WO2022269762A1 - 飛行体 - Google Patents

飛行体 Download PDF

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Publication number
WO2022269762A1
WO2022269762A1 PCT/JP2021/023633 JP2021023633W WO2022269762A1 WO 2022269762 A1 WO2022269762 A1 WO 2022269762A1 JP 2021023633 W JP2021023633 W JP 2021023633W WO 2022269762 A1 WO2022269762 A1 WO 2022269762A1
Authority
WO
WIPO (PCT)
Prior art keywords
frame
aircraft
propeller
airfoil
fuselage
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/JP2021/023633
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
鈴木陽一
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aeronext Inc
Original Assignee
Aeronext Inc
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 Aeronext Inc filed Critical Aeronext Inc
Priority to PCT/JP2021/023633 priority Critical patent/WO2022269762A1/ja
Priority to JP2023529282A priority patent/JP7704458B2/ja
Priority to US18/573,267 priority patent/US12378012B2/en
Priority to CN202221530901.8U priority patent/CN218806519U/zh
Priority to CN202210694369.1A priority patent/CN115503944A/zh
Publication of WO2022269762A1 publication Critical patent/WO2022269762A1/ja
Anticipated expiration legal-status Critical
Priority to JP2025104068A priority patent/JP2025126222A/ja
Ceased legal-status Critical Current

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Classifications

    • 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
    • B64U20/77—Constructional aspects of the UAV body the body being formed integrally with wings or rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • 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
    • 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
    • B64C1/0009—Aerodynamic aspects
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • 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
    • 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
    • B64U30/20—Rotors; Rotor supports
    • 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
    • B64U30/21—Rotary wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors

Definitions

  • the present invention relates to an aircraft.
  • Airplanes in which cylindrical pipes are arranged radially as shown in Fig. 33 (hereinafter collectively referred to as existing airframes), which are widely distributed in the market, do not take relative wind into consideration, resulting in poor flight efficiency. Difficult to improve.
  • Patent Document 1 discloses an aircraft having a shape that improves fuel efficiency when the aircraft cruises in the nose direction.
  • Patent Document 1 by providing an airfoil-shaped main body in an aircraft capable of loading cargo, the resistance against the relative wind from the front of the aircraft can be reduced, and the body can be lifted by the relative wind from the nose direction during flight.
  • a flying object is disclosed that can generate lift in the parts of the flying object and improve the fuel efficiency of the flying object.
  • the aircraft will be able to fly longer than existing aircraft, so it will be possible to expand the range of services such as home delivery and reduce the fuel consumption of the aircraft.
  • FIG. 1 is a conceptual diagram of an aircraft according to the present invention viewed from above;
  • FIG. 2 is another top view of the aircraft of FIG. 1;
  • FIG. 2 is a side view of the aircraft of FIG. 1;
  • FIG. FIG. 2 is a side view of the aircraft of FIG. 1 during cruising;
  • FIG. 2 is a front view of the aircraft of FIG. 1;
  • FIG. 2 is a functional block diagram of the aircraft of FIG. 1;
  • FIG. 2 is a cross-sectional view of the aircraft of FIG. 1 along the line AA';
  • FIG. 2 is a BB' cross-sectional view of the aircraft of FIG. 1;
  • FIG. 10 is a schematic top view of another flying object according to the present invention
  • 20 is another top view of the aircraft of FIG. 19
  • FIG. FIG. 20 is a side view of the aircraft of FIG. 19
  • FIG. 20 is a side view of the aircraft of FIG. 19 during cruising
  • FIG. 20 is a front view of the aircraft of FIG. 19
  • It is an example of the cross-sectional shape of a frame.
  • FIG. 10 is a schematic top view of another flying object according to the present invention
  • 20 is another top view of the aircraft of FIG. 19
  • FIG. FIG. 20 is a side view of the aircraft of FIG. 19
  • FIG. 20 is a side view of the aircraft of FIG. 19 during cruising
  • FIG. 20 is a front view of the aircraft of FIG. 19;
  • FIG. 10 is a schematic top view of another flying object according to the present invention
  • 20 is another top view of the aircraft of FIG. 19
  • FIG. 20 is a side view of the aircraft of FIG. 19
  • FIG. 20 is
  • the frame includes a frame portion located below the radius of rotation of the pull-type rotor; The frame portion is positioned forward of the front frame and has a wider lateral area than the rear frame. 7.
  • the frame includes a frame portion located below the radius of rotation of the pull-type rotor; The frame portion is positioned forward of the front frame and has a wider lateral area than the rear frame. 7.
  • a radial frame as shown in Fig. 33, a ladder frame as shown in Fig. 1, a monocoque frame as shown in Fig. 32, etc. are generally known.
  • a carbon pipe or a metal pipe having a circular or square cross section is used for the radial frame and the ladder-shaped frame.
  • Radial frames are considered to be suitable for use in photography and hobby applications in which the direction of travel is not specified because the drag force of the frame does not change significantly regardless of the direction in which the flying object travels.
  • the frame and mounting parts that make up the flying object 100 are made of materials that are strong enough to withstand flight, takeoff and landing.
  • resin, FRP, etc. are rigid and lightweight, so they are suitable as a constituent material of an aircraft.
  • a metal it is possible to prevent an increase in weight while improving the strength by using a material having a low specific gravity such as aluminum or magnesium.
  • the angle is adjusted to the wind received from the front due to the advance of the aircraft, so that the flight It prevents the frame from increasing drag during body cruising and improves flight efficiency.
  • the thickness in the horizontal direction is not limited, and the thickness in the vertical direction may be increased while the overall thickness in the horizontal direction remains the same, or only a portion of the thickness in the horizontal direction may be extended in the vertical direction. good too.
  • the rear of the aircraft is more affected by the wind than the front, so the nose of the aircraft tends to face upwind (so-called weathervane effect).
  • the weathervane effect is achieved even with this cross-sectional shape.
  • the areas of the front frame 21(f) and the rear frame 21(r) in side view are different, and the area of the rear frame 21(r) in side view is the same as that of the front frame 21(f). ), by making the area wider than the side view, it is possible to assist the change of the nose direction by the automatic control of the aircraft, or to make the nose naturally face upwind even without the automatic control of the nose direction. can do.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Toys (AREA)
  • Body Structure For Vehicles (AREA)
PCT/JP2021/023633 2021-06-22 2021-06-22 飛行体 Ceased WO2022269762A1 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
PCT/JP2021/023633 WO2022269762A1 (ja) 2021-06-22 2021-06-22 飛行体
JP2023529282A JP7704458B2 (ja) 2021-06-22 2021-06-22 飛行体
US18/573,267 US12378012B2 (en) 2021-06-22 2021-06-22 Aerial vehicle
CN202221530901.8U CN218806519U (zh) 2021-06-22 2022-06-20 飞行体
CN202210694369.1A CN115503944A (zh) 2021-06-22 2022-06-20 飞行体
JP2025104068A JP2025126222A (ja) 2021-06-22 2025-06-19 飛行体

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2021/023633 WO2022269762A1 (ja) 2021-06-22 2021-06-22 飛行体

Publications (1)

Publication Number Publication Date
WO2022269762A1 true WO2022269762A1 (ja) 2022-12-29

Family

ID=84500628

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2021/023633 Ceased WO2022269762A1 (ja) 2021-06-22 2021-06-22 飛行体

Country Status (4)

Country Link
US (1) US12378012B2 (https=)
JP (2) JP7704458B2 (https=)
CN (2) CN115503944A (https=)
WO (1) WO2022269762A1 (https=)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPWO2022224630A1 (https=) * 2021-04-23 2022-10-27
JP7704458B2 (ja) * 2021-06-22 2025-07-08 株式会社エアロネクスト 飛行体
US20250153870A1 (en) * 2023-11-15 2025-05-15 Virginia Tech Intellectual Properties, Inc. Novel extended range vertical take-off and landing drone

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150158581A1 (en) * 2013-12-09 2015-06-11 Martin Johannes Fengler Flying machine
CN108557094A (zh) * 2018-04-08 2018-09-21 中博宇图信息科技有限公司 一种多功能无人机
US20180312254A1 (en) * 2017-04-26 2018-11-01 Autel Robotics Co., Ltd. Arm and unmanned aerial vehicle
US20190112047A1 (en) * 2017-10-17 2019-04-18 Aerospace Inventions, LLC Aerodynamic drone using airfoil-designed fuselages and associated parts
JP2019172256A (ja) * 2017-11-06 2019-10-10 株式会社エアロネクスト 飛行体及び飛行体の制御方法

Family Cites Families (77)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6848649B2 (en) * 2000-10-03 2005-02-01 Charles Gilpin Churchman V/STOL biplane aircraft
EP2097317A1 (en) * 2006-11-02 2009-09-09 Severino Manuel Oliveira Raposo System and process of vector propulsion with independent control of three translation and three rotation axis
FR2961041B1 (fr) * 2010-06-02 2012-07-27 Parrot Procede de commande synchronisee des moteurs electriques d'un drone telecommande a voilure tournante tel qu'un quadricoptere
WO2014059549A1 (en) * 2012-10-19 2014-04-24 Aeryon Labs Inc Hovering unmanned aerial vehicle
US10137982B1 (en) * 2014-05-11 2018-11-27 Wing Aviation Llc Propeller units
IL233902B (en) * 2014-07-31 2020-07-30 Israel Aerospace Ind Ltd Propulsion system
US9676477B1 (en) * 2014-08-25 2017-06-13 Amazon Techonlogies, Inc. Adjustable unmanned aerial vehicles
FR3032687B1 (fr) * 2015-02-16 2018-10-12 Hutchinson Aerodyne vtol a soufflante(s) axiale(s) porteuse(s)
US10151546B2 (en) 2015-04-08 2018-12-11 Ra Brands, L.L.C. Shotgun with magazine loading system
KR101767943B1 (ko) * 2015-05-08 2017-08-17 광주과학기술원 추력의 방향 설정이 가능한 멀티로터 타입의 무인 비행체
EP3206947B1 (en) * 2015-06-01 2021-07-07 SZ DJI Technology Co., Ltd. Systems and methods for foldable arms
CN108473198A (zh) * 2015-09-03 2018-08-31 乔伊·音·陈 多转子旋翼飞机飞行器
CA2999270A1 (en) * 2015-09-23 2017-03-30 Walmart Apollo, Llc Systems and methods of delivering products with unmanned delivery aircrafts
EP3184425B1 (en) * 2015-12-21 2018-09-12 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Multirotor aircraft
US11095129B2 (en) * 2016-02-12 2021-08-17 Capacitor Sciences Incorporated Capacitor based power system and unmanned vehicle with the capacitor based power system thereof
US9821909B2 (en) * 2016-04-05 2017-11-21 Swift Engineering, Inc. Rotating wing assemblies for tailsitter aircraft
US11027837B2 (en) * 2016-07-01 2021-06-08 Textron Innovations Inc. Aircraft having thrust to weight dependent transitions
US11608173B2 (en) * 2016-07-01 2023-03-21 Textron Innovations Inc. Aerial delivery systems using unmanned aircraft
US10214285B2 (en) * 2016-07-01 2019-02-26 Bell Helicopter Textron Inc. Aircraft having autonomous and remote flight control capabilities
US10633087B2 (en) * 2016-07-01 2020-04-28 Textron Innovations Inc. Aircraft having hover stability in inclined flight attitudes
US10183746B2 (en) * 2016-07-01 2019-01-22 Bell Helicopter Textron Inc. Aircraft with independently controllable propulsion assemblies
US10597164B2 (en) * 2016-07-01 2020-03-24 Textron Innovations Inc. Aircraft having redundant directional control
US10981661B2 (en) * 2016-07-01 2021-04-20 Textron Innovations Inc. Aircraft having multiple independent yaw authority mechanisms
US10737778B2 (en) * 2016-07-01 2020-08-11 Textron Innovations Inc. Two-axis gimbal mounted propulsion systems for aircraft
US10870487B2 (en) * 2016-07-01 2020-12-22 Bell Textron Inc. Logistics support aircraft having a minimal drag configuration
US10315761B2 (en) * 2016-07-01 2019-06-11 Bell Helicopter Textron Inc. Aircraft propulsion assembly
US10220944B2 (en) * 2016-07-01 2019-03-05 Bell Helicopter Textron Inc. Aircraft having manned and unmanned flight modes
US11104446B2 (en) * 2016-07-01 2021-08-31 Textron Innovations Inc. Line replaceable propulsion assemblies for aircraft
US10301016B1 (en) * 2016-08-09 2019-05-28 Vimana, Inc. Stabilized VTOL flying apparatus and aircraft
CN106184737B (zh) 2016-09-23 2017-06-23 西北工业大学 复合式布局垂直起降飞行器以及垂直起降飞行方法
FR3056555B1 (fr) * 2016-09-29 2018-12-07 Safran Helicopter Engines Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac
AU2017349625A1 (en) * 2016-10-24 2019-05-30 Hybridskys Technology Pty Ltd Hybrid aircraft
EP3366586B1 (en) * 2017-02-27 2020-08-19 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A thrust producing unit with at least two rotor assemblies and a shrouding
CN108622404B (zh) * 2017-03-17 2022-05-24 株式会社理光 飞行器以及飞行系统
AU2018266343B2 (en) * 2017-05-08 2023-09-21 Insitu, Inc. Modular aircraft with vertical takeoff and landing capability
US10442522B2 (en) * 2017-05-26 2019-10-15 Bell Textron Inc. Aircraft with active aerosurfaces
US10661892B2 (en) * 2017-05-26 2020-05-26 Textron Innovations Inc. Aircraft having omnidirectional ground maneuver capabilities
CN110770123A (zh) * 2017-07-05 2020-02-07 深圳市大疆创新科技有限公司 便携式一体化uav
US10081436B1 (en) * 2017-07-06 2018-09-25 Autoflightx International Limited Hybrid VTOL fixed-wing drone
US9957045B1 (en) * 2017-09-03 2018-05-01 Brehnden Daly Stackable drones
JP6707761B2 (ja) * 2017-09-27 2020-06-10 株式会社石川エナジーリサーチ エンジン搭載自立型飛行装置
CN111566008A (zh) * 2017-12-12 2020-08-21 卡梅伦·斯潘塞 可变几何形状垂直起降(vtol)飞行器系统
PH12020551665B1 (en) * 2018-04-24 2024-01-31 Thomas W Melcher Electric vertical takeoff and landing aircraft
WO2019210128A2 (en) * 2018-04-27 2019-10-31 Aai Corporation Variable pitch rotor assembly for electrically driven vectored thrust aircraft applications
US11267570B2 (en) * 2018-05-03 2022-03-08 Joby Aero, Inc. Quad-wing vertical takeoff and landing aircraft
US11794888B1 (en) * 2018-05-18 2023-10-24 Taylor & Lego Holdings, Llc. Unmanned aerial vehicle
CN110654534A (zh) * 2018-06-29 2020-01-07 中光电智能机器人股份有限公司 旋翼机
IL263301B2 (en) * 2018-11-25 2023-09-01 Israel Aerospace Ind Ltd Aircraft and the method of operation of aircraft
US11130570B2 (en) * 2018-11-29 2021-09-28 International Business Machines Corporation Method and system for delivering goods and retrieving reusable totes for drone delivery
US11613353B2 (en) * 2019-02-04 2023-03-28 The Boeing Company Expedited design and qualification of unmanned aerial vehicles
FR3093994B1 (fr) * 2019-03-18 2021-06-11 Airbus Helicopters Procédé et dispositif pour déplacer un centre de gravité d’un aéronef
US11827348B2 (en) * 2019-03-21 2023-11-28 Gurkan ACIKEL VTOL tilting fuselage winged frame multirotor aircraft
US11702202B1 (en) * 2019-05-03 2023-07-18 United States Of America As Represented By The Secretary Of The Air Force Systems, methods and apparatus for multi-arm expansion
EP3757004B1 (en) * 2019-06-27 2023-03-29 Volocopter GmbH Vtol aircraft with wing connecting booms
WO2021095518A1 (ja) * 2019-11-15 2021-05-20 株式会社石川エナジーリサーチ 飛行装置
USD1045668S1 (en) * 2020-08-24 2024-10-08 Sonin Hybrid, LLC Drone
US20230415892A1 (en) * 2020-11-27 2023-12-28 Aeronext Inc. Aircraft, landing method and system
US11975824B2 (en) * 2020-12-11 2024-05-07 California Institute Of Technology Systems for flight control on a multi-rotor aircraft
WO2022159951A1 (en) * 2021-01-19 2022-07-28 California Institute Of Technology Systems and methods for yaw-torque reduction on a multi-rotor aircraft
US12378015B2 (en) * 2021-03-17 2025-08-05 Aeronext Inc. Flight device with end parts displaceable along front end parts of wing parts
JP7770700B2 (ja) * 2021-04-09 2025-11-17 株式会社エアロネクスト 飛行体の着陸方法、飛行体、情報処理装置、プログラム
JPWO2022224630A1 (https=) * 2021-04-23 2022-10-27
WO2022239141A1 (ja) * 2021-05-12 2022-11-17 株式会社エアロネクスト 懸下部材の位置制限装置
US11905007B2 (en) * 2021-06-07 2024-02-20 Archer Aviation, Inc. Flying wing vertical take-off and landing aircraft
JP7704458B2 (ja) * 2021-06-22 2025-07-08 株式会社エアロネクスト 飛行体
US20240336377A1 (en) * 2021-07-13 2024-10-10 Aeronext Inc. Flying vehicle
US12234011B2 (en) * 2021-08-02 2025-02-25 Gerald E. Brown Convertiplane with stopped rotors, and repositionable rotor blades
US12134466B2 (en) * 2021-08-09 2024-11-05 Insitu, Inc. Unmanned aerial vehicles including wing capture devices and related methods
EP4393819A4 (en) * 2021-08-23 2025-07-30 Aeronext Inc Flying object
JP6954708B1 (ja) * 2021-08-26 2021-10-27 株式会社石川エナジーリサーチ エンジン搭載飛行装置
US11649060B2 (en) * 2021-09-14 2023-05-16 Beta Air, Llc Method and system for propulsion in an electric aircraft
US11932387B2 (en) * 2021-12-02 2024-03-19 Textron Innovations Inc. Adaptive transition systems for VTOL aircraft
US11643207B1 (en) * 2021-12-07 2023-05-09 Textron Innovations Inc. Aircraft for transporting and deploying UAVs
US12103673B2 (en) * 2022-01-10 2024-10-01 Textron Innovations Inc. Payload saddle assemblies for use on aircraft
US11639230B1 (en) * 2022-04-30 2023-05-02 Beta Air, Llc System for an integral hybrid electric aircraft
US12145753B2 (en) * 2022-08-09 2024-11-19 Pete Bitar Compact and lightweight drone delivery device called an ArcSpear electric jet drone system having an electric ducted air propulsion system and being relatively difficult to track in flight
US12312085B2 (en) * 2023-05-18 2025-05-27 Performance Drone Works Llc Mechanical release device for unmanned aerial vehicle drop-payload

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150158581A1 (en) * 2013-12-09 2015-06-11 Martin Johannes Fengler Flying machine
US20180312254A1 (en) * 2017-04-26 2018-11-01 Autel Robotics Co., Ltd. Arm and unmanned aerial vehicle
US20190112047A1 (en) * 2017-10-17 2019-04-18 Aerospace Inventions, LLC Aerodynamic drone using airfoil-designed fuselages and associated parts
JP2019172256A (ja) * 2017-11-06 2019-10-10 株式会社エアロネクスト 飛行体及び飛行体の制御方法
CN108557094A (zh) * 2018-04-08 2018-09-21 中博宇图信息科技有限公司 一种多功能无人机

Also Published As

Publication number Publication date
US20240278943A1 (en) 2024-08-22
CN218806519U (zh) 2023-04-07
CN115503944A (zh) 2022-12-23
US12378012B2 (en) 2025-08-05
JPWO2022269762A1 (https=) 2022-12-29
JP2025126222A (ja) 2025-08-28
JP7704458B2 (ja) 2025-07-08

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