BR112021018640A2 - Aeronave de decolagem e pouso na vertical (vtol) - Google Patents
Aeronave de decolagem e pouso na vertical (vtol)Info
- Publication number
- BR112021018640A2 BR112021018640A2 BR112021018640A BR112021018640A BR112021018640A2 BR 112021018640 A2 BR112021018640 A2 BR 112021018640A2 BR 112021018640 A BR112021018640 A BR 112021018640A BR 112021018640 A BR112021018640 A BR 112021018640A BR 112021018640 A2 BR112021018640 A2 BR 112021018640A2
- Authority
- BR
- Brazil
- Prior art keywords
- vtol
- landing
- aircraft
- vertical takeoff
- wing
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
-
- 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
- B64C29/0041—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 jet motors
- B64C29/0075—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 jet motors the motors being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/001—Flying-boats; Seaplanes with means for increasing stability on the water
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
- B64C39/068—Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
- B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2211/00—Modular constructions of airplanes or helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- 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
- Y02T50/30—Wing lift 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
- Y02T50/40—Weight 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
aeronave de decolagem e pouso na vertical (vtol). a presente invenção se refere a uma aeronave de decolagem e pouso na vertical (vtol) (100) com: uma estrutura de asas com asas para frente à esquerda e à direita (20, 22); e asas para trás à esquerda e à direita (30, 32), cada uma das asas direitas (20, 30) conectadas e cada uma das asas esquerdas (22, 32) conectadas em uma configuração de asa fechada; em que cada asa (20, 22, 30, 32) possui um bordo de ataque fixo (100) e no mínimo uma superfície móvel de controle de fuga (110), também em que cada asa (20, 22, 30, 32) possui no mínimo uma nacela do motor (195), a nacela do motor (195) montada pivotantemente na parte inferior do bordo de ataque fixo (100) e presa firmemente à superfície de controle de fuga (110).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2019900954A AU2019900954A0 (en) | 2019-03-21 | Vertical take-off and landing (VTOL) aircraft | |
PCT/AU2020/050261 WO2020186305A1 (en) | 2019-03-21 | 2020-03-19 | Vertical take-off and landing (vtol) aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112021018640A2 true BR112021018640A2 (pt) | 2021-11-23 |
Family
ID=72518885
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112021018640A BR112021018640A2 (pt) | 2019-03-21 | 2020-03-19 | Aeronave de decolagem e pouso na vertical (vtol) |
Country Status (9)
Country | Link |
---|---|
US (1) | US20220161927A1 (pt) |
EP (1) | EP3941828A4 (pt) |
JP (1) | JP7436499B2 (pt) |
CN (1) | CN113613997A (pt) |
AU (1) | AU2020243830A1 (pt) |
BR (1) | BR112021018640A2 (pt) |
CA (1) | CA3133709A1 (pt) |
SG (1) | SG11202109871TA (pt) |
WO (1) | WO2020186305A1 (pt) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20220074826A (ko) * | 2019-05-29 | 2022-06-03 | 크래프트 에어로스페이스 테크놀로지스 인크. | 탠덤 윙과 분산 추진 시스템을 사용한 새로운 항공기 설계 |
KR20210088052A (ko) * | 2020-01-03 | 2021-07-14 | 현대자동차주식회사 | 수직이착륙 에어 모빌리티 |
BR112023004590A2 (pt) * | 2020-09-18 | 2023-04-11 | AMSL Innovations Pty Ltd | Estrutura da aeronave |
EP3998196B1 (en) * | 2021-03-05 | 2023-05-24 | Lilium eAircraft GmbH | Aircraft engine comprising a variable area exhaust nozzle |
KR20230152673A (ko) | 2021-03-05 | 2023-11-03 | 릴리움 게엠베하 | 가변 영역 배기 노즐을 포함하는 항공기 엔진 |
EP3998197A1 (en) * | 2021-03-05 | 2022-05-18 | Lilium eAircraft GmbH | Engine comprising a movable aerodynamic component |
ES1269111Y (es) | 2021-04-18 | 2021-09-17 | Alexandre Emilio Martin | Dispositivo aeronautico de propulsion en flap con motor de helice |
WO2023049497A1 (en) * | 2021-09-27 | 2023-03-30 | Sia Fixar-Aero | Closed polygonal wing member and uses thereof |
USD995399S1 (en) * | 2021-12-06 | 2023-08-15 | Riegl Laser Measurement Systems Gmbh | Pod mountable to an aircraft |
US11827346B1 (en) | 2022-05-04 | 2023-11-28 | Beta Air, Llc | Electric aircraft |
CN114750941B (zh) * | 2022-05-19 | 2024-04-12 | 重庆大学 | 一种自适应消隙倾转机构及倾转旋翼机 |
UA152017U (uk) * | 2022-09-06 | 2022-10-12 | Євген Олександрович Кононихін | Літальний апарат вертикального зльоту і посадки із замкнутим крилом |
CN116573179A (zh) * | 2023-05-31 | 2023-08-11 | 北京航空航天大学云南创新研究院 | 一种盒式布局倾转旋翼微型无人飞行器 |
Family Cites Families (22)
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US2961188A (en) * | 1956-05-02 | 1960-11-22 | Josephine M Taylor | Lift-propulsion device for aircraft |
US3181810A (en) * | 1961-02-27 | 1965-05-04 | Curtiss Wright Corp | Attitude control system for vtol aircraft |
US3179354A (en) * | 1962-04-24 | 1965-04-20 | Alvarez-Calderon Alberto | Convertiplane and apparatus thereof |
US3131873A (en) * | 1963-07-29 | 1964-05-05 | Ryan Aeronautical Co | Ejector flap system for aircraft wing with ducted fan |
US4120470A (en) * | 1976-09-28 | 1978-10-17 | The Boeing Company | Efficient trailing edge system for an aircraft wing |
DE102005016578A1 (de) | 2005-04-11 | 2006-10-19 | Airbus Deutschland Gmbh | Einfachspaltklappe mit gleitender Abweiserklappe und absenkbarem Spoiler |
IL187368A (en) | 2007-11-14 | 2016-04-21 | Vestal Ltd | Wing with flow cap |
ITPI20130073A1 (it) * | 2013-08-08 | 2015-02-09 | Claudio Bottoni | Aeromobile boxwing |
DE102013109392A1 (de) | 2013-08-29 | 2015-03-05 | Airbus Defence and Space GmbH | Schnellfliegendes, senkrechtstartfähiges Fluggerät |
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 |
WO2015143098A2 (en) | 2014-03-18 | 2015-09-24 | Joby Aviation, Inc. | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades |
US10144509B2 (en) * | 2014-06-03 | 2018-12-04 | Juan Gabriel Cruz Ayoroa | High performance VTOL aircraft |
CN204208303U (zh) * | 2014-11-27 | 2015-03-18 | 王航 | 采用襟翼提高升阻比的航模飞机 |
US10370100B2 (en) * | 2015-03-24 | 2019-08-06 | United States Of America As Represented By The Administrator Of Nasa | Aerodynamically actuated thrust vectoring devices |
DE102015207445B4 (de) | 2015-04-23 | 2023-08-17 | Lilium GmbH | Tragfläche für ein Luftfahrzeug und Luftfahrzeug |
CN105270614B (zh) * | 2015-10-30 | 2017-10-10 | 佛山市神风航空科技有限公司 | 一种对称型八轴飞行器 |
US20180162525A1 (en) | 2016-12-08 | 2018-06-14 | Aurora Flight Sciences Corporation | Double-Blown Wing Vertical Takeoff and Landing Aircraft |
US10183746B2 (en) * | 2016-07-01 | 2019-01-22 | Bell Helicopter Textron Inc. | Aircraft with independently controllable propulsion assemblies |
FR3065440B1 (fr) * | 2017-04-24 | 2019-06-07 | Fly-R | Aeronef a voilure rhomboedrique a atterrissage vertical |
US10589842B2 (en) * | 2017-05-25 | 2020-03-17 | Textron Innovations Inc. | Spinners for use on tiltrotor aircraft |
EP3412567A1 (en) * | 2017-06-08 | 2018-12-12 | Airbus Defence and Space GmbH | Aerial vehicle |
CN108408043B (zh) * | 2018-03-02 | 2019-11-29 | 北京航空航天大学 | 一种盒式倾转翼飞行器 |
-
2020
- 2020-03-19 EP EP20774348.5A patent/EP3941828A4/en active Pending
- 2020-03-19 WO PCT/AU2020/050261 patent/WO2020186305A1/en active Application Filing
- 2020-03-19 BR BR112021018640A patent/BR112021018640A2/pt unknown
- 2020-03-19 SG SG11202109871T patent/SG11202109871TA/en unknown
- 2020-03-19 US US17/441,007 patent/US20220161927A1/en active Pending
- 2020-03-19 CA CA3133709A patent/CA3133709A1/en active Pending
- 2020-03-19 CN CN202080023209.3A patent/CN113613997A/zh active Pending
- 2020-03-19 AU AU2020243830A patent/AU2020243830A1/en active Pending
- 2020-03-19 JP JP2021556357A patent/JP7436499B2/ja active Active
Also Published As
Publication number | Publication date |
---|---|
JP7436499B2 (ja) | 2024-02-21 |
EP3941828A1 (en) | 2022-01-26 |
SG11202109871TA (en) | 2021-10-28 |
WO2020186305A1 (en) | 2020-09-24 |
US20220161927A1 (en) | 2022-05-26 |
CN113613997A (zh) | 2021-11-05 |
EP3941828A4 (en) | 2022-11-16 |
AU2020243830A1 (en) | 2021-09-02 |
CA3133709A1 (en) | 2020-09-24 |
JP2022526884A (ja) | 2022-05-27 |
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