BR112023017877A2 - Motor de aeronave compreendendo um bocal de escape de área variável - Google Patents
Motor de aeronave compreendendo um bocal de escape de área variávelInfo
- Publication number
- BR112023017877A2 BR112023017877A2 BR112023017877A BR112023017877A BR112023017877A2 BR 112023017877 A2 BR112023017877 A2 BR 112023017877A2 BR 112023017877 A BR112023017877 A BR 112023017877A BR 112023017877 A BR112023017877 A BR 112023017877A BR 112023017877 A2 BR112023017877 A2 BR 112023017877A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- engine
- exhaust nozzle
- variable area
- area exhaust
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- 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
- B64C29/0041—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
- B64C29/0066—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 with horizontal jet and jet deflector
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/12—Canard-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Transmission Devices (AREA)
- Exhaust Silencers (AREA)
Abstract
motor de aeronave compreendendo um bocal de escape de área variável. a presente invenção se refere a um motor (310) de uma aeronave de decolagem e pouso vertical (300), em que o motor é configurado para ser móvel em relação a um componente de aeronave (342) da aeronave (300) entre uma posição pairada para decolagem e pouso e uma posição de cruzeiro para voo para frente, em que o motor (310) compreende um componente aerodinâmico (332) tendo pelo menos um elemento aerodinâmico (334) móvel entre uma primeira posição (336) de acordo com um primeiro estado operacional da aeronave e uma segunda posição (338) de acordo com um segundo estado operacional da aeronave, o elemento aerodinâmico definindo uma superfície aerodinâmica em contato com uma corrente de ar que passa pelo motor.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP21161126.4A EP3998196B1 (en) | 2021-03-05 | 2021-03-05 | Aircraft engine comprising a variable area exhaust nozzle |
PCT/EP2022/052238 WO2022184355A1 (en) | 2021-03-05 | 2022-01-31 | Aircraft engine comprising a variable area exhaust nozzle |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112023017877A2 true BR112023017877A2 (pt) | 2023-10-10 |
Family
ID=83067308
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112023017877A BR112023017877A2 (pt) | 2021-03-05 | 2022-01-31 | Motor de aeronave compreendendo um bocal de escape de área variável |
Country Status (5)
Country | Link |
---|---|
US (1) | US11939052B2 (pt) |
JP (1) | JP2024508177A (pt) |
KR (1) | KR20230152673A (pt) |
CN (1) | CN115009523A (pt) |
BR (1) | BR112023017877A2 (pt) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3998197A1 (en) * | 2021-03-05 | 2022-05-18 | Lilium eAircraft GmbH | Engine comprising a movable aerodynamic component |
US20240084762A1 (en) * | 2022-09-14 | 2024-03-14 | Raytheon Technologies Corporation | Vectoring exhaust nozzle for an aircraft powerplant |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3664612A (en) * | 1969-12-22 | 1972-05-23 | Boeing Co | Aircraft engine variable highlight inlet |
GB2393941B (en) * | 1990-01-26 | 2004-09-29 | Rolls Royce Plc | Vectorable variable area nozzle |
FR2768773B1 (fr) * | 1997-09-25 | 1999-11-05 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a coquilles internes |
US6808140B2 (en) | 2002-02-08 | 2004-10-26 | Moller Paul S | Vertical take-off and landing vehicles |
US20110147533A1 (en) * | 2009-12-21 | 2011-06-23 | Honeywell International Inc. | Morphing ducted fan for vertical take-off and landing vehicle |
US9656760B2 (en) * | 2013-11-07 | 2017-05-23 | Sikorsky Aircraft Corporation | Variable geometry helicopter engine inlet |
US10570926B2 (en) * | 2015-12-03 | 2020-02-25 | The Boeing Company | Variable-geometry ducted fan |
US10926874B2 (en) | 2016-01-15 | 2021-02-23 | Aurora Flight Sciences Corporation | Hybrid propulsion vertical take-off and landing aircraft |
US20170355449A1 (en) | 2016-06-10 | 2017-12-14 | Goodrich Aerospace Services Private Limited | Electrical architecture for slat/flap control using smart sensors and effectors |
CN113613997B (zh) | 2019-03-21 | 2024-06-14 | 艾姆索创新私人有限公司 | 竖直起降(vtol)航空器 |
FR3094956B1 (fr) * | 2019-04-10 | 2021-03-05 | Safran | Systeme propulsif pour un aeronef |
US20220018309A1 (en) * | 2020-05-15 | 2022-01-20 | Rohr, Inc. | Passively actuated variable area nozzle for an aircraft propulsion system |
US11492107B2 (en) * | 2020-07-22 | 2022-11-08 | Textron Innovations Inc. | Ducted proprotor systems having adaptive duct geometries |
-
2022
- 2022-01-31 JP JP2023553728A patent/JP2024508177A/ja active Pending
- 2022-01-31 BR BR112023017877A patent/BR112023017877A2/pt unknown
- 2022-01-31 KR KR1020237028926A patent/KR20230152673A/ko unknown
- 2022-03-02 US US17/684,803 patent/US11939052B2/en active Active
- 2022-03-02 CN CN202210206577.2A patent/CN115009523A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
KR20230152673A (ko) | 2023-11-03 |
US20220348320A1 (en) | 2022-11-03 |
CN115009523A (zh) | 2022-09-06 |
US11939052B2 (en) | 2024-03-26 |
JP2024508177A (ja) | 2024-02-22 |
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