WO2018236295A1 - Facilitation du mouvement horizontal de drones - Google Patents

Facilitation du mouvement horizontal de drones Download PDF

Info

Publication number
WO2018236295A1
WO2018236295A1 PCT/TR2017/000109 TR2017000109W WO2018236295A1 WO 2018236295 A1 WO2018236295 A1 WO 2018236295A1 TR 2017000109 W TR2017000109 W TR 2017000109W WO 2018236295 A1 WO2018236295 A1 WO 2018236295A1
Authority
WO
WIPO (PCT)
Prior art keywords
drone
wings
foldable
drones
folded
Prior art date
Application number
PCT/TR2017/000109
Other languages
English (en)
Inventor
Ali Turan
Original Assignee
Ali Turan
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 Ali Turan filed Critical Ali Turan
Publication of WO2018236295A1 publication Critical patent/WO2018236295A1/fr

Links

Classifications

    • 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
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers

Definitions

  • Drones have propellers with which they perform departing, landing and horizontal movements.
  • FIGURES AND THEIR EXPLANATION are identical to FIGURES AND THEIR EXPLANATION:
  • FIGURE- 1 Aerial viewpoint of the drone with wings.
  • FIGURE-2 The view of the drone when its wings are folded upwards.
  • FIGURE-3 The view of the drone when its wings are folded upwards and downwards more than once.
  • FIGURE-4 The use of the drone wings as legs when the drone wings are folded upwards and downwards more than once.
  • FIGURE-5 The use of the drone wings as legs when they are folded downwards.
  • FIGURE-6 The use of the folding edges of the drone wings as legs when the drone wings are folded upwards and downwards more than once.
  • FIGURE-7 The horizontal movement position of the drone, when the wings are open and drone motors are turned horizontal.
  • FIGURE-8 The positioning adjustment of the drone motors for the drones' balance at the drone's horizontal movement.
  • Drone wing that is foldable to upwards
  • FIGURE- 1 Aerial viewpoint of the drone with wings.
  • the drone propellers (5) which are mechanically connected to the drone engines (6), the vertical movement of the drone is controlled.
  • the drone motors are made horizontal by opening the wings after the drone is departed as shown in FIGURE-7 where the drone propellers (5) applies horizontal force to the drone and enables it move in the drone's horizontal movement direction (11). Since flaps do not exist on the drone wings to maintain the balance, the drone's balance needs to be maintained in the horizontal axis (10) by turning the drone motors (6) to the motor angle (8), as shown in FIGURE-8.
  • FIGURE-2 The drone that has drone wings that are folded upwards (2). Since the drone wings are folded upwards, the landing to the ground (8) can be made over the drone leg (7).
  • FIGURE-3 The drone that has drone wing that is foldable more than once (4). Allocation of little space is aimed after folding the drone wing by first folding it to upwards, secondly to downwards. In this structure, the drone lands to the ground (8) over the drone leg (7).
  • FIGURE-4 The drone that has drone wing that is foldable more than once (4). Allocation of little space is aimed after folding the drone wing by first folding it to upwards, secondly to downwards.
  • the drone wing that is foldable more than once (4) is used as drone leg (7) when it is folded. Drone lands to the ground (8) over the drone wing that is foldable more than once (4).
  • FIGURE-5 The drone that has drone wings that are folded downwards (3). Since the drone wing is folded downwards, the drone has a structure that enables landing over the drone wing that is foldable to downwards (3).
  • FIGURE-6 The drone structure that has drone wing that is foldable more than once (4). Allocation of little space is aimed after folding the drone wing by first folding it to downwards, secondly to upwards.
  • the drone wing that is foldable more than once (4) is used as drone leg (7) when it is folded. Drone lands to the ground (8) over the drone wing that is foldable more than once (4).
  • FIGURE-7 Explained within the explanation of FIGURE- 1.
  • FIGURE-8 Explained within the explanation of FIGURE- 1.
  • Drones has become a product suitable for many applications by their ability to depart vertically from the ground, land vertically to the ground, stay in mid-air and perform manoeuvres with ease. Designed system, while preserving the existing abilities of the drones, provides them with ability of horizontally traveling longer distances and fly for longer time periods.
  • foldable drone wing is attached to the drone body (1).
  • the advantage of foldable drone wings is to minimise the space that the drone allocated at the ground (8) at departure and landings by being fold at the departure and landings, and making the drone consume less energy, by reducing the air resistance that will be created because of the drone wings, at the departure of the drone, FIGURE-2,3,4,5,6.
  • the drone can be made allocate less space when it is folded, by making the drone wings foldable more than once as well as letting them foldable once to upwards or downwards, FIGURE-3,4,6.
  • the drone wings can be used a drone legs (7) for landing, FIGURE-4,5,6.
  • the drone wings can be folded when standing in mid-air to make the drone be affected by the weather conditions less.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Catching Or Destruction (AREA)

Abstract

L'objectif de l'invention est de réaliser des drones capables de parcourir de plus longues distances et de rester en vol pendant de plus longues périodes en les amenant à utiliser leurs ailes dans leurs mouvements horizontaux grâce au développement de drones avec des ailes pliables permettant de consommer moins d'énergie, qui peuvent décoller et atterrir sur de petites parcelles sans nécessiter de grandes parcelles au décollage et à l'atterrissage grâce à leurs ailes.
PCT/TR2017/000109 2017-06-21 2017-10-19 Facilitation du mouvement horizontal de drones WO2018236295A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR2017/09189 2017-06-21
TR2017/09189A TR201709189A2 (tr) 2017-06-21 2017-06-21 Dron'larin yatay yol almalarinin kolaylaştilmasi

Publications (1)

Publication Number Publication Date
WO2018236295A1 true WO2018236295A1 (fr) 2018-12-27

Family

ID=64737764

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2017/000109 WO2018236295A1 (fr) 2017-06-21 2017-10-19 Facilitation du mouvement horizontal de drones

Country Status (2)

Country Link
TR (1) TR201709189A2 (fr)
WO (1) WO2018236295A1 (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3604124A1 (fr) * 2018-08-03 2020-02-05 Aurora Flight Sciences Corporation Appareil combiné en vol et au sol pour un véhicule
CN112141319A (zh) * 2019-06-27 2020-12-29 海鹰航空通用装备有限责任公司 一种m型可变后掠折叠无人机
JPWO2021024323A1 (fr) * 2019-08-02 2021-02-11
JPWO2021053829A1 (fr) * 2019-09-20 2021-03-25
JP7029838B1 (ja) 2021-07-28 2022-03-04 株式会社Acsl 無人航空機
JP7044413B1 (ja) 2020-11-10 2022-03-30 株式会社石川エナジーリサーチ 飛行装置
JP7048131B1 (ja) 2021-07-28 2022-04-05 株式会社Acsl 無人航空機

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1723962A (en) * 1927-03-31 1929-08-06 Fairchild Airplane Mfg Corp Folding wing
CN102233950A (zh) * 2010-04-24 2011-11-09 靳文勇 垂直起降小型飞行器
CN205633014U (zh) * 2016-05-25 2016-10-12 江苏数字鹰科技发展有限公司 一种折叠机翼垂直起降飞机
US20170057630A1 (en) * 2014-02-18 2017-03-02 Iat 21 Innovative Aeronautics Technologies Gmbh Aircraft

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1723962A (en) * 1927-03-31 1929-08-06 Fairchild Airplane Mfg Corp Folding wing
CN102233950A (zh) * 2010-04-24 2011-11-09 靳文勇 垂直起降小型飞行器
US20170057630A1 (en) * 2014-02-18 2017-03-02 Iat 21 Innovative Aeronautics Technologies Gmbh Aircraft
CN205633014U (zh) * 2016-05-25 2016-10-12 江苏数字鹰科技发展有限公司 一种折叠机翼垂直起降飞机

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL268375B1 (en) * 2018-08-03 2023-05-01 Aurora Flight Sciences Corp Combined flight and ground device for vehicles
US11046416B2 (en) 2018-08-03 2021-06-29 Aurora Flight Sciences Corporation Combination flight and ground apparatus for a vehicle
EP3604124A1 (fr) * 2018-08-03 2020-02-05 Aurora Flight Sciences Corporation Appareil combiné en vol et au sol pour un véhicule
IL268375B2 (en) * 2018-08-03 2023-09-01 Aurora Flight Sciences Corp Combined flight and ground device for vehicles
CN112141319A (zh) * 2019-06-27 2020-12-29 海鹰航空通用装备有限责任公司 一种m型可变后掠折叠无人机
CN112141319B (zh) * 2019-06-27 2024-05-03 海鹰航空通用装备有限责任公司 一种m型可变后掠折叠无人机
JPWO2021024323A1 (fr) * 2019-08-02 2021-02-11
JP7438523B2 (ja) 2019-08-02 2024-02-27 株式会社エアロネクスト 飛行体及び飛行体の飛行方法
JPWO2021053829A1 (fr) * 2019-09-20 2021-03-25
JP7398790B2 (ja) 2019-09-20 2023-12-15 株式会社エアロネクスト 飛行体
WO2022102336A1 (fr) * 2020-11-10 2022-05-19 株式会社石川エナジーリサーチ Dispositif de vol
JP2022076852A (ja) * 2020-11-10 2022-05-20 株式会社石川エナジーリサーチ 飛行装置
JP7044413B1 (ja) 2020-11-10 2022-03-30 株式会社石川エナジーリサーチ 飛行装置
WO2023007909A1 (fr) * 2021-07-28 2023-02-02 株式会社Acsl Véhicule aérien sans pilote
JP2023018908A (ja) * 2021-07-28 2023-02-09 株式会社Acsl 無人航空機
JP2023018907A (ja) * 2021-07-28 2023-02-09 株式会社Acsl 無人航空機
WO2023007910A1 (fr) * 2021-07-28 2023-02-02 株式会社Acsl Véhicule aérien sans pilote
JP7048131B1 (ja) 2021-07-28 2022-04-05 株式会社Acsl 無人航空機
JP7029838B1 (ja) 2021-07-28 2022-03-04 株式会社Acsl 無人航空機

Also Published As

Publication number Publication date
TR201709189A2 (tr) 2019-01-21

Similar Documents

Publication Publication Date Title
WO2018236295A1 (fr) Facilitation du mouvement horizontal de drones
US9499266B1 (en) Five-wing aircraft to permit smooth transitions between vertical and horizontal flight
US9682772B2 (en) Multi-stage tilting and multi-rotor flying car
WO2017123346A3 (fr) Aéronef sans pilote doté d'assemblages de plaques d'aile qui assurent une capacité à décollage et d'atterrissage verticaux efficaces
EA201300348A1 (ru) Преобразуемый летательный аппарат вертикального взлета и посадки с поворотным крылом
NZ592991A (en) Aircraft system that enables ground traveling
BR112018009344A2 (pt) veículo aéreo com componentes desdobráveis
US20180312241A1 (en) Landing gear fairing with aerodynamic surfaces for tail sitter aircraft
CN205633014U (zh) 一种折叠机翼垂直起降飞机
US10011350B2 (en) Vertical take-off and landing drag rudder
CN108883828A (zh) 无尾无人驾驶飞行器
CN204489187U (zh) 一种垂直起降水平飞行无人机
WO2020003239A3 (fr) Aéronef à décollage et atterrissage verticaux
CN204037895U (zh) 一种无人机起落架
KR20230163324A (ko) 가변형 주익을 구비하여 수직이착륙이 가능한 글라이더 드론
RU2015135212A (ru) Противокорабельная крылатая ракета - экранолет (пккрэ)
CN204871592U (zh) 旋翼臂内设置可折叠起落杆的无人飞行器
CN204473127U (zh) 后三点式航测固定翼无人机尾轮装置
CN205396533U (zh) 倾转旋翼式无人机机翼及倾转旋翼式无人机
CN105799917B (zh) 一种直升机旋翼桨叶系留方法及直升机旋翼桨叶系留装置
RU2616458C1 (ru) Сверхзвуковой летательный аппарат
CN204996122U (zh) 一种迷你四轴模型整体保护框结构
Masahiko et al. Establishment of Unmanned aerial vehicle systems for Earth system sciences in the polar region
ES2386217B1 (es) Sistema para despegue y aterrizaje de los aviones de forma rápida y con muy poco recorrido
CN106042803A (zh) 两栖无人机

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: 17914793

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: 17914793

Country of ref document: EP

Kind code of ref document: A1