 is formed with a heat dissipation hole 19, and the heat dissipation hole 19 communicates with the outside of the receiving cavity 15 and the inclined portion 17, and the heat dissipation hole 19 is opened in the middle of the inclined portion 17.
- the heat dissipation holes 19 are formed at an intermediate position of the inclined portion 17 along the longitudinal direction of the inclined portion 17).
- the body 10 is formed on the opposite sides of the receiving cavity 15 with at least two heat dissipation holes 19, and the center lines of the two heat dissipation holes 19 on the opposite two inclined portions 17 are coaxial.
- the heat dissipation hole 19 includes a first inner side surface 192 and a second inner side surface 194 obliquely connected to the first inner side surface 192.
- the first inner side surface 192 is parallel to the flight direction of the drone, and the second inner side surface 194 is located on the first inner side surface 192.
- the cross section of the heat dissipation hole 19 may be a triangle, a parallelogram, a pentagon, a hexagon, or the like.
- the second positioning member 20 is located on the front end wall 12, the number of the second positioning members 20 is the same as the number of the first positioning members 202, and each of the second positioning members 20 and the corresponding first positioning member 202 cooperation.
- the second positioning member 20 can be a bump, Groove or through hole. Specifically, when the first positioning member 202 is a bump, the second positioning member 20 may be a groove or a through hole; when the first positioning member 202 is a groove or a through hole, the second positioning member 20 may be a convex block. .
- the second engaging member 30 extends from the bottom surface 13 in a direction away from the top surface 11 , the number of the second engaging members 30 is the same as the number of the first engaging members 204 , and the plurality of second engaging members 30 are distributed on the body 10 . On the opposite sides, specifically, a plurality of second engaging members 30 are distributed on both sides of the inclined portion 17. The plurality of second engaging members 30 are higher than the inclined portion 17 . Since the inclined portion 17 is a part of the receiving cavity 15 , the second engaging member 30 is higher than the inclined portion 17 . The bottom of the receiving cavity 15 extends outward and exposes the receiving cavity 15.
- the second engaging member 30 can be a hook, a card hole or a card slot; or a part of the second engaging member 30 can be a card hole and/or a card slot, and the rest is a hook, that is, the second
- the engaging member 30 includes both a hook and a card hole or a card slot.
- the second engaging member 30 can be a card hole or a card slot; when the first engaging member 204 is a card hole or a card slot, the second engaging member 30 When the part of the first engaging member 204 is a hook and the rest is a card hole and a card slot, correspondingly, a part of the second engaging member 30 may be a card hole or a card slot, and the rest may be a card hole or a card slot. Some are hooks.
- the edge of the inclined portion 17 is recessed toward the top surface 11 to form a notch 172, and the center of the notch 172 is offset from the center of the inclined portion 17.
- the shape of the upper cover 100 does not match the shape of the body 200 so that the upper cover 100 cannot be attached to the body 200. In this way, it is convenient to quickly determine the correct mounting direction of the upper cover 100, and the upper cover 100 can be quickly mounted to the body 20, that is, the notch 172 is formed on the upper cover 100 to have a foolproof effect.
- the electronic component is disposed at an intermediate position of the body 200, which causes the intermediate position of the body 200 to be more difficult to dissipate heat and has a higher temperature, and belongs to a heat concentration area, and the heat dissipation hole 19 is opened at an intermediate position of the inclined portion 17, thus improving the absence of The heat dissipation effect of the man-machine.
- the heat dissipation holes 19 on both sides are used as the air outlets to discharge the hot airflow inside the drone, thereby taking away heat, which is beneficial to the internal electronic components of the drone. Cooling.
- the angle between the first inner sidewall 192 and the second inner sidewall 194 of the heat dissipation hole 19 is an obtuse angle.
- the second engaging member 30 is higher than the inclined portion 17, so that the second engaging member 30 is first connected to the first engaging member 204 first, and then the inclined portion 17 is engaged with the body 200, thereby facilitating the second
- the engaging member 30 is engaged with the first engaging member 204, and the electronic component that the inclined portion 17 and the body 200 are sandwiched on the body 200 can be avoided.
- the fastener penetrates through the mounting hole 206 and cooperates with the plurality of blind holes 42 to strengthen the upper cover 100 to the body 200, thereby preventing the upper cover 100 from falling off the body 200.
- the upper cover 100 does not need to open a hole penetrating through the top surface 11 and the bottom surface 13 of the body 10, so that the upper cover 100 is integrally formed. And has a good waterproof effect.
- the fuselage 200 is located below the upper cover 100, and the fastener is mounted from the bottom up (the direction of the fuselage 200 to the upper cover 100), and after installation, the drone In normal flight, the fasteners are located below the fuselage 200, and water droplets are difficult to enter.
- the mounting post 40 can support the upper cover 100; on the other hand, the upper cover 100 is prevented from squeezing the electronic components located on the fuselage 200 to cause the electronic The component is damaged while avoiding deformation of the upper cover 100 and affecting the use of the upper cover 100.
- the number of the notches 172 formed by each of the inclined portions 17 in the above embodiment may be two, three, four or any number, and multiple notches
- the center of the 172 is asymmetrical with the plane passing through the centers of the two inclined portions 17, so that the opening 172 is formed in the upper cover 100 to have a foolproof effect.
- the cooling air enters the cavity formed by the fuselage 200 and the upper cover 100 from the heat dissipation hole 19 to be located in the cavity.
- the extending direction of the outer slanting portion 17 of the vent hole 19 in the above embodiment to the receiving cavity 15 can be inclined toward the nose of the drone.
- the external cooling air is easily entered into the inside of the housing chamber 19 by the heat dissipation holes 19.
- the distribution of the plurality of second engaging members 30 in the above embodiment is not limited to being located on opposite sides of the body 10, and the plurality of second engaging members 30 are distributed on the body.
- the projection of the upper cover 100 in the direction of the body 200 in the above embodiment can completely cover the cross section of the body 200 or the body 200 connected to the upper cover 100, so that rainwater can be prevented from flowing along the upper cover 100.
- the top surface 11 flows into the interior of the body 200.
- a plurality of mounting posts 40 may not be disposed in the above embodiment, and the upper cover 100 may be fixed by engaging the second engaging component 30 with the first engaging component 204 .
- the upper cover 100 can also be fixed to the body 200 by gluing, welding, or the like.
- the end of the fuselage 200 near the head is provided with a limit protrusion 208
- the front end wall 12 of the upper cover 100 is provided with 208 of the limit protrusion.
- the limiting slot 122 is provided.
- the limiting protrusion 208 is located at an intermediate position of the body 200 near the head, and the limiting groove 122 is opened at an intermediate position of the front end wall 12. In the direction away from the bottom surface 13, the width of the limiting groove 122 is gradually increased.
- the limiting slot 122 is facilitated to engage with the limiting protrusion 208.
- the limiting slot 122 is engaged with the limiting protrusion 208 to facilitate the cooperation of the second positioning component 20 with the first positioning component 202 on the body 200.
- the embodiments of the present invention may satisfy only one of the foregoing embodiments or the foregoing multiple embodiments, that is, the embodiments in which one or more of the foregoing embodiments are combined also belong to the protection scope of the embodiments of the present invention. .
- first and second are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated.
- features defining “first” or “second” may include at least one of the features, either explicitly or implicitly.
- a plurality means at least two, for example two, three, unless specifically defined otherwise.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Casings For Electric Apparatus (AREA)
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
Description
本发明涉及无人机技术,具体涉及一种无人机的上盖及无人机。The invention relates to a drone technology, in particular to an upper cover and a drone of a drone.
无人机包括机身和上盖,机身内设置有电子元件,上盖安装在机身上并覆盖电子元件。上盖通常是利用螺钉等紧固件而锁紧在机身上,在紧固件锁紧上盖与机身和松开上盖与机身时容易受到电子元件的干扰,从而导致上盖安装及拆卸困难。The drone includes a body and an upper cover, and the body is provided with electronic components, and the upper cover is mounted on the body and covers the electronic components. The upper cover is usually locked to the body by fasteners such as screws. When the fastener locks the upper cover and the body and loosens the upper cover and the body, it is easily interfered by electronic components, thereby causing the upper cover to be installed. And difficult to disassemble.
发明内容Summary of the invention
本发明的实施方式提供了一种无人机的上盖及无人机。Embodiments of the present invention provide an upper cover and a drone of a drone.
本发明实施方式的上盖,安装在所述无人机的机身上,所述机身设置有第一定位件及多个第一卡合件,所述上盖包括:The upper cover of the embodiment of the present invention is mounted on the body of the drone, and the body is provided with a first positioning member and a plurality of first engaging members, and the upper cover comprises:
本体,所述本体在所述无人机的机头的一端形成有前端壁;a body having a front end wall formed at one end of the nose of the drone;
设置在所述前端壁上的第二定位件,所述第二定位件与所述第一定位件配合;及a second positioning member disposed on the front end wall, the second positioning member mating with the first positioning member; and
设置在所述本体上的多个第二卡合件,所述多个第二卡合件与所述多个第一卡合件配合,所述上盖安装在所述机身上时,所述多个第二卡合件与所述多个第一卡合件卡合,且所述第二定位件与所述第一定位件结合。a plurality of second engaging members disposed on the body, the plurality of second engaging members are engaged with the plurality of first engaging members, and when the upper cover is mounted on the body The plurality of second engaging members are engaged with the plurality of first engaging members, and the second positioning members are coupled with the first positioning members.
在某些实施方式中,所述第一定位件为凸块,所述第二定位件为凹槽或通孔;或者In some embodiments, the first positioning member is a bump, and the second positioning member is a groove or a through hole; or
所述第一定位件为凹槽或通孔,所述第二定位件为凸块。The first positioning member is a groove or a through hole, and the second positioning member is a protrusion.
在某些实施方式中,所述多个第一卡合件均为卡勾,所述多个第二卡合件均为卡孔或卡槽;或In some embodiments, the plurality of first engaging members are hooks, and the plurality of second engaging members are all card holes or card slots; or
所述多个第一卡合件均为卡孔或卡槽,所述多个第二卡合件均为卡勾;或The plurality of first engaging members are all card holes or card slots, and the plurality of second engaging members are hooks; or
所述多个第一卡合件中的部分第一卡合件为卡勾,所述多个第一卡合件 中的其余第一卡合件为卡孔或卡槽,所述多个第二卡合件中的部分第二卡合件为卡孔或卡槽,所述多个第二卡合件中的其余第二卡合件为卡勾。a part of the first engaging members is a hook, and the plurality of first engaging members The remaining first engaging member is a card hole or a card slot, and a part of the plurality of second engaging members is a card hole or a card slot, and the plurality of second engaging members are The remaining second engaging members are hooks.
在某些实施方式中,所述本体包括相背的顶面及底面,所述多个第二卡合件自所述底面朝向背离所述顶面的方向延伸,所述多个第二卡合件分布于所述本体的相对两侧。In some embodiments, the body includes opposite top and bottom surfaces, and the plurality of second engaging members extend from the bottom surface toward a direction away from the top surface, the plurality of second engaging portions The pieces are distributed on opposite sides of the body.
在某些实施方式中,所述本体向内凹陷形成收容腔,所述收容腔的前端为所述前端壁,所述收容腔的两侧边缘分别形成有倾斜部,所述多个第二卡合件高于所述倾斜部。In some embodiments, the body is recessed inwardly to form a receiving cavity, the front end of the receiving cavity is the front end wall, and the two sides of the receiving cavity are respectively formed with inclined portions, the plurality of second cards The fitting is higher than the inclined portion.
在某些实施方式中,所述本体向内凹陷形成收容腔,所述收容腔的前端为所述前端壁,所述收容腔的两侧边缘分别形成有倾斜部,每个倾斜部的边缘向所述顶面的方向凹陷以形成缺口,所述缺口的中心与倾斜部的中心错开。In some embodiments, the body is recessed inwardly to form a receiving cavity, the front end of the receiving cavity is the front end wall, and the two sides of the receiving cavity are respectively formed with inclined portions, and the edges of each inclined portion are oriented The direction of the top surface is recessed to form a notch, the center of the notch being offset from the center of the inclined portion.
在某些实施方式中,所述本体向内凹陷形成收容腔,所述收容腔的前端为所述前端壁,所述收容腔的两侧边缘分别形成有倾斜部,所述倾斜部上形成有将所述收容腔和所述本体的顶面外部相连通的散热孔。In some embodiments, the body is recessed inwardly to form a receiving cavity, the front end of the receiving cavity is the front end wall, and the two sides of the receiving cavity are respectively formed with inclined portions, and the inclined portion is formed with a heat dissipation hole that communicates the receiving cavity with the outside of the top surface of the body.
在某些实施方式中,沿着所述倾斜部的长度方向,所述散热孔开设在所述倾斜部的中间位置。In some embodiments, the heat dissipation hole is opened at an intermediate position of the inclined portion along a length direction of the inclined portion.
在某些实施方式中,所述散热孔包括第一内侧面及与所述第一内侧面倾斜连接的第二内侧面,所述第一内侧面平行于所述无人机的飞行方向,所述第二内侧面位于所述第一内侧面的远离所述前端壁的一侧,所述第一内侧壁与所述第二内侧壁之间的夹角为钝角。In some embodiments, the heat dissipation hole includes a first inner side surface and a second inner side surface obliquely connected to the first inner side surface, the first inner side surface being parallel to a flight direction of the drone, The second inner side surface is located on a side of the first inner side surface away from the front end wall, and an angle between the first inner side wall and the second inner side wall is an obtuse angle.
在某些实施方式中,所述上盖还包括:In some embodiments, the upper cover further includes:
自所述底面延伸的多个安装柱,每个所述安装柱形成有盲孔,所述上盖安装在所述机身上并通过紧固件与多个所述盲孔配合以将所述上盖固定在所述机身上。a plurality of mounting posts extending from the bottom surface, each of the mounting posts being formed with a blind hole, the upper cover being mounted on the body and cooperating with a plurality of the blind holes by a fastener to The upper cover is fixed to the body.
在某些实施方式中,所述多个安装柱的长度大于所述收容腔的深度。In some embodiments, the length of the plurality of mounting posts is greater than the depth of the receiving cavity.
本发明实施方式的无人机包括:The drone of the embodiment of the present invention includes:
机身,所述机身设置有第一定位件及多个第一卡合件;和a fuselage, the body is provided with a first positioning member and a plurality of first engaging members; and
上述任意一项实施方式所述的上盖,所述上盖安装在所述机身上,所述多个第二卡合件与所述多个第一卡合件卡合,所述第二定位件与所述第一定位件结合。The upper cover according to any one of the preceding embodiments, wherein the upper cover is mounted on the body, the plurality of second engaging members are engaged with the plurality of first engaging members, and the second A positioning member is coupled to the first positioning member.
本发明实施方式的无人机和上盖,通过第二定位件与第一定位件配合, 多个第二卡合件与多个第一卡合件卡合实现将上盖安装到机身上,由于这种方法容易实现定位且不需要紧固件,因而上盖安装到机身上时电子元件对上盖的拆装影响较小,便于上盖安装到机身上及从机身上拆卸下来。The UAV and the upper cover of the embodiment of the present invention are matched with the first positioning member by the second positioning member. The plurality of second engaging members are engaged with the plurality of first engaging members to realize the mounting of the upper cover to the body. Since the method is easy to realize positioning and does not require fasteners, when the upper cover is mounted to the body The electronic component has less influence on the disassembly and assembly of the upper cover, and is convenient for the upper cover to be mounted on the body and detached from the body.
本发明的实施方式的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本发明的实施方式的实践了解到。The additional aspects and advantages of the embodiments of the present invention will be set forth in part in the description which follows.
本发明的上述和/或附加的方面和优点从结合下面附图对实施方式的描述中将变得明显和容易理解,其中:The above and/or additional aspects and advantages of the present invention will become apparent and readily understood from
图1是本发明某些实施方式的无人机的上盖的立体示意图;1 is a perspective view of an upper cover of a drone according to some embodiments of the present invention;
图2是本发明某些实施方式的无人机的上盖的立体示意图;2 is a perspective view of an upper cover of a drone according to some embodiments of the present invention;
图3是本发明某些实施方式的无人机的机身的立体示意图;3 is a perspective view of a fuselage of a drone according to some embodiments of the present invention;
图4是本发明某些实施方式的无人机的上盖的平面示意图;4 is a schematic plan view of an upper cover of a drone according to some embodiments of the present invention;
图5是本发明某些实施方式的无人机的上盖的平面示意图;和Figure 5 is a plan view of the upper cover of the drone of some embodiments of the present invention;
图6是本发明某些实施方式的无人机的上盖的平面示意图。6 is a schematic plan view of an upper cover of a drone according to some embodiments of the present invention.
主要元件符号说明:The main component symbol description:
机身200、第一定位件202、第一卡合件204、安装孔206、限位凸起208、上盖100、本体10、前端壁12、限位槽122、顶面11、底面13、收容腔15、倾斜部17、缺口172、散热孔19、第一内侧壁192、第二内侧壁194、第二定位件20、第二卡合件30、安装柱40、盲孔42。The body 200, the
以下结合附图对本发明的实施方式作进一步说明。附图中相同或类似的标号自始至终表示相同或类似的元件或具有相同或类似功能的元件。Embodiments of the present invention will be further described below in conjunction with the accompanying drawings. The same or similar reference numerals in the drawings denote the same or similar elements or elements having the same or similar functions.
另外,下面结合附图描述的本发明的实施方式是示例性的,仅用于解释本发明的实施方式,而不能理解为对本发明的限制。In addition, the embodiments of the present invention described below in conjunction with the accompanying drawings are merely illustrative of the embodiments of the invention, and are not to be construed as limiting.
在本发明中,除非另有明确的规定和限定,第一特征在第二特征“上”或“下”可以是第一和第二特征直接接触,或第一和第二特征通过中间媒介间接接触。而且,第一特征在第二特征“之上”、“上方”和“上面”可是第一特征在第二特征正上方或斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”可以是第一特 征在第二特征正下方或斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, the first feature "on" or "under" the second feature may be a direct contact of the first and second features, or the first and second features may be indirectly through an intermediate medium, unless otherwise explicitly stated and defined. contact. Moreover, the first feature "above", "above" and "above" the second feature may be that the first feature is directly above or above the second feature, or merely that the first feature level is higher than the second feature. The first feature "below", "below" and "below" the second feature may be the first feature Signed directly below or obliquely below the second feature, or simply indicates that the first feature level is less than the second feature.
在本说明书的描述中,参考术语“某些实施方式”、“一个实施方式”、“一些实施方式”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中,对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外,在不相互矛盾的情况下,本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。In the description of the present specification, the description with reference to the terms "some embodiments", "one embodiment", "some embodiments", "example", "specific example", or "some examples", etc. Particular features, structures, materials or features described in the examples or examples are included in at least one embodiment or example of the invention. In the present specification, the schematic representation of the above terms is not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in a suitable manner in any one or more embodiments or examples. In addition, various embodiments or examples described in the specification, as well as features of various embodiments or examples, may be combined and combined.
尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。Although the embodiments of the present invention have been shown and described, it is understood that the above-described embodiments are illustrative and are not to be construed as limiting the scope of the invention. The embodiments are subject to variations, modifications, substitutions and variations.
请参阅图1-3,本发明实施方式的无人机的上盖100,安装在无人机的机身200上,机身200设置有第一定位件202及多个第一卡合件204,上盖100包括本体10、第二定位件20和多个第二卡合件30。本体10在无人机的机头的一端形成有前端壁12。第二定位件20设置在前端壁12上,第二定位件20与第一定位件202配合。多个第二卡合件30设置在本体10上,多个第二卡合件30与多个第一卡合件204配合,上盖100安装在机身200上时,多个第二卡合件30与多个第一卡合件204卡合,且第二定位件20与第一定位件202结合。1-3, the
本发明实施方式的无人机和上盖100,通过第二定位件20与第一定位件202配合,多个第二卡合件30与多个第一卡合件204卡合实现将上盖100安装到机身200上,由于这种方法容易实现定位且不需要紧固件,因而上盖100安装到机身200上时电子元件对上盖100的拆装影响较小,便于上盖100安装到机身200上及从机身200上拆卸下来。The UAV and the
请参阅图1及图3,本发明实施方式的无人机包括机身200和上盖100。上盖100安装在机身200上。Referring to FIGS. 1 and 3 , the drone of the embodiment of the present invention includes a body 200 and an
请参阅图3,机身200设置有第一定位件202、多个第一卡合件204和多个安装孔206。第一定位件202可以为凸块、凹槽或通孔,第一定位件202的数量可以为一个、两个或任意多个。第一卡合件204可以为卡勾、卡孔或卡槽;或者,第一卡合件204中的一部分为卡勾,其余部分为卡孔和/或卡槽,
也就是说,第一卡合件204既包括卡勾,又包括卡孔或卡槽。第一卡合件204的数量可以为两个、三个、四个或任意多个。安装孔206贯穿机身200或机身200上的一个元件。安装孔206的数量可以为两个、三个、四个或任意多个。Referring to FIG. 3 , the body 200 is provided with a
请参阅图1-2,上盖100包括本体10、第二定位件20、多个第二卡合件30和多个安装柱40。Referring to FIGS. 1-2 , the
本体10包括相背的顶面11和底面13,底面13位于本体10靠近机身200的一侧。本体10向内凹陷形成收容腔15,也可以理解为,顶面11和底面13自边缘位置朝本体10的中间位置逐渐向无人机的顶部凸出形成收容腔15。本体10包括位于收容腔15的前端的前端壁12和位于收容腔15的两侧边缘的倾斜部17,具体地,本体10的前端壁12形成在无人机100的机头的一端,且前端壁12自底面13向下(以无人机飞行的视角来看)延伸形成,倾斜部17自本体10的中间位置倾斜向下并向外延伸形成。倾斜部17位于收容腔15相对的两侧,前端壁12与位于收容腔15相对两侧的倾斜部17均连接,前端壁12和倾斜部17均为围成收容腔15的一部分。The
每个倾斜部17的边缘向顶面11的方向凹陷以形成缺口172,缺口172的中心与倾斜部17的中心错开。The edge of each
请参阅图1及图4,每个倾斜部17上均形成有散热孔19,散热孔19将收容腔15和倾斜部17的外部相连通,散热孔19开设在倾斜部17的中间位置(也可以理解为,散热孔19开设在倾斜部17沿倾斜部17的长度方向的中间位置上)。可以理解,本体10位于收容腔15相对的两侧上形成有至少两个散热孔19,位于相对两个倾斜部17上的两个散热孔19的中心线同轴。散热孔19包括第一内侧面192及与第一内侧面192倾斜连接的第二内侧面194,第一内侧面192平行于无人机的飞行方向,第二内侧面194位于第一内侧面192的远离前端壁12的一侧,第一内侧壁192与第二内侧壁194之间的夹角为钝角。具体地,散热孔19的截面可以呈三角形、平行四边形、五边形、六边形等。Referring to FIG. 1 and FIG. 4, each of the
请参阅图5-6,第二定位件20位于前端壁12上,第二定位件20的数量与第一定位件202的数量一致,且每个第二定位件20与对应的第一定位件202配合。当上盖100安装到机身200上时,第一定位件202与第二定位件20结合并用于将上盖100定位在机身200上。第二定位件20可以为凸块、
凹槽或通孔。具体地,当第一定位件202为凸块时,第二定位件20可以为凹槽或通孔;当第一定位件202为凹槽或通孔时,第二定位件20可以为凸块。Referring to FIGS. 5-6, the
第二卡合件30自底面13朝向背离顶面11的方向延伸,第二卡合件30的数量与第一卡合件204的数量一致,多个第二卡合件30分布于本体10的相对两侧,具体地,多个第二卡合件30分布于靠近倾斜部17的两侧。多个第二卡合件30高于倾斜部17,由于倾斜部17为围成收容腔15的一部分,因而第二卡合件30高于倾斜部17可以理解为:第二卡合件30自收容腔15的底部向外延伸并露出收容腔15。The second engaging
第二卡合件30可以为卡勾、卡孔或卡槽;或者,第二卡合件30中的一部分可以为卡孔和/或卡槽,其余部分为卡勾,也就是说,第二卡合件30既包括卡勾又包括卡孔或卡槽。具体地,当第一卡合件204为卡勾时,第二卡合件30可以为卡孔或卡槽;当第一卡合件204为卡孔或卡槽时,第二卡合件30可以为卡勾;当第一卡合件204中的一部分为卡勾,其余部分为卡孔和卡槽时,对应地,第二卡合件30中的一部分可以为卡孔或卡槽,其余部分为卡勾。The second engaging
请参阅图1及图2,安装柱40自底面13朝机身200的方向延伸形成,每个安装柱40的中间位置均形成有盲孔42,上盖100安装在机身200后通过紧固件(图未示)贯穿安装孔206并与多个盲孔42配合以将上盖100固定在机身200上。具体地,安装柱40的数量可以为两个、三个、四个、五个、六个或任意多个,多个安装柱20设置在靠近本体10边缘的位置并环绕收容腔15,以防止上盖100固定在机身200上后本体100的边缘翘起的情况发生(也就是说,避免上盖100与机身200产生间隙)。紧固件可以为螺钉,此时盲孔42为螺纹孔,紧固件与盲孔42螺合以将上盖100固定在机身200上。安装柱40的长度L大于收容腔15的深度D,也就是说,安装柱40从收容腔15露出并高于倾斜部17。Referring to FIG. 1 and FIG. 2 , the mounting
本发明实施方式的上盖100首先通过第二定位件20与第一定位件202配合,多个第二卡合件30与多个第一卡合件204卡合实现将上盖100安装到机身200上;再通过紧固件贯穿安装孔206并与多个盲孔42配合以实现将上盖100加强固定在机身200上。The
本发明实施方式的无人机和上盖100,通过第二定位件20与第一定位件202配合,多个第二卡合件30与多个第一卡合件204卡合实现将上盖100安
装到机身200上,由于这种方法容易实现定位且不需要紧固件,因而上盖100安装到机身200上时电子元件对上盖100的拆装影响较小,便于上盖100安装到机身200上及从机身200上拆卸下来。The UAV and the
本发明实施方式的无人机和上盖100还具有以下有益效果:The drone and the
第一,倾斜部17自本体10的中间位置倾斜向下并向外延伸形成,滴落到顶面11上的雨水容易自上往下顺着倾斜部17流下而远离无人机。First, the
第二,倾斜部17的边缘向顶面11的方向凹陷以形成缺口172,且缺口172的中心与倾斜部17的中心错开。当上盖100的安装方向不正确时(例如,机头与机尾方向弄错),上盖100的形状与机身200的形状不匹配使上盖100不能安装到机身200上。如此,便于快速地确定上盖100正确的安装方向,并能够快速地将上盖100安装到机身20上,也就是说,在上盖100上开设缺口172具有防呆的作用。Second, the edge of the
第三,上盖100开设散热孔19,无人机在飞行时,根据无人机内部的气流流向设计,冷却风可以自散热孔19进入机身200与上盖100共同形成的腔体内从而对位于腔体内的电子元件散热或者冷却风可以自无人机的其他散热孔进入机身200与上盖100共同形成的腔体内并自散热孔19排出进而为电子元件散热。通常,电子元件多设置在机身200的中间位置,导致机身200中间位置较难散热且温度较高,属于热量集中区域,散热孔19开设在倾斜部17的中间位置,如此,提升了无人机的散热效果。在本实施方式中,由于无人机内部的气流流向设计,两侧的散热孔19是作为出风口用作排出无人机内部的热气流,从而带走热量,利于无人机内部电子元件的散热。Thirdly, the
第四,散热孔19的第一内侧壁192与第二内侧壁194之间的夹角为钝角,在无人机向前飞行时,带有热量的风在散热孔19钝角的引导下容易从散热孔19中排出,从而能够更进一步提升无人机的散热效果。Fourth, the angle between the first
第五,第二卡合件30高于倾斜部17,如此,第二卡合件30首先与第一卡合件204先连接,然后倾斜部17才与机身200配合,进而便于实现第二卡合件30与第一卡合件204卡合,能够避免倾斜部17与机身200夹到机身200上的电子元件。Fifthly, the second engaging
第六,紧固件贯穿安装孔206并与多个盲孔42配合以实现将上盖100加强固定在机身200上,避免了上盖100从机身200上脱落的情况发生。上盖100不必开设贯穿本体10的顶面11和底面13的孔,便于上盖100一体成型
并具有较好的防水效果。而且,以无人机正常飞行的视角来观察,机身200位于上盖100的下方,紧固件是从下往上安装(机身200至上盖100的方向),安装好后,无人机正常飞行时,紧固件都处于机身200的下方,水滴很难进入。另外,由于安装柱40的长度L大于收容腔15的深度D,一方面,安装柱40能够支撑上盖100;另一方面,避免上盖100挤压位于机身200上的电子元件而导致电子元件损害的同时避免上盖100发生变形而影响上盖100使用。Sixth, the fastener penetrates through the mounting
请参阅图1及图2,在某些实施方式中,上述实施方式中的每个倾斜部17形成的缺口172的数量可以为两个、三个、四个或任意多个,且多个缺口172的中心与穿过两个倾斜部17中心的平面不对称,如此在上盖100上开设缺口172具有防呆的作用。Referring to FIG. 1 and FIG. 2 , in some embodiments, the number of the
请参阅图1及图2,在某些实施方式中,若根据无人机内部的气流流向设计,冷却风是自散热孔19进入机身200与上盖100共同形成的腔体内从而对位于腔体内的电子元件散热时,上述实施方式中的散热孔19的自倾斜部17的外部穿透倾斜部17向收容腔15延伸的延伸方向可朝无人机的机头方向倾斜,此时,当无人机朝机头的正向飞行时,外部冷却空气容易由散热孔19进入收容腔19的内部。Referring to FIG. 1 and FIG. 2, in some embodiments, according to the airflow direction design inside the drone, the cooling air enters the cavity formed by the fuselage 200 and the
请参阅图1-3,在某些实施方式中,上述实施方式中的多个第二卡合件30的分布不限于位于本体10的相对两侧,多个第二卡合件30分布于本体10的三侧、或本体30的四周,具体地,多个第二卡合件30分布的位置越多,多个第二卡合件30与多个第一卡合件204卡合时越难从机身200上脱落出来。1-3, in some embodiments, the distribution of the plurality of second
在某些实施方式中,上述实施方式中的上盖100沿机身200方向的投影能够完全覆盖机身200或机身200与上盖100连接的截面,如此,能够避免雨水沿着上盖100的顶面11流入机身200内部。In some embodiments, the projection of the
请参阅图1及图2,在某些实施方式中,上述实施方式中可以不设置多个安装柱40,上盖100可以通过第二卡合件30与第一卡合件204卡合实现固定在机身200上。当然,上盖100也可以通过胶合、焊接等方式固定在机身200上。Referring to FIG. 1 and FIG. 2 , in some embodiments, a plurality of mounting
请参阅图1-3,在某些实施方式中,上述实施方式中机身200靠近机头的一端设置有限位凸起208,上盖100的前端壁12开设有与限位凸起208匹
配的限位槽122。具体地,限位凸起208位于机身200靠近机头的中间位置,限位槽122开设在前端壁12的中间位置。在远离底面13的方向上,限位槽122的宽度逐渐增加。如此,上盖100安装到机身200上时,便于限位槽122与限位凸起208卡合。同时,限位槽122与限位凸起208卡合,便于第二定位件20与机身200上的第一定位件202配合。Referring to FIG. 1-3, in some embodiments, the end of the fuselage 200 near the head is provided with a
具体地,本发明实施方式可以只满足上述其中一个实施方式或同时满足上述多个实施方式,也就是说,上述一个或多个实施方式组合而成的实施方式也属于本发明实施方式的保护范围。Specifically, the embodiments of the present invention may satisfy only one of the foregoing embodiments or the foregoing multiple embodiments, that is, the embodiments in which one or more of the foregoing embodiments are combined also belong to the protection scope of the embodiments of the present invention. .
在本说明书的描述中,参考术语“某些实施方式”、“一个实施方式”、“一些实施方式”、“示意性实施方式”、“示例”、“具体示例”、或“一些示例”的描述意指结合所述实施方式或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施方式或示例中。在本说明书中,对上述术语的示意性表述不一定指的是相同的实施方式或示例。而且,描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施方式或示例中以合适的方式结合。In the description of the present specification, reference is made to the terms "some embodiments", "one embodiment", "some embodiments", "illustrative embodiments", "example", "specific examples", or "some examples" The description means that specific features, structures, materials or characteristics described in connection with the embodiments or examples are included in at least one embodiment or example of the invention. In the present specification, the schematic representation of the above terms does not necessarily mean the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in a suitable manner in any one or more embodiments or examples.
此外,术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个所述特征。在本发明的描述中,“多个”的含义是至少两个,例如两个,三个,除非另有明确具体的限定。Moreover, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" or "second" may include at least one of the features, either explicitly or implicitly. In the description of the present invention, "a plurality" means at least two, for example two, three, unless specifically defined otherwise.
尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型,本发明的范围由权利要求及其等同物限定。 Although the embodiments of the present invention have been shown and described, it is understood that the above-described embodiments are illustrative and are not to be construed as limiting the scope of the invention. The scope of the invention is defined by the claims and their equivalents.
Claims (12)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201780060239.XA CN109789919A (en) | 2017-04-10 | 2017-06-14 | The upper cover and unmanned plane of unmanned plane |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720370042.3 | 2017-04-10 | ||
CN201720370042.3U CN206926801U (en) | 2017-04-10 | 2017-04-10 | The upper lid and unmanned plane of unmanned plane |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2018188188A1 true WO2018188188A1 (en) | 2018-10-18 |
Family
ID=61350440
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2017/088336 WO2018188188A1 (en) | 2017-04-10 | 2017-06-14 | Upper cover of unmanned aerial vehicle and unmanned aerial vehicle |
Country Status (2)
Country | Link |
---|---|
CN (2) | CN206926801U (en) |
WO (1) | WO2018188188A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN206926801U (en) * | 2017-04-10 | 2018-01-26 | 深圳市大疆创新科技有限公司 | The upper lid and unmanned plane of unmanned plane |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7059565B2 (en) * | 2003-10-21 | 2006-06-13 | The Boeing Company | Aircraft frame hole patterns and brackets, and associated methods |
CN204548517U (en) * | 2015-03-26 | 2015-08-12 | 深圳市大疆创新科技有限公司 | Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component |
CN204776026U (en) * | 2015-06-10 | 2015-11-18 | 深圳九星智能航空科技有限公司 | Lid quick assembly disassembly device behind unmanned aerial vehicle |
CN205418056U (en) * | 2016-03-29 | 2016-08-03 | 零度智控(北京)智能科技有限公司 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
EP3059172A1 (en) * | 2015-02-23 | 2016-08-24 | Fuji Jukogyo Kabushiki Kaisha | Structure for aircraft, method of manufacturing structure for aircraft and method of making design information of structure for aircraft |
CN106477039A (en) * | 2016-12-21 | 2017-03-08 | 深圳市道通智能航空技术有限公司 | A kind of rotor wing unmanned aerial vehicle |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1996039016A2 (en) * | 1995-06-01 | 1996-12-05 | Apple Computer, Inc. | Monitor housing having replaceable lid with thermal vent |
CN200997103Y (en) * | 2006-09-27 | 2007-12-26 | 联想(北京)有限公司 | Dustproof blind flange |
CN204392739U (en) * | 2014-12-26 | 2015-06-10 | 深圳市大疆创新科技有限公司 | Radiator structure and use the image transmission of this radiator structure |
CN205554624U (en) * | 2016-03-17 | 2016-09-07 | 深圳市大疆创新科技有限公司 | Shooting equipment and unmanned aerial vehicle |
CN206926801U (en) * | 2017-04-10 | 2018-01-26 | 深圳市大疆创新科技有限公司 | The upper lid and unmanned plane of unmanned plane |
-
2017
- 2017-04-10 CN CN201720370042.3U patent/CN206926801U/en not_active Expired - Fee Related
- 2017-06-14 CN CN201780060239.XA patent/CN109789919A/en active Pending
- 2017-06-14 WO PCT/CN2017/088336 patent/WO2018188188A1/en active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7059565B2 (en) * | 2003-10-21 | 2006-06-13 | The Boeing Company | Aircraft frame hole patterns and brackets, and associated methods |
EP3059172A1 (en) * | 2015-02-23 | 2016-08-24 | Fuji Jukogyo Kabushiki Kaisha | Structure for aircraft, method of manufacturing structure for aircraft and method of making design information of structure for aircraft |
CN204548517U (en) * | 2015-03-26 | 2015-08-12 | 深圳市大疆创新科技有限公司 | Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component |
CN204776026U (en) * | 2015-06-10 | 2015-11-18 | 深圳九星智能航空科技有限公司 | Lid quick assembly disassembly device behind unmanned aerial vehicle |
CN205418056U (en) * | 2016-03-29 | 2016-08-03 | 零度智控(北京)智能科技有限公司 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
CN106477039A (en) * | 2016-12-21 | 2017-03-08 | 深圳市道通智能航空技术有限公司 | A kind of rotor wing unmanned aerial vehicle |
Also Published As
Publication number | Publication date |
---|---|
CN206926801U (en) | 2018-01-26 |
CN109789919A (en) | 2019-05-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3246251B1 (en) | Rotorcraft and connecting structure for arm and airframe of rotorcraft | |
TWI539085B (en) | Locking apparatus | |
US9169845B2 (en) | Fan plate | |
WO2019134399A1 (en) | Unmanned aerial vehicle and casing thereof | |
US20070193724A1 (en) | Heat dissipating device | |
JP2008171695A (en) | Heating cooking device | |
CN103906415A (en) | Heat dissipation waterproof structure and set top box thereof | |
CN107444613A (en) | Winglet | |
WO2018188188A1 (en) | Upper cover of unmanned aerial vehicle and unmanned aerial vehicle | |
US6552269B1 (en) | Electrical outlet cover | |
CN103049059A (en) | Server combination | |
US20220151089A1 (en) | Electronic cabinet, and air inlet therefore | |
CN210129149U (en) | Tool-free server case upper cover locking device | |
US20170267333A1 (en) | Aircraft wing assembly | |
CN206125455U (en) | Camera mount for unmanned aerial vehicle | |
CN106428591B (en) | A kind of unmanned plane camera fixed frame | |
TW201443383A (en) | Air duct | |
CN104675833B (en) | Screw cover and assembly structure of screw cover and air port and air conditioner | |
CN203627499U (en) | Screw cover and assembly structure of screw cover and air port and air conditioner | |
CN210373370U (en) | Quick connection structure with waterproof function | |
CN207635485U (en) | Air condensing units top cap and have its air condensing units | |
USD891327S1 (en) | Decorative shroud for a coolant radiator with flush-fit fan | |
US20220171442A1 (en) | Louver assemblies for computer case ventilation | |
CN210707872U (en) | Novel heat radiation structure of unmanned aerial vehicle | |
CN205489195U (en) | Heat dissipation type electric power cabinet |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 17905244 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 17905244 Country of ref document: EP Kind code of ref document: A1 |