PT4337526T - Veículo aéreo não tripulado de rotor de ângulo fixo híbrido com capacidades de descolagem e aterragem vertical - Google Patents

Veículo aéreo não tripulado de rotor de ângulo fixo híbrido com capacidades de descolagem e aterragem vertical

Info

Publication number
PT4337526T
PT4337526T PT217357607T PT21735760T PT4337526T PT 4337526 T PT4337526 T PT 4337526T PT 217357607 T PT217357607 T PT 217357607T PT 21735760 T PT21735760 T PT 21735760T PT 4337526 T PT4337526 T PT 4337526T
Authority
PT
Portugal
Prior art keywords
aerial vehicle
unmanned aerial
fixed angle
rotor unmanned
vertical takeoff
Prior art date
Application number
PT217357607T
Other languages
English (en)
Original Assignee
Sia Fixar Aero
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 Sia Fixar Aero filed Critical Sia Fixar Aero
Publication of PT4337526T publication Critical patent/PT4337526T/pt

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
    • B64C29/0025—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 fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/20—Vertical take-off and landing [VTOL] aircraft
    • 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
    • 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
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
PT217357607T 2021-06-15 2021-06-15 Veículo aéreo não tripulado de rotor de ângulo fixo híbrido com capacidades de descolagem e aterragem vertical PT4337526T (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2021/055258 WO2022263879A1 (en) 2021-06-15 2021-06-15 Hybrid fixed angle rotor unmanned aerial vehicle with vertical takeoff and landing capabilities

Publications (1)

Publication Number Publication Date
PT4337526T true PT4337526T (pt) 2026-01-29

Family

ID=76662508

Family Applications (1)

Application Number Title Priority Date Filing Date
PT217357607T PT4337526T (pt) 2021-06-15 2021-06-15 Veículo aéreo não tripulado de rotor de ângulo fixo híbrido com capacidades de descolagem e aterragem vertical

Country Status (15)

Country Link
US (1) US12397935B2 (pt)
EP (2) EP4337526B1 (pt)
JP (2) JP7741207B2 (pt)
KR (1) KR20240022565A (pt)
CN (1) CN117545694A (pt)
AU (1) AU2021451146A1 (pt)
BR (1) BR112023026139A2 (pt)
CA (1) CA3223043A1 (pt)
FI (1) FI4337526T3 (pt)
IL (2) IL322731A (pt)
LT (1) LT4337526T (pt)
PT (1) PT4337526T (pt)
RS (1) RS67708B1 (pt)
WO (1) WO2022263879A1 (pt)
ZA (1) ZA202311519B (pt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102787878B1 (ko) * 2024-07-02 2025-03-26 함명래 회전기립식 수직이착륙 텐덤기
US20250375991A1 (en) * 2025-08-22 2025-12-11 Guanhao Wu Dual-Mode Vehicle with Selectively Attachable Flight Module and Energy Transmission Control

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9493235B2 (en) * 2002-10-01 2016-11-15 Dylan T X Zhou Amphibious vertical takeoff and landing unmanned device
CN101885295A (zh) * 2010-07-19 2010-11-17 杨朝习 陆空两用飞行器
DE102012002310A1 (de) 2012-02-06 2013-08-08 Airbus Operations Gmbh Flugzeug mit mindestens zwei Flugzeugrümpfen und einer ersten Tragflügelanordnung mit mindestens zwei nicht verbundenen Tragflügelabschnitten
WO2015115913A1 (en) 2014-01-30 2015-08-06 Global Aerial Platforms Limited Multipurpose aircraft
US10183747B1 (en) * 2016-08-26 2019-01-22 Kitty Hawk Corporation Multicopter with boom-mounted rotors
US10577091B2 (en) * 2017-04-24 2020-03-03 Bcg Digital Ventures Gmbh Vertical take-off and landing aircraft
USD822579S1 (en) 2017-04-24 2018-07-10 AFS-DV VTOL Technologies Corporation Aircraft
AU2018355573B2 (en) * 2017-10-27 2024-10-03 Elroy Air, Inc. Compound multi-copter aircraft
US20200317332A1 (en) 2017-12-22 2020-10-08 Neoptera Ltd Tandem wing tail-sitting aircraft with tilting body
WO2020141513A2 (en) * 2018-12-31 2020-07-09 Polarity Mobility Av Ltd. Evtol aircraft
CN114430725A (zh) * 2019-05-21 2022-05-03 杰欧比飞行有限公司 使用固定前倾旋翼来模拟刚性机翼空气动力学的垂直起降飞行器
GB2586835B (en) * 2019-09-05 2022-04-27 Rallings Alan Motor vehicles for use on the ground and in the air
CN212022972U (zh) 2019-12-21 2020-11-27 京飞(菏泽)航天科技有限公司 一种垂直起降飞行器
WO2022008061A1 (de) * 2020-07-10 2022-01-13 Hw Aviation Ag Hybrid-drohne zur landung an vertikalen strukturen
JP7610444B2 (ja) 2021-03-25 2025-01-08 本田技研工業株式会社 航空機
US12151801B2 (en) * 2021-03-25 2024-11-26 Textron Systems Corporation Flight control arrangement using separate fixed-wing and VTOL control modules
US12037111B2 (en) * 2021-09-16 2024-07-16 Textron Innovations Inc. Quad tilt rotor unmanned aircraft
US20230382521A1 (en) * 2022-05-26 2023-11-30 Deng Huang Structural features of vertical take-off and landing (vtol) aerial vehicle

Also Published As

Publication number Publication date
JP2025179171A (ja) 2025-12-09
US12397935B2 (en) 2025-08-26
WO2022263879A1 (en) 2022-12-22
EP4628404A1 (en) 2025-10-08
LT4337526T (lt) 2026-01-12
IL309301A (en) 2024-02-01
IL322731A (en) 2025-10-01
CA3223043A1 (en) 2022-12-22
EP4337526A1 (en) 2024-03-20
ZA202311519B (en) 2025-11-26
RS67708B1 (sr) 2026-02-27
EP4337526B1 (en) 2025-11-19
JP7741207B2 (ja) 2025-09-17
FI4337526T3 (fi) 2026-01-26
KR20240022565A (ko) 2024-02-20
BR112023026139A2 (pt) 2024-03-05
US20240286772A1 (en) 2024-08-29
CN117545694A (zh) 2024-02-09
AU2021451146A1 (en) 2024-01-04
JP2024525179A (ja) 2024-07-10

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