BRPI1013173A2 - nacela de recepção de um motor de aeronave - Google Patents
nacela de recepção de um motor de aeronaveInfo
- Publication number
- BRPI1013173A2 BRPI1013173A2 BRPI1013173A BRPI1013173A BRPI1013173A2 BR PI1013173 A2 BRPI1013173 A2 BR PI1013173A2 BR PI1013173 A BRPI1013173 A BR PI1013173A BR PI1013173 A BRPI1013173 A BR PI1013173A BR PI1013173 A2 BRPI1013173 A2 BR PI1013173A2
- Authority
- BR
- Brazil
- Prior art keywords
- cockpit
- receiving
- aircraft engine
- aircraft
- engine
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- 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
- 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
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P5/00—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors
- H02P5/74—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors controlling two or more ac dynamo-electric motors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
- H02P9/007—Control circuits for doubly fed generators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P2101/00—Special adaptation of control arrangements for generators
- H02P2101/30—Special adaptation of control arrangements for generators for aircraft
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P2207/00—Indexing scheme relating to controlling arrangements characterised by the type of motor
- H02P2207/01—Asynchronous machines
-
- 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
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0902578A FR2946014B1 (fr) | 2009-05-28 | 2009-05-28 | Nacelle de moteur d'aeronef comportant un capot mobile mu par des moteurs electriques |
PCT/EP2010/056924 WO2010136369A1 (fr) | 2009-05-28 | 2010-05-19 | Nacelle de moteur d'aeronef comportant un capot mobile mu par des moteurs electriques |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI1013173A2 true BRPI1013173A2 (pt) | 2016-04-05 |
Family
ID=41569888
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI1013173A BRPI1013173A2 (pt) | 2009-05-28 | 2010-05-19 | nacela de recepção de um motor de aeronave |
Country Status (8)
Country | Link |
---|---|
US (1) | US8907595B2 (pt) |
EP (1) | EP2435307B1 (pt) |
CN (1) | CN102448822B (pt) |
BR (1) | BRPI1013173A2 (pt) |
CA (1) | CA2761761C (pt) |
FR (1) | FR2946014B1 (pt) |
RU (1) | RU2486107C1 (pt) |
WO (1) | WO2010136369A1 (pt) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2920204B1 (fr) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | Procede et systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur |
CN103129740B (zh) * | 2013-02-07 | 2015-07-15 | 玉环天润航空机械制造有限公司 | 动力舱整流罩的锁闭机构 |
US10384774B2 (en) | 2016-09-08 | 2019-08-20 | General Electric Company | Tiltrotor propulsion system for an aircraft |
US10384773B2 (en) | 2016-09-08 | 2019-08-20 | General Electric Company | Tiltrotor propulsion system for an aircraft |
US10252797B2 (en) | 2016-09-08 | 2019-04-09 | General Electric Company | Tiltrotor propulsion system for an aircraft |
US10392106B2 (en) | 2016-09-08 | 2019-08-27 | General Electric Company | Tiltrotor propulsion system for an aircraft |
US10822101B2 (en) * | 2017-07-21 | 2020-11-03 | General Electric Company | Vertical takeoff and landing aircraft having a forward thrust propulsor |
US20210122466A1 (en) * | 2019-10-28 | 2021-04-29 | Uber Technologies, Inc. | Aerial vehicle with differential control mechanisms |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1326910A (fr) * | 1962-06-27 | 1963-05-10 | Westinghouse Electric Corp | Commande de moteur |
US3688171A (en) * | 1971-08-13 | 1972-08-29 | Gen Motors Corp | Induction motor braking system |
GB9301457D0 (en) * | 1993-01-26 | 1993-03-17 | Short Brothers Plc | An aircraft propulsuve power unit |
FR2711862B1 (fr) * | 1993-10-25 | 1995-12-01 | Centre Nat Rech Scient | Système d'alimentation de n moteurs asynchrones. |
FR2755730B1 (fr) * | 1996-11-14 | 1999-01-08 | Hispano Suiza Sa | Systeme de commande electrique pour inverseur de poussee de turboreacteur |
US6340135B1 (en) * | 2000-05-30 | 2002-01-22 | Rohr, Inc. | Translating independently mounted air inlet system for aircraft turbofan jet engine |
RU2204507C1 (ru) * | 2002-06-19 | 2003-05-20 | Открытое акционерное общество "Казанский вертолётный завод" | Капот двигателя летательного аппарата |
-
2009
- 2009-05-28 FR FR0902578A patent/FR2946014B1/fr not_active Expired - Fee Related
-
2010
- 2010-05-19 US US13/320,360 patent/US8907595B2/en not_active Expired - Fee Related
- 2010-05-19 BR BRPI1013173A patent/BRPI1013173A2/pt not_active IP Right Cessation
- 2010-05-19 EP EP10723048.4A patent/EP2435307B1/fr active Active
- 2010-05-19 RU RU2011153208/11A patent/RU2486107C1/ru not_active IP Right Cessation
- 2010-05-19 CN CN201080023824.0A patent/CN102448822B/zh not_active Expired - Fee Related
- 2010-05-19 WO PCT/EP2010/056924 patent/WO2010136369A1/fr active Application Filing
- 2010-05-19 CA CA2761761A patent/CA2761761C/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
WO2010136369A1 (fr) | 2010-12-02 |
EP2435307B1 (fr) | 2013-07-10 |
US20120107109A1 (en) | 2012-05-03 |
CA2761761C (fr) | 2013-09-17 |
US8907595B2 (en) | 2014-12-09 |
CN102448822A (zh) | 2012-05-09 |
FR2946014B1 (fr) | 2011-05-20 |
CN102448822B (zh) | 2014-01-22 |
CA2761761A1 (fr) | 2010-12-02 |
FR2946014A1 (fr) | 2010-12-03 |
RU2486107C1 (ru) | 2013-06-27 |
EP2435307A1 (fr) | 2012-04-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B08F | Application fees: application dismissed [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 9A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2516 DE 26-03-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |