+

WO2018032866A1 - Hydroglisseur à double hélice et deux moteurs - Google Patents

Hydroglisseur à double hélice et deux moteurs Download PDF

Info

Publication number
WO2018032866A1
WO2018032866A1 PCT/CN2017/088058 CN2017088058W WO2018032866A1 WO 2018032866 A1 WO2018032866 A1 WO 2018032866A1 CN 2017088058 W CN2017088058 W CN 2017088058W WO 2018032866 A1 WO2018032866 A1 WO 2018032866A1
Authority
WO
WIPO (PCT)
Prior art keywords
engine
propeller
hull
scull
rudder
Prior art date
Application number
PCT/CN2017/088058
Other languages
English (en)
Chinese (zh)
Inventor
陈大力
王丹丹
张忠阳
李钢
郭晴阳
王民
郭晓娜
郑帅
Original Assignee
抚顺抚运安仪救生装备有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 抚顺抚运安仪救生装备有限公司 filed Critical 抚顺抚运安仪救生装备有限公司
Publication of WO2018032866A1 publication Critical patent/WO2018032866A1/fr

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H7/00—Propulsion directly actuated on air
    • B63H7/02—Propulsion directly actuated on air using propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B3/00—Hulls characterised by their structure or component parts
    • B63B3/14—Hull parts
    • B63B3/48—Decks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H21/00—Use of propulsion power plant or units on vessels
    • B63H21/12—Use of propulsion power plant or units on vessels the vessels being motor-driven
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H23/00—Transmitting power from propulsion power plant to propulsive elements
    • B63H23/02—Transmitting power from propulsion power plant to propulsive elements with mechanical gearing
    • B63H23/06—Transmitting power from propulsion power plant to propulsive elements with mechanical gearing for transmitting drive from a single propulsion power unit
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/08—Steering gear

Definitions

  • the invention relates to a twin-engine scull airboat.
  • a double-engined scull airboat including a hull.
  • An engine bracket is arranged in the cabin of the hull, and the engine and the propeller are mounted on the engine bracket. on. There are no parts below the hull waterline, you can sail in the area where the water is full of debris, or you can drive in shallow water, ice, snow, swamp and shoal.
  • the patent is a single-single-propeller structure, which is light in weight, powerful, stable and flexible, but has a small hull load as a device.
  • the low-capacity, core components are completely dependent on imports and the supply is unstable, and the design is simple and easy to be copied.
  • an object of the present invention is to provide a dual-engine scull airship.
  • the airboat has a wide applicability, in addition to the full function and performance of a general assault boat and a small yacht, it also has the capacity that ordinary ships do not have.
  • a dual-engine scull airship comprising a hull, an engine system, a reducer group, a propeller system, a steering system and a control system; wherein the upper deck of the hull is forwardly inclined, front low and high
  • the engine system is located at a rear 1/3 position of the hull, and includes two engines; the engine system is coupled to the propeller system through the reducer group, and the propeller system is driven by the engine system;
  • the hull is divided into upper and lower parts, the bottom of the ship is welded with 5083 alloy aluminum, and the bottom of the bottom of the ship is inverted "concave"; the bow and the bottom of the ship are tangentially curved upward; the freeboard on both sides of the hull has a camber angle Several T-shaped aluminum ribs are welded on the inside side of the side.
  • the engine system is disposed in a canopy made of metal, and the two engines are longitudinally symmetrically disposed on both sides of the central axis of the hull; the two engines are mounted on a set of brackets, and the bracket is connected with the bottom bolt; the two engines Sharing one accelerator pedal and synchronizing the speed, the two engines each have an independent starting power supply system, fuel supply system, cooling system and monitoring system, sharing a group of fuel tanks.
  • the reducer group includes two sets of reducers, and the reducer adopts a split structure, and each set of reducers corresponds to one engine, and the input synchronous gear of the reducer is directly connected with the output shaft of the engine, and the output of the reducer is synchronized.
  • a gear is coupled to the propeller input shaft on the propeller system, and two synchronizing gears transmit power through a synchronizing toothed belt connection, the outer side of the retarder being provided with a retarder cover.
  • the engine is connected to the bottom of the hull through an engine bracket, and a joint of the two is provided with a damper foot; the fuel tank of the engine is disposed on an engine bracket below the engine.
  • the propeller system includes two sets of propellers, the propeller consisting of a support frame, a drive shaft, a propeller, and a shroud; the angle of the propeller blades is adjustable by changing the inclination of the propeller blades, and further Change the direction and size of the thrust.
  • the inclination angle of the blade is adjusted between -5° and +15°; the middle position, that is, 0° is an idle speed; the forward inclination is positioned to 10° and 15°, and 10° is a normal forward speed. , 15° is the high speed gear; the reverse tilt angle is positioned at -5°, and the thrust direction is changed without changing the direction of rotation of the propeller.
  • the airboat is slowing down and reversing the maneuver.
  • the steering system is vertically disposed on the rudder of the bow for the cable control;
  • the rudder has a total of three rudder plates, the left and right rudder plates are disposed at the longitudinal axis of the propeller, and the middle portion is at the central axis of the hull
  • the maximum swing angles of the left and right sides are each 50°.
  • control system includes a plurality of control buttons disposed on the bridge, an electronic accelerator pedal that controls the two engines, and a steering wheel.
  • the hull is provided with two inflatable airbags in the bow and the bow; the hull is divided into a front storage compartment, a middle passenger compartment and a rear engine compartment, and the middle passenger compartment is divided into a hard top type, Soft top and open.
  • the invention has wide applicability, and has the functions and performances of a general assault boat and a small yacht, and also has the capacity that ordinary ships do not have.
  • Figure 1 is a perspective view of a hard-top double-engined scull airboat of the present invention
  • FIG. 2 is a top plan view of a hard top double-engined twin-blade airboat of the present invention
  • Figure 3 is a perspective view of the soft top double-engined scull air boat of the present invention.
  • Figure 4 is a top plan view of the soft top double-engined scull airboat of the present invention.
  • Figure 5 is a perspective view of the open double-engined scull airboat of the present invention.
  • Figure 6 is a top plan view of the open type double-engine scull airboat of the present invention.
  • Figure 7 is a side view of the twin-engined two-blade airboat of the present invention.
  • Figure 8 is a schematic structural view of a propeller system of the present invention.
  • Figure 9 is a schematic view showing the connection structure of the propeller system, the engine system and the hull of the present invention.
  • Figure 10 is a perspective view of the hull of the present invention.
  • Figure 11 is a plan view of the hull of the present invention.
  • Figure 12 is a schematic view showing the structure of the engine and the bottom of the ship according to the present invention.
  • Figure 13 is a schematic structural view showing the connection of the engine system of the present invention to the bottom of the ship;
  • FIG. An embodiment of the present invention is shown in FIG. a reducer group (not shown), a propeller system 3, a steering system 4, and a control system; wherein the upper deck of the hull 1 is inclined forward, is low in front and high in height, and the engine system 2 is located in the rear 1/1 of the hull 1. 3 position, which comprises two engines 21; the engine system 2 is connected to the propeller system 3 via a reducer group, and the propeller system 3 is driven by the engine system 2; the steering system 4 is a rudder 14 vertically disposed at the bow, and the rudder 14 is passed
  • the handle control boosting device is coupled to the handle or steering wheel in the control system.
  • the hull 1 is naturally horizontal after the water inlet deck, and the axis of the drive shaft 10 of the thruster system 3 is parallel to the horizontal plane.
  • the hull 1 is divided into upper and lower parts, the bottom 19 of the ship is welded by 5083 alloy aluminum, and the bottom of the bottom 19 is inverted "concave", that is, the bottom of the ship is provided with a groove 18; the bow and the bottom of the ship are tangentially curved upward; the hull There are camber angles on the freeboard sides and a number of T-shaped aluminum reinforcements on the inside of the side.
  • the bottom 19 of the boat forms an inverted "concave" type bottom, which increases the strength and reduces the contact area when running on a hard flat surface, thereby reducing the frictional force, and also arranging the functional mechanism in the middle groove. Achieve different purposes of use.
  • the length of the hull is 5,930 mm wide and 2,705 mm wide, and the tail is 850 mm high.
  • the upper deck is tilted forward and the bow is 755 mm above the ground. Since the maximum length of the aluminum plate that can be purchased at present is 6 m, the maximum length that can be produced without lateral welding can maximize the use of raw materials.
  • the bottom material is 5mm thick, the side wall and the deck material are 3mm thick, and the reinforcing T-shaped material is 40 ⁇ 40 ⁇ 4mm.
  • the upper part of the hull 1 is divided into a front storage compartment, a middle passenger compartment and a rear engine compartment according to the compartment.
  • the hard-top central passenger compartment is made of a metal frame with a fiberglass structure, bolted to the lower hull interface, and has a sealed structure that is protected from rain and water guns and can be used around the clock.
  • the front storage compartment occupies the bow section, and the upper flap has a waterproof structure to withstand storm scouring and cabin volume. It is about 600L.
  • the central passenger compartment is the main cabin, driving and riding, the cabin is 2200mm at the widest point, the narrowest part of the tail is 1500mm, and the height of the cabin is 1510mm. Members will have plenty of head space and leg space in the seat to ensure each member.
  • the driver is in the middle of the first row.
  • the hard top cannot be opened.
  • the first row and the second row have a large area.
  • the portholes, the four portholes on both sides are limited to the hull structure can only be partially opened, but can be quickly disassembled, which is convenient to open when opening a large area.
  • the third row has no portholes due to the curved structure of the cabin, and the roof has a large area.
  • Skylight 7 to ensure the lighting in the cabin.
  • the rear engine compartment is also open on both sides of the door structure, made of heat-resistant FRP or aluminum alloy material, with vents on the front and rear.
  • the surface of the hull and the inner surface are painted with paint, and the surface is additionally sprayed with a matt finish to meet the quality inspection standards of the automobile.
  • a reinforcing guard rail 8 is provided at an upper portion of the hull 1.
  • the engine system 2 is disposed in a canopy made of metal, and the two engines 21 are longitudinally symmetrically disposed on both sides of the central axis of the hull 1; the two engines 21 are mounted on a set of brackets, that is, the engine bracket 20, the bracket and the bottom bolt Connection; two engines 21 share an accelerator pedal, and the speed is synchronized.
  • the two engines each have an independent starting power supply system, a fuel supply system, a cooling system and a monitoring system, sharing a group of fuel tanks.
  • the engine 21 uses two identical in-line four-cylinder turbocharged petrol engines, each with independent intake, exhaust, cooling, power, fueling, ECU control, and operational monitoring systems.
  • a throttle controller through the adjustment of the ECU control unit, makes the speed of the two engines consistent at 0%-100% throttle opening, so that the thrust of the left and right sides will be straight.
  • the two engines share a set of fuel tanks 25.
  • the reducer group adopts a split structure, the reducer group includes two sets of reducers, each set of reducers corresponds to one transmitter, the input synchronous gear 24 of the reducer is connected with the output shaft 23 of the engine 21, and the output synchronous gear 15 of the reducer Connected to a propeller drive shaft 10 fixed to the propeller system 3, the two synchronizing gears transmit power using a synchronous toothed belt connection, and the outer side of the reducer is provided with a reducer cover. Furthermore, a pitch torque converter 5 is also provided on the propeller input shaft of the propeller system 3.
  • the design of the reducer of the present application has a reduction ratio of 2:1 (total gear ratio of 70:140), and the synchronous toothed belt has a specification of RPP8M-2104-100. After the reducer is installed, the reducer cover is fully wrapped, dustproof and waterproof.
  • the engine 21 is connected to the bilge 19 of the hull 1 through the engine bracket 20, and the connection between the two is provided with a damper foot pad 22; the fuel tank 25 of the engine 21 is disposed at the engine bracket below the engine 21. on.
  • the setting of the shock absorber foot pad 22 can effectively alleviate the vibration generated during the working process of the engine.
  • the propeller system 3 includes two sets of propellers, which are composed of a support frame 9, a drive shaft 10, a propeller 11 and a shroud 12; the angle of the blades of the propeller 11 is adjustable, by changing the inclination of the propeller blades, Then change the direction and size of the thrust.
  • the inclination angle of the blade is adjusted between -5° and +15°; the middle position, that is, 0° is the idle speed; when the blade inclination angle is at this position, no thrust is generated when the rotation is performed, and the air boat does not move.
  • the positive tilt angle is positioned to 10° and 15°, and 10° is the normal forward gear. It is used in air boat start, medium and low speed sailing, and cross-country and off-road conditions; 15° is high speed; only in air boat high speed Used during cruising, reducing engine speed saves fuel.
  • the reverse tilt is positioned at -5°, and the thrust direction is changed without changing the direction of rotation of the propeller, so that the air boat can be decelerated and reversing.
  • Each propeller 11 is provided with a separate shroud 12 that can lift the thrust and also provide protection.
  • the propeller 11 is mounted on the propeller mount 17 by a propeller mount 16.
  • the steering system 4 is vertically disposed on the rudder 14 of the bow for the cable control; the rudder 14 has a total of three rudder plates, the left and right rudder plates are disposed at the longitudinal axis of the propeller, and the middle portion is at the central axis of the hull, passing through the two
  • the pull rods between the group pull wires and the rudder plates rotate synchronously, and the maximum swing angles of the left and right sides are each 50°.
  • the rudder 14 is fixed to the directional rudder 13.
  • the driver in the cab controls the rudder through the steering wheel or the lever, and the steering wheel is electronically assisted by 1:1 steering.
  • the drawbars are mechanically connected, divided into two left and right, and are arranged in reverse linkage with each other.
  • the control system includes several control buttons on the bridge, an electronic accelerator pedal that controls the two engines, and a steering wheel. Electrical equipment such as lights, warning lights, and in-cabin drain pumps are controlled by switches on the bridge.
  • the hull 1 is provided with two inflatable airbags (not shown) in the bow and the bow; the anti-sinking airbag is opened by a knob switch on the bridge.
  • Inflatable airbag usually folds and stores without occupying storage space. If there is water in the hull, overturning, etc., the airbag is filled with buoyancy by high-pressure gas storage device, which can provide buoyancy of more than 3 tons to prevent the air boat from sinking. In the water.
  • the dual-engine scull airboat of the present application also includes an auxiliary system, for example, a monitoring system, a passenger cabin air conditioning system, a lighting system, a low-power AC/DC power supply system, a hard plane reduction device, and other auxiliary function systems can refer to existing The configuration of cars and yachts is added.
  • an auxiliary system for example, a monitoring system, a passenger cabin air conditioning system, a lighting system, a low-power AC/DC power supply system, a hard plane reduction device, and other auxiliary function systems can refer to existing The configuration of cars and yachts is added.
  • the monitoring system consists of two engine tachometers, two water temperature meters, two voltmeters, a speedometer, a fuel gauge, a rudder angle gauge, a flat panel display, and a navigation recorder.
  • two sets of heaters and air-conditioning units are installed inside to work synchronously to provide sufficient warm/cold air for the passenger compartment.
  • the light of the airboat of the present application is composed of two sets of LED lights integrated in the bow, a single set of power of 60W, variable light, providing illumination for conventional night flights.
  • the hard top is also fitted with a set of four 55W xenon dimmers to increase the intensity of the illumination.
  • the power supply system on the air boat is provided by two 12V 120AH batteries, and the battery is charged by the generator when the engine is running.
  • the two batteries are disconnected in parallel when starting the engine, and the rest time is in parallel.
  • the speed reducer of the present application is a hydraulic cylinder that pushes a speed reducer on the bottom of the bow to friction with the ground to reduce the speed.
  • the driver depresses the deceleration pedal to perform the electrohydraulic operation, which increases the safety factor for the ice and snow plane.
  • FIG. 3, FIG. 4, and FIG. 7-13 Another embodiment of the present invention is shown in FIG. 3, FIG. 4, and FIG. 7-13.
  • the difference between the embodiment and the embodiment 1 is that the middle passenger compartment of the dual-engine scull airboat is a soft top type, and the soft top can be Open and store at the rear of the passenger compartment. At this time, the cabin becomes a convertible, which gives excellent visibility. After the soft top is closed, there are two curtains that can be rolled up on both sides. The curtain and the soft top are connected by a sealing zipper. Rainproof.
  • FIG. 5, FIG. 6, and FIG. 7-13 Another embodiment of the present invention is shown in FIG. 5, FIG. 6, and FIG. 7-13.
  • the difference between this embodiment and the embodiment 1 is that the central passenger compartment of the dual-engine scull airboat is open, and the open type is waterproof.
  • the canopy has only a detachable awning.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

La présente invention concerne un hydroglisseur à double hélice et deux moteurs, comprenant un corps de bateau (1), un système de moteur (2), un ensemble réducteur de vitesse, un système d'hélice (3), un système de direction (4), et un système de commande. Un pont supérieur du corps de bateau (1) s'incline vers l'avant, avec une extrémité avant inférieure et une extrémité arrière supérieure. Le système moteur (2) est situé à la position 1/3 à l'arrière du corps de bateau (1) et comprend deux moteurs (21). Le système de moteur (2) est raccordé au système d'hélice (3) au moyen de l'ensemble réducteur de vitesse, de telle sorte que le système de moteur entraîne le système d'hélice (3). Le système de direction (4) est un gouvernail (14) disposé verticalement au niveau de la poupe. Le gouvernail (14) est raccordé à une poignée ou à un volant dans le système de commande au moyen d'un dispositif de commande et d'assistance de poignée. Après que le corps de bateau (1) est lancé, le pont est naturellement dans un état horizontal, et l'axe d'un arbre d'entraînement (10) du système d'hélice (3) est parallèle au plan horizontal. L'hydroglisseur est largement applicable, et a une capacité de déplacement que n'ont pas les embarcations courantes, en plus de toutes les fonctions et capacités des embarcations d'assaut ordinaires et des petits bateaux de plaisance.
PCT/CN2017/088058 2016-08-19 2017-06-13 Hydroglisseur à double hélice et deux moteurs WO2018032866A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201610695048.8A CN106081038A (zh) 2016-08-19 2016-08-19 一种双发双桨空气艇
CN201610695048.8 2016-08-19

Publications (1)

Publication Number Publication Date
WO2018032866A1 true WO2018032866A1 (fr) 2018-02-22

Family

ID=58070274

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/088058 WO2018032866A1 (fr) 2016-08-19 2017-06-13 Hydroglisseur à double hélice et deux moteurs

Country Status (2)

Country Link
CN (1) CN106081038A (fr)
WO (1) WO2018032866A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112388217A (zh) * 2019-08-19 2021-02-23 中集安瑞环科技股份有限公司 筒体加强圈装配定位设备
EP3830806A4 (fr) * 2018-08-01 2022-05-04 Quantum Innovations, Inc. Véhicule marin à propulsion par hélice et procédé de navigation par voie navigable commandée à distance
CN115158620A (zh) * 2022-08-09 2022-10-11 江苏科技大学 一种用于吊舱推进器的分冰防护装置及其设计方法

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106081038A (zh) * 2016-08-19 2016-11-09 抚顺抚运安仪救生装备有限公司 一种双发双桨空气艇
CN106394541B (zh) * 2016-11-21 2018-09-25 黑龙江水运规划设计院 水陆两栖滑行艇
CN106515330B (zh) * 2016-12-12 2018-11-06 李新亚 高速两栖登陆车
CN107264762A (zh) * 2017-07-12 2017-10-20 樊朝杰 一种船用方向机
CN108163172A (zh) * 2018-01-22 2018-06-15 哈尔滨工程大学 一种水田无人风动艇
CN108128431A (zh) * 2018-02-06 2018-06-08 杨辉 一种单发航空螺旋桨空气船
CN108860445A (zh) * 2018-04-03 2018-11-23 惠安县圆周率智能科技有限公司 一种带有微气泡功能的水翼艇
CN108583777B (zh) * 2018-06-27 2023-04-07 长沙紫宸科技开发有限公司 一种便携手提箱式自回正水上娱乐艇
CN112537415A (zh) * 2020-12-08 2021-03-23 南京航空航天大学 用于水上无人运输物资的轻小型风扇推进装置

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002060550A1 (fr) * 2001-01-31 2002-08-08 Zee Franklin Dispositif a propulsion aerienne
US20050112962A1 (en) * 2003-11-21 2005-05-26 Husky Airboats Ltd. Counter rotating air propeller drive system
CN101032961A (zh) * 2006-04-03 2007-09-12 邱刚 双空气螺旋桨拉进式全垫升气垫船
CN201580527U (zh) * 2009-11-18 2010-09-15 抚顺抚运安仪救生装备有限公司 抢险救援艇船体
CN202935564U (zh) * 2012-11-09 2013-05-15 叶耀林 新型轮船
CN104325850A (zh) * 2013-07-22 2015-02-04 孙学文 新型雪地船
CN105711790A (zh) * 2016-01-27 2016-06-29 抚顺抚运安仪救生装备有限公司 一种空气艇
CN106081038A (zh) * 2016-08-19 2016-11-09 抚顺抚运安仪救生装备有限公司 一种双发双桨空气艇
CN205931200U (zh) * 2016-08-19 2017-02-08 抚顺抚运安仪救生装备有限公司 一种双发双桨空气艇

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201009884Y (zh) * 2007-03-06 2008-01-23 邱刚 双空气螺旋桨拉进式全垫升气垫船
CN102060095A (zh) * 2009-11-18 2011-05-18 抚顺抚运安仪救生装备有限公司 动力帆抢险救援艇
CN204846281U (zh) * 2015-08-21 2015-12-09 沈阳抚运飞舟商贸有限公司 搜索救援型空气动力艇
CN105539794A (zh) * 2016-02-23 2016-05-04 张家港江苏科技大学产业技术研究院 一种可变距水下推进系统

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002060550A1 (fr) * 2001-01-31 2002-08-08 Zee Franklin Dispositif a propulsion aerienne
US20050112962A1 (en) * 2003-11-21 2005-05-26 Husky Airboats Ltd. Counter rotating air propeller drive system
CN101032961A (zh) * 2006-04-03 2007-09-12 邱刚 双空气螺旋桨拉进式全垫升气垫船
CN201580527U (zh) * 2009-11-18 2010-09-15 抚顺抚运安仪救生装备有限公司 抢险救援艇船体
CN202935564U (zh) * 2012-11-09 2013-05-15 叶耀林 新型轮船
CN104325850A (zh) * 2013-07-22 2015-02-04 孙学文 新型雪地船
CN105711790A (zh) * 2016-01-27 2016-06-29 抚顺抚运安仪救生装备有限公司 一种空气艇
CN106081038A (zh) * 2016-08-19 2016-11-09 抚顺抚运安仪救生装备有限公司 一种双发双桨空气艇
CN205931200U (zh) * 2016-08-19 2017-02-08 抚顺抚运安仪救生装备有限公司 一种双发双桨空气艇

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3830806A4 (fr) * 2018-08-01 2022-05-04 Quantum Innovations, Inc. Véhicule marin à propulsion par hélice et procédé de navigation par voie navigable commandée à distance
CN112388217A (zh) * 2019-08-19 2021-02-23 中集安瑞环科技股份有限公司 筒体加强圈装配定位设备
CN115158620A (zh) * 2022-08-09 2022-10-11 江苏科技大学 一种用于吊舱推进器的分冰防护装置及其设计方法
CN115158620B (zh) * 2022-08-09 2024-04-05 江苏科技大学 一种用于吊舱推进器的分冰防护装置及其设计方法

Also Published As

Publication number Publication date
CN106081038A (zh) 2016-11-09

Similar Documents

Publication Publication Date Title
WO2018032866A1 (fr) Hydroglisseur à double hélice et deux moteurs
US6840825B1 (en) Amphibious recreational vehicle
CN110758700A (zh) 一种用于船体的外挂式电动推进装置
CN103171737B (zh) 一种节能高速列船
CN112659829A (zh) 一种全浮式水陆两栖车
CN204846281U (zh) 搜索救援型空气动力艇
CN205707146U (zh) 一种太阳能双体旅游船
CN106218807B (zh) 多功能履带式高效水翼登陆艇及操作方法
US20240416699A1 (en) Amphibious vehicle
CN205931200U (zh) 一种双发双桨空气艇
CN207328765U (zh) 全封闭型巡逻执法空气艇
CN211196570U (zh) 一种用于船体的外挂式电动推进装置
CN111688896A (zh) 用于船舶的电池分体型外挂电动推进装置
CN216069507U (zh) 一种全浮式水陆两栖车
CN213292676U (zh) 一种使用吊舱式电动螺旋桨的船舶外挂推进装置
CN113442669A (zh) 一种6x6水陆两栖救援车
CN209305798U (zh) 一种方便吊装的新型娱乐游艇
RU68424U1 (ru) Устройство для компенсации опрокидывающего момента амфибийного аппарата на воздушной подушке
CN208993676U (zh) 一种水陆两用的气动船
CN219428315U (zh) 一种适应高海况高航速三座迷你快艇
CN221776017U (zh) 太阳能动力绿色载货汽车滚装船
CN219927391U (zh) 电动两栖房艇
CN112141307A (zh) 一种使用吊舱式电动螺旋桨的船舶外挂推进装置
CN216069508U (zh) 一种6x6水陆两栖救援车
CN220924482U (zh) 太阳能电力推进绿色滚装船

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: 17840842

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: 17840842

Country of ref document: EP

Kind code of ref document: A1

点击 这是indexloc提供的php浏览器服务，不要输入任何密码和下载