JP7738337B2 - 垂直離着陸性能を有する航空機の制御 - Google Patents

垂直離着陸性能を有する航空機の制御

Info

Publication number
JP7738337B2
JP7738337B2 JP2022568826A JP2022568826A JP7738337B2 JP 7738337 B2 JP7738337 B2 JP 7738337B2 JP 2022568826 A JP2022568826 A JP 2022568826A JP 2022568826 A JP2022568826 A JP 2022568826A JP 7738337 B2 JP7738337 B2 JP 7738337B2
Authority
JP
Japan
Prior art keywords
aircraft
wings
processor
thrust
wing
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.)
Active
Application number
JP2022568826A
Other languages
English (en)
Japanese (ja)
Other versions
JP2023526056A5 (cg-RX-API-DMAC7.html
JP2023526056A (ja
Inventor
ペトロフ,ヴァル
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.)
PteroDynamics Inc
Original Assignee
PteroDynamics 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 PteroDynamics Inc filed Critical PteroDynamics Inc
Publication of JP2023526056A publication Critical patent/JP2023526056A/ja
Publication of JP2023526056A5 publication Critical patent/JP2023526056A5/ja
Application granted granted Critical
Publication of JP7738337B2 publication Critical patent/JP7738337B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/102—Simultaneous control of position or course in three dimensions specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/12—Static balancing; Determining position of centre of gravity
    • G01M1/122—Determining position of centre of gravity
    • G01M1/125—Determining position of centre of gravity of aircraft
    • G01M1/127—Determining position of centre of gravity of aircraft during the flight
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/20—Control system inputs
    • G05D1/24—Arrangements for determining position or orientation
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/40—Control within particular dimensions
    • G05D1/46—Control of position or course in three dimensions [3D]
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/40—Control within particular dimensions
    • G05D1/49—Control of attitude, i.e. control of roll, pitch or yaw
    • G05D1/495—Control of attitude, i.e. control of roll, pitch or yaw to ensure stability
    • G05D1/496—Control of attitude, i.e. control of roll, pitch or yaw to ensure stability compensating for coupling between different axes of movement
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/60—Intended control result
    • G05D1/617—Safety or protection, e.g. defining protection zones around obstacles or avoiding hazards
    • G05D1/621—Safety or protection, e.g. defining protection zones around obstacles or avoiding hazards responding to weather conditions, e.g. storms or wind shear
    • 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
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2109/00—Types of controlled vehicles
    • G05D2109/20—Aircraft, e.g. drones
    • G05D2109/22—Aircraft, e.g. drones with fixed wings
    • G05D2109/23—Vertical take-off and landing [VTOL] aircraft; Short take-off and landing [STOL, STOVL] aircraft
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2109/00—Types of controlled vehicles
    • G05D2109/20—Aircraft, e.g. drones
    • G05D2109/22—Aircraft, e.g. drones with fixed wings
    • G05D2109/23—Vertical take-off and landing [VTOL] aircraft; Short take-off and landing [STOL, STOVL] aircraft
    • G05D2109/24—Convertible aircraft, e.g. tiltrotor aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Circuits Of Receivers In General (AREA)
  • Automatic Assembly (AREA)
  • Transmission Devices (AREA)
JP2022568826A 2020-05-14 2021-05-13 垂直離着陸性能を有する航空機の制御 Active JP7738337B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US202063024693P 2020-05-14 2020-05-14
US63/024,693 2020-05-14
PCT/US2021/032258 WO2021242535A2 (en) 2020-05-14 2021-05-13 Control of aircraft with vertical take-off and landing capabilities

Publications (3)

Publication Number Publication Date
JP2023526056A JP2023526056A (ja) 2023-06-20
JP2023526056A5 JP2023526056A5 (cg-RX-API-DMAC7.html) 2024-05-22
JP7738337B2 true JP7738337B2 (ja) 2025-09-12

Family

ID=78745069

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2022568826A Active JP7738337B2 (ja) 2020-05-14 2021-05-13 垂直離着陸性能を有する航空機の制御

Country Status (10)

Country Link
US (1) US12455574B2 (cg-RX-API-DMAC7.html)
EP (1) EP4149835A4 (cg-RX-API-DMAC7.html)
JP (1) JP7738337B2 (cg-RX-API-DMAC7.html)
KR (1) KR20230010733A (cg-RX-API-DMAC7.html)
CN (1) CN115916645B (cg-RX-API-DMAC7.html)
AU (1) AU2021278828A1 (cg-RX-API-DMAC7.html)
BR (1) BR112022023131A2 (cg-RX-API-DMAC7.html)
CA (1) CA3178662A1 (cg-RX-API-DMAC7.html)
IL (1) IL298177B2 (cg-RX-API-DMAC7.html)
WO (1) WO2021242535A2 (cg-RX-API-DMAC7.html)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2621982A (en) * 2022-08-24 2024-03-06 Airbus Operations Ltd Aircraft attitude controller and wing system
US20250346373A1 (en) * 2024-05-10 2025-11-13 Lockheed Martin Corporation Airspeed driven tilt angle for electric tiltrotor aircraft
KR102802164B1 (ko) * 2024-09-05 2025-05-02 주식회사 에이디시스템 접익형 수직 이착륙 무인 비행 장치
KR102966417B1 (ko) * 2025-10-15 2026-05-19 주식회사 지케이피엠씨 튜브형 발사체를 이용하는 인공지능 기반의 드론 운용 시스템 및 방법
KR102966423B1 (ko) * 2025-10-17 2026-05-18 주식회사 지케이피엠씨 접이식 고정익 드론의 날개 전개 제어 장치 및 방법

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170097644A1 (en) 2015-08-19 2017-04-06 Sikorsky Aircraft Corporation Hover attitude trim for vehicle
US20180149545A1 (en) 2016-11-30 2018-05-31 Sikorsky Aircraft Corporation Systems and methods for determining aircraft center-of-gravity
US20190225333A1 (en) 2017-04-27 2019-07-25 PteroDynamics, Inc. Vertical Takeoff and Landing Airframe

Family Cites Families (74)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1556414A (en) 1925-07-11 1925-10-06 Blackburn Aeroplane & Motor Co Aeroplane with folding wings
US1848389A (en) 1929-02-14 1932-03-08 Sikorsky Aviat Corp Aircraft, especially aircraft of the direct lift amphiblan type and means of constructing and operating the same
US1793056A (en) 1929-08-01 1931-02-17 Cairns Dev Company Folding wing
US1846992A (en) 1931-05-05 1932-02-23 Decker Virgil Cecil Four winged aeroplane
US2572421A (en) 1947-09-20 1951-10-23 Jr Edmund Abel Aircraft folding wing construction
US2674422A (en) 1949-05-12 1954-04-06 Pellarini Luigi Folding wing for roadable aircraft
US3081964A (en) 1958-12-08 1963-03-19 Boeing Co Airplanes for vertical and/or short take-off and landing
US3179354A (en) 1962-04-24 1965-04-20 Alvarez-Calderon Alberto Convertiplane and apparatus thereof
US3231221A (en) 1964-03-10 1966-01-25 Haviland H Platt Vertical take-off airplanes
US3246861A (en) 1964-03-30 1966-04-19 Curci Alfred Convertible aircraft
US3519224A (en) 1966-03-18 1970-07-07 Turbo Circle Wing Inc Vertical takeoff and landing aircraft
US3439890A (en) 1967-05-15 1969-04-22 Raymond M Stits Folding wing airplane
US3666209A (en) 1970-02-24 1972-05-30 Boeing Co V/stol aircraft with variable tilt wing
US3937424A (en) 1973-11-16 1976-02-10 Vereinigte Flugtechnische Werke-Fokker Gmbh Electrically powered aircraft
US4691878A (en) * 1985-11-06 1987-09-08 The United States Of America As Represented By The Secretary Of The Navy Tilt-rotor wing fold mechanism and method
DE3907063A1 (de) * 1989-03-04 1990-09-13 Messerschmitt Boelkow Blohm Solargeneratoranordnung fuer teil- und vollentfaltung
US5094412A (en) 1989-10-13 1992-03-10 Bell Helicopter Textron Inc. Flaperon system for tilt rotor wings
BR9106696A (pt) 1990-07-25 1993-06-08 Sadleir Vtol Aircraft Co Pty L Unidade de empuxo para aeronave do tipo vtol
US5192037A (en) 1991-08-23 1993-03-09 Mcdonnell Douglas Corporation Double-pivoting deployment system for aerosurfaces
US5242132A (en) * 1992-03-31 1993-09-07 Edward Wukowitz Multi-hulled aircraft/boat
US5405105A (en) * 1993-05-28 1995-04-11 Hudson Valley V/Stol Aircraft, Inc. Tilt wing VTOL aircraft
US5765783A (en) 1994-03-04 1998-06-16 The Boeing Company Vertically launchable and recoverable winged aircraft
US5839691A (en) 1996-05-22 1998-11-24 Lariviere; Jean Soulez Vertical takeoff and landing aircraft
US6382556B1 (en) * 1999-12-20 2002-05-07 Roger N. C. Pham VTOL airplane with only one tiltable prop-rotor
US9776715B2 (en) 2002-10-01 2017-10-03 Andrew H B Zhou Amphibious vertical takeoff and landing unmanned device
WO2008065664A2 (en) * 2006-11-30 2008-06-05 Urban Aeronautics Ltd. Flight control cockpit modes in ducted fan vtol vehicles
US8157206B2 (en) 2008-06-11 2012-04-17 Icon Aircraft, Inc. Two-motion wing-fold mechanism with independent load path
EP2303610B1 (en) 2008-07-28 2020-01-08 Fleck Future Concepts GmbH Combined air, water and road vehicle
US8366049B2 (en) 2008-10-09 2013-02-05 Abe Karem Hover delivery of cabin payload in tilt-rotor and tilt-wing aircraft
RU2403177C1 (ru) 2009-07-31 2010-11-10 Общество С Ограниченной Ответственностью "Научно-Производственная Фирма "Сигма-Тс" Самолет со складываемым крылом и устройство складывания крыла самолета
FR2948628B1 (fr) * 2009-08-03 2012-02-03 Airbus Operations Sas Avion a controle en lacet par trainee differentielle
US8162253B2 (en) 2009-08-19 2012-04-24 Seiford Sr Donald S Convertible vehicle for road, air, and water usage
US8800912B2 (en) 2009-10-09 2014-08-12 Oliver Vtol, Llc Three wing, six-tilt propulsion unit, VTOL aircraft
US20130008997A1 (en) 2010-03-24 2013-01-10 Gentile Francis X Combination ground vehicle and helicopter and fixed wing aircraft
FR2959208B1 (fr) * 2010-04-22 2012-05-25 Eurl Jmdtheque Engin gyropendulaire a propulsion compensatoire et collimation de gradient fluidique multi-milieux multimodal a decollage et atterrissage vertical
WO2011140551A1 (en) * 2010-05-07 2011-11-10 Ohio University Multi-modal vehicle
EP2625098A4 (en) 2010-10-06 2018-01-17 Donald Orval Shaw Aircraft with wings and movable propellers
IL217501A (en) 2012-01-12 2017-09-28 Israel Aerospace Ind Ltd A method and system for maneuvering aircraft
US20130206921A1 (en) 2012-02-15 2013-08-15 Aurora Flight Sciences Corporation System, apparatus and method for long endurance vertical takeoff and landing vehicle
US9914523B2 (en) 2012-10-30 2018-03-13 The Boeing Company Wing hinge assembly including hinged torque boxes
US8849480B2 (en) * 2013-03-01 2014-09-30 Honeywell International Inc. Aircraft gross weight and center of gravity validator
CN105121188B (zh) 2013-03-15 2019-03-15 特力飞车股份有限公司 具有垂直起飞和固定翼巡航能力的组合的飞行/行驶车辆
GB201307739D0 (en) 2013-04-30 2013-06-12 Reiter Johannes Aircraft for vertical take-off and landing with hinged and bendable wings
US10099770B2 (en) 2013-07-26 2018-10-16 Icon Aircraft, Inc. Manuel wing-fold mechanism
US10071801B2 (en) 2013-08-13 2018-09-11 The United States Of America As Represented By The Administrator Of Nasa Tri-rotor aircraft capable of vertical takeoff and landing and transitioning to forward flight
US9567075B2 (en) 2014-02-10 2017-02-14 Northrop Grumman Systems Corporation Tilt wing aerial vehicle
US9694911B2 (en) 2014-03-18 2017-07-04 Joby Aviation, Inc. Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
EP3140188B1 (en) 2014-05-08 2018-12-19 Northrop Grumman Systems Corporation Vertical takeoff and landing (vtol) unmanned aerial vehicle (uav)
US10279903B2 (en) 2014-05-20 2019-05-07 Sikorsky Aircraft Corporation In-flight reconfigurable aircraft tail
US9676488B2 (en) 2014-06-10 2017-06-13 Sikorsky Aircraft Corporation Dual dissimilar engines for an aircraft
US9475585B2 (en) 2014-06-25 2016-10-25 The Boeing Company Tilt-rotor vertical-lift aircraft
US9550561B1 (en) * 2014-08-11 2017-01-24 Amazon Technologies, Inc. Determining center of gravity of an automated aerial vehicle and a payload
US20170267338A1 (en) * 2014-10-01 2017-09-21 Sikorsky Aircraft Corporation Acoustic signature variation of aircraft utilizing a clutch
US9550567B1 (en) 2014-10-27 2017-01-24 Amazon Technologies, Inc. In-flight reconfigurable hybrid unmanned aerial vehicle
US9464958B2 (en) * 2015-01-16 2016-10-11 Bell Helicopter Textron Inc. Dynamic center of gravity determination
US9714090B2 (en) 2015-06-12 2017-07-25 Sunlight Photonics Inc. Aircraft for vertical take-off and landing
US10059442B2 (en) 2015-07-10 2018-08-28 Zenon Dragan Vertical takeoff and landing unmanned aircraft system
CN105035319A (zh) * 2015-07-27 2015-11-11 江阴市翔诺电子科技有限公司 一种新型垂直起降飞行器及其控制方法
EP3347269B1 (en) 2015-09-11 2019-07-31 Northrop Grumman Systems Corporation Vertical takeoff and landing (vtol) unmanned aerial vehicle (uav)
US10464684B2 (en) 2016-02-01 2019-11-05 Bell Textron Inc. Tapered sockets for aircraft engine mount assemblies
US10513325B2 (en) * 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Joint member for a composite wing structure
US9821909B2 (en) 2016-04-05 2017-11-21 Swift Engineering, Inc. Rotating wing assemblies for tailsitter aircraft
US10317914B2 (en) * 2016-04-18 2019-06-11 Latitude Engineering, LLC Wind finding and compensation for unmanned aircraft systems
US10246185B2 (en) 2016-06-27 2019-04-02 Panasonic Intellectual Property Management Co., Ltd. Aircraft system and method for vertical takeoff and landing
WO2018032425A1 (zh) * 2016-08-17 2018-02-22 深圳市大疆创新科技有限公司 无人机及控制无人机姿态的控制方法、控制装置
EP3521163B1 (en) * 2016-10-03 2021-09-08 Aeronext Inc. Delivery rotary-wing aircraft
DE102016119152B4 (de) * 2016-10-07 2018-12-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Windmessung mittels eines Multikopters
FR3065440B1 (fr) * 2017-04-24 2019-06-07 Fly-R Aeronef a voilure rhomboedrique a atterrissage vertical
US10442522B2 (en) * 2017-05-26 2019-10-15 Bell Textron Inc. Aircraft with active aerosurfaces
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
US11053646B2 (en) * 2018-02-14 2021-07-06 Lily Helipads, LLC Helicopter and VTOL aircraft landing pad information sheet
US11708157B2 (en) * 2018-09-11 2023-07-25 Eve Uam, Llc Vertical take-off and landing (VTOL) aircraft with cruise rotor positioning control for minimum drag
US11541987B2 (en) * 2019-08-19 2023-01-03 Textron Innovations Inc. Aircraft with foldable tail
US11459117B1 (en) * 2019-09-23 2022-10-04 Amazon Technologies, Inc. Drone-based cameras to detect wind direction for landing

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170097644A1 (en) 2015-08-19 2017-04-06 Sikorsky Aircraft Corporation Hover attitude trim for vehicle
US20180149545A1 (en) 2016-11-30 2018-05-31 Sikorsky Aircraft Corporation Systems and methods for determining aircraft center-of-gravity
US20190225333A1 (en) 2017-04-27 2019-07-25 PteroDynamics, Inc. Vertical Takeoff and Landing Airframe

Also Published As

Publication number Publication date
US12455574B2 (en) 2025-10-28
CN115916645B (zh) 2026-07-21
CA3178662A1 (en) 2021-12-02
IL298177B1 (en) 2026-01-01
EP4149835A4 (en) 2024-04-17
BR112022023131A2 (pt) 2023-02-07
IL298177A (en) 2023-01-01
EP4149835A2 (en) 2023-03-22
AU2021278828A1 (en) 2023-01-19
WO2021242535A2 (en) 2021-12-02
KR20230010733A (ko) 2023-01-19
AU2021278828A8 (en) 2023-02-16
JP2023526056A (ja) 2023-06-20
US20230195143A1 (en) 2023-06-22
IL298177B2 (en) 2026-05-01
WO2021242535A3 (en) 2022-03-10
CN115916645A (zh) 2023-04-04

Similar Documents

Publication Publication Date Title
US20240217655A1 (en) Air vehicle and method of operation of air vehicle
US20230303244A1 (en) High speed multi-rotor vertical takeoff and landing aircraft
AU2019203204B2 (en) Vertical takeoff and landing (VTOL) air vehicle
US10144509B2 (en) High performance VTOL aircraft
US10538321B2 (en) Tri-rotor aircraft capable of vertical takeoff and landing and transitioning to forward flight
US10850835B2 (en) Unmanned aerial vehicle with monolithic wing and twin-rotor propulsion/lift modules
EP3140188B1 (en) Vertical takeoff and landing (vtol) unmanned aerial vehicle (uav)
US9616995B2 (en) Aircraft and methods for operating an aircraft
US12455574B2 (en) Control of aircraft with vertical take-off and landing capabilities
KR102135285B1 (ko) 수직 이착륙 고정익 무인기
US11845544B2 (en) Foldable aircraft
WO2016028358A2 (en) High Performance VTOL Aircraft
Ang et al. Design and implementation of a thrust-vectored unmanned tail-sitter with reconfigurable wings

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20230112

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20240510

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20240510

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20250128

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20250204

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20250507

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20250729

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20250826

R150 Certificate of patent or registration of utility model

Ref document number: 7738337

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150