WO2023000571A1 - Voiture volante - Google Patents

Voiture volante Download PDF

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Publication number
WO2023000571A1
WO2023000571A1 PCT/CN2021/133437 CN2021133437W WO2023000571A1 WO 2023000571 A1 WO2023000571 A1 WO 2023000571A1 CN 2021133437 W CN2021133437 W CN 2021133437W WO 2023000571 A1 WO2023000571 A1 WO 2023000571A1
Authority
WO
WIPO (PCT)
Prior art keywords
flying car
flying
state
rotors
wings
Prior art date
Application number
PCT/CN2021/133437
Other languages
English (en)
Chinese (zh)
Inventor
王谭
梁毅诚
赵德力
黄锦腾
胡岩伟
Original Assignee
广东汇天航空航天科技有限公司
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 广东汇天航空航天科技有限公司 filed Critical 广东汇天航空航天科技有限公司
Publication of WO2023000571A1 publication Critical patent/WO2023000571A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft

Definitions

  • the two wings spread out radially relative to the body, and the rotors rotate to discharge air toward the bottom of the body for Provide lift when the flying car is in a hanging state.
  • the preset distance corresponds to the distance between the arms of the pitch control arm of the flying car .
  • the flying car provided in this embodiment includes a body, which is provided with a control system for controlling the switching between the flying state and the driving state of the flying car; wings arranged on opposite sides of the body, the wings are close to One end of the vehicle body is rotatably connected to the vehicle body along the first rotation direction; the rotors are respectively installed on the two wings, and the rotors are rotatably installed on the two wings along the second rotation direction.
  • the rotor 300 of the flying car enters the folding state, the rotor 300 is rotated to the bottom of the wing 200 through the tilting structure, so as to realize the folding and folding of the rotor 300, thereby reducing the space occupied by the rotor 300 in the width direction of the body 100 , to reduce the width dimension of the flying car.
  • the two rotors 300 are configured to have a pitch differential and a tilt differential, and the two rotors 300 provide the flying car with a control moment in the rolling direction through the pitch differential; the two rotors 300 provide The flying car provides control torque in the yaw direction.
  • the empennage includes a first empennage 410 connected to the vehicle body and a second empennage 420 (shown in FIG. 7 ) that is rotationally connected to the first empennage 410; when the flying car is in flight, the second empennage 420 rotates to Transversely or rotate to the extension direction of the first tail 410; when the flying car is in a driving state, the second tail 420 rotates to the longitudinal direction or rotates to a direction perpendicular to the first tail 410.
  • the second empennage 420 and the first empennage 410 there is a rotating shaft for the folding of the second empennage 400.
  • the axial direction of the rotating shaft is arranged laterally.
  • the lateral direction can be the direction of the X axis.
  • the second empennage 400 can rotate laterally around the axis of rotation.
  • the longitudinal direction may be the Z-axis direction.
  • the second tail 400 may be a reverse tail for controlling the flying direction of the flying car. In the driving state, after the second tail 400 is folded through the rotating shaft, the width of the flying car can be further reduced.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Toys (AREA)

Abstract

L'invention concerne une voiture volante, comprenant une carrosserie de voiture (100) pourvue d'un système de commande utilisé pour commander la voiture volante de sorte à commuter entre un état de vol et un état de déplacement ; des ailes (200) disposées sur deux côtés opposés du corps d'habitacle (100), l'extrémité de chaque aile (200) proche de la carrosserie de voiture (100) étant reliée de manière rotative au corps d'habitacle (100) dans un premier sens de rotation ; des rotors (300) respectivement prévus sur les deux ailes (200), chaque rotor (300) étant disposé de manière rotative à l'extrémité de chacune des deux ailes (200) à distance du corps d'habitacle (100) dans un second sens de rotation ; des ailes arrière disposées sur deux côtés de la partie arrière du corps d'habitacle (100) ; et un ventilateur à conduit (500) disposé au milieu des deux ailes arrière. Lorsque la voiture volante est dans l'état volant, les ailes (200) tournent par rapport au corps d'habitacle (100) dans le premier sens de rotation pour être dans un état déplié, et les rotors (300) peuvent tourner dans le second sens de rotation ; lorsque la voiture volante est dans l'état de déplacement, les ailes (200), les rotors (300) et le corps d'habitacle (100) se chevauchent au moins partiellement dans la direction longitudinale. La voiture volante peut être commutée entre trois configurations de déplacement sur route, de décollage et atterrissage verticaux, et de vol horizontal.
PCT/CN2021/133437 2021-07-20 2021-11-26 Voiture volante WO2023000571A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202110819931.4A CN113370730B (zh) 2021-07-20 2021-07-20 飞行汽车
CN202110819931.4 2021-07-20

Publications (1)

Publication Number Publication Date
WO2023000571A1 true WO2023000571A1 (fr) 2023-01-26

Family

ID=77582670

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2021/133437 WO2023000571A1 (fr) 2021-07-20 2021-11-26 Voiture volante

Country Status (2)

Country Link
CN (1) CN113370730B (fr)
WO (1) WO2023000571A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113370730B (zh) * 2021-07-20 2022-12-20 广东汇天航空航天科技有限公司 飞行汽车
CN113753230B (zh) * 2021-10-11 2023-08-18 广东汇天航空航天科技有限公司 飞行器、机翼组件及飞行汽车
CN114043831A (zh) * 2021-11-01 2022-02-15 广东汇天航空航天科技有限公司 飞行汽车
WO2023088307A1 (fr) * 2021-11-17 2023-05-25 广东汇天航空航天科技有限公司 Système de commande et procédé associé pour une voiture volante, et voiture volante
CN113895190A (zh) * 2021-11-17 2022-01-07 广东汇天航空航天科技有限公司 飞行汽车的操纵系统及飞行汽车
CN115091905B (zh) * 2022-07-21 2024-05-31 北京航空航天大学 一种电动飞行汽车

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110042507A1 (en) * 2009-08-19 2011-02-24 Seiford Sr Donald S Convertible Vehicle For Road, Air, and Water Usage
US20160243910A1 (en) * 2013-12-20 2016-08-25 Xinru HU Amphibious Flying Car
CN107984992A (zh) * 2017-11-28 2018-05-04 北京航空航天大学 一种可垂直起降的陆空两用运载器
CN108146169A (zh) * 2017-11-28 2018-06-12 北京航空航天大学 一种机翼后折式陆空两用运载器
CN108528162A (zh) * 2018-06-15 2018-09-14 中宇航通（北京）科技有限公司 飞行汽车伸缩式尾翼机构及飞行汽车
CN110065352A (zh) * 2019-05-24 2019-07-30 上海应用技术大学 一种倾转涵道式结构的飞行汽车
CN113370730A (zh) * 2021-07-20 2021-09-10 广东汇天航空航天科技有限公司 飞行汽车

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Publication number Priority date Publication date Assignee Title
US5622133A (en) * 1994-09-20 1997-04-22 Seagull Decor Co., Ltd. Transport facility with dynamic air cushion
CN101161549A (zh) * 2007-11-29 2008-04-16 东北师范大学 旋翼式地效飞行器
CN205768418U (zh) * 2016-05-21 2016-12-07 龙川 改进型分布式电动涵道风扇襟翼增升系统及其飞行汽车
CN108313263A (zh) * 2018-01-26 2018-07-24 易瓦特科技股份公司 用于固定翼无人机的机身动力系统
CN108528714A (zh) * 2018-01-26 2018-09-14 易瓦特科技股份公司 用于固定翼无人机的可调式旋翼动力机头装置
CN210133282U (zh) * 2019-03-05 2020-03-10 张振环 一种改良版鱼鹰运输机
CN110654190A (zh) * 2019-10-31 2020-01-07 南京航空航天大学 一种倾转无轴涵道旋翼飞行汽车及其工作方法

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110042507A1 (en) * 2009-08-19 2011-02-24 Seiford Sr Donald S Convertible Vehicle For Road, Air, and Water Usage
US20160243910A1 (en) * 2013-12-20 2016-08-25 Xinru HU Amphibious Flying Car
CN107984992A (zh) * 2017-11-28 2018-05-04 北京航空航天大学 一种可垂直起降的陆空两用运载器
CN108146169A (zh) * 2017-11-28 2018-06-12 北京航空航天大学 一种机翼后折式陆空两用运载器
CN108528162A (zh) * 2018-06-15 2018-09-14 中宇航通（北京）科技有限公司 飞行汽车伸缩式尾翼机构及飞行汽车
CN110065352A (zh) * 2019-05-24 2019-07-30 上海应用技术大学 一种倾转涵道式结构的飞行汽车
CN113370730A (zh) * 2021-07-20 2021-09-10 广东汇天航空航天科技有限公司 飞行汽车

Also Published As

Publication number Publication date
CN113370730A (zh) 2021-09-10
CN113370730B (zh) 2022-12-20

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