BR112015022654A2 - trava de reversor de empuxo de motor - Google Patents
trava de reversor de empuxo de motorInfo
- Publication number
- BR112015022654A2 BR112015022654A2 BR112015022654A BR112015022654A BR112015022654A2 BR 112015022654 A2 BR112015022654 A2 BR 112015022654A2 BR 112015022654 A BR112015022654 A BR 112015022654A BR 112015022654 A BR112015022654 A BR 112015022654A BR 112015022654 A2 BR112015022654 A2 BR 112015022654A2
- Authority
- BR
- Brazil
- Prior art keywords
- slot
- thrust reverser
- sidewall surface
- engine thrust
- pin
- 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
- F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
-
- 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
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/56—Kinematic linkage, i.e. transmission of position using cams or eccentrics
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49947—Assembling or joining by applying separate fastener
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Transmission Devices (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Abstract
resumo trava de reversor de empuxo de motor a invenção refere-se a um sistema de trava de reversor de empuxo de motor de aeronave (100) que inclui um membro de captura de pino (102). o membro de captura de pino inclui um corpo que é girável ao redor de um eixo geométrico definido por um pivô (104) que se estende pelo corpo. o corpo inclui uma superfície interior que define uma fenda (150). a fenda tem uma abertura que é dimensionada para receber um pino (110) na fenda. um lado da fenda inclui uma superfície de parede lateral projetada que se projeta na fenda em direção a uma outra superfície de parede lateral da fenda. a superfície de parede lateral projetada define um ápice (206) entre as extremidades aberta e fechada da fenda. entre o ápice e a extremidade fechada da fenda, a superfície de parede lateral projetada é voltada para o eixo geométrico rotacional.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/827,192 US9109536B2 (en) | 2013-03-14 | 2013-03-14 | Engine thrust reverser lock |
PCT/US2014/020557 WO2014158852A1 (en) | 2013-03-14 | 2014-03-05 | Engine thrust reverser lock |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112015022654A2 true BR112015022654A2 (pt) | 2017-07-18 |
BR112015022654A8 BR112015022654A8 (pt) | 2019-11-26 |
Family
ID=50349920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015022654A BR112015022654A8 (pt) | 2013-03-14 | 2014-03-05 | sistema de trava de reversor de empuxo de motor de aeronave, sistema de travamento de reversor de empuxo de motor de aeronave e trava de reversor de empuxo de motor de aeronave |
Country Status (7)
Country | Link |
---|---|
US (2) | US9109536B2 (pt) |
EP (1) | EP2971732B1 (pt) |
JP (1) | JP6060309B2 (pt) |
CN (1) | CN105190004B (pt) |
BR (1) | BR112015022654A8 (pt) |
CA (1) | CA2905325C (pt) |
WO (1) | WO2014158852A1 (pt) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2970521B1 (fr) * | 2011-01-17 | 2013-01-04 | Aircelle Sa | Inverseur de poussee pour turboreacteur d'aeronef a nombre de verrous reduit |
US9567943B2 (en) * | 2015-05-15 | 2017-02-14 | Rohr, Inc. | Pivoting track lock |
US9689345B2 (en) | 2015-06-10 | 2017-06-27 | Woodward, Inc. | Electric track lock |
US9850849B2 (en) * | 2015-07-07 | 2017-12-26 | Rohr, Inc. | Thrust reverser tertiary lock |
US10533519B2 (en) * | 2016-01-13 | 2020-01-14 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
US10415504B2 (en) * | 2016-02-09 | 2019-09-17 | Honeywell International Inc. | Translating cowl thrust reverser system with over-stow unlocking capability |
US10294893B2 (en) | 2016-05-25 | 2019-05-21 | Honeywell International Inc. | System and method for monitoring a translating cowl thrust reverser |
US10288007B2 (en) | 2017-02-02 | 2019-05-14 | Woodward, Inc. | Thrust reverser flow limiting valve |
FR3063527B1 (fr) * | 2017-03-06 | 2019-04-05 | Safran Electronics & Defense | Verin a verrouillage integre |
CN108661821B (zh) | 2017-03-31 | 2022-03-18 | Mra系统有限责任公司 | 反推力器组件及操作方法 |
FR3065260B1 (fr) * | 2017-04-14 | 2020-10-09 | Safran Aircraft Engines | Systeme inverseur de poussee pour turboreacteur |
US10570854B2 (en) * | 2017-08-18 | 2020-02-25 | Woodward, Inc. | Three actuator cascade type thrust reverser actuation system |
US10907577B2 (en) * | 2017-10-23 | 2021-02-02 | Rohr, Inc. | Translating lock for pivot door thrust reverser |
US11441514B2 (en) | 2018-10-02 | 2022-09-13 | Woodward, Inc. | Tertiary lock |
US10865738B2 (en) | 2019-02-27 | 2020-12-15 | Woodward, Inc. | Traveling finger lock for an actuator |
FR3107092B1 (fr) * | 2020-02-11 | 2022-09-09 | Safran Aircraft Engines | Procédé et système de commande d’un inverseur de poussée d’un aéronef |
US11486334B2 (en) * | 2020-05-29 | 2022-11-01 | The Boeing Company | Locking actuators for thrust reverser actuation systems, engines and aircraft including the same, and associated methods |
US11686273B2 (en) | 2020-10-12 | 2023-06-27 | Woodward, Inc. | Self-damping actuator |
US11788490B1 (en) | 2022-12-05 | 2023-10-17 | Woodward, Inc. | Traveling finger lock for an actuator |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2488335B1 (fr) | 1980-08-11 | 1986-01-31 | Snecma | Dispositif detecteur de position d'un inverseur de poussee de turboreacteur et de son verrouillage |
DE3337202A1 (de) * | 1983-10-13 | 1985-04-25 | Volkswagenwerk Ag, 3180 Wolfsburg | Verriegelungseinrichtung fuer einen schwenkbaren deckel, insbesondere fuer eine motor- oder kofferraumhaube eines kraftfahrzeuges |
US4798511A (en) * | 1986-12-23 | 1989-01-17 | Deere & Company | Method and apparatus for attaching a loader to a tractor |
IL103190A (en) | 1991-09-25 | 1995-06-29 | Messier Bugatti | A security locking device that includes a movable hook |
DE69207851T2 (de) | 1991-10-10 | 1996-08-29 | Lucas Industries P.L.C., Solihull, West Midlands | Verriegelung einer Schubumkehrvorrichtung |
FR2683860B1 (fr) * | 1991-11-14 | 1995-04-28 | Hurel Dubois Avions | Installation de securite pour inverseur de poussee a portes equipant un avion et ensemble incorporant une telle installation. |
US5224342A (en) | 1992-02-13 | 1993-07-06 | Lair Jean Pierre | Latching and sealing arrangement for jet engine thrust reverser |
GB9215496D0 (en) | 1992-07-21 | 1992-09-02 | Lucas Ind Plc | Lock for an engine thrust reverser |
WO1994007018A1 (en) | 1992-09-21 | 1994-03-31 | The Boeing Company | Mechanical lock for jet engine thrust reverser |
GB9320447D0 (en) | 1993-10-05 | 1993-12-22 | Lucas Ind Plc | Lock for an engine thrust reverser |
JP2991042B2 (ja) * | 1994-06-24 | 1999-12-20 | 株式会社田村電機製作所 | 開閉装置 |
GB9418895D0 (en) | 1994-09-20 | 1994-11-09 | Lucas Ind Plc | Lock mechanism |
GB2305460B (en) | 1995-09-25 | 1999-12-15 | Dowty Boulton Paul Ltd | Lock for engine thrust reverser |
US6021636A (en) | 1997-07-25 | 2000-02-08 | Alliedsignal Inc. | Lightweight tertiary thrust reverser lock assembly with a blocking member |
GB9907614D0 (en) | 1999-04-06 | 1999-05-26 | Lucas Ind Plc | Lock for a thrust reverser |
US6584763B2 (en) | 2001-08-01 | 2003-07-01 | Rohr, Inc. | Lock for the translating sleeve of a turbofan engine thrust reverser |
US6786039B2 (en) | 2001-09-07 | 2004-09-07 | Honeywell International, Inc. | Thrust reverser actuator with an automatic relock and lock drop prevention mechanism |
US6684623B2 (en) | 2002-02-27 | 2004-02-03 | Honeywell International, Inc. | Gearless electric thrust reverser actuators and actuation system incorporating same |
FR2860554B1 (fr) | 2003-10-06 | 2005-12-23 | Hurel Hispano | Verrou pour inverseur de poussee, muni d'un dispositif de blocage |
US7409820B2 (en) | 2004-11-16 | 2008-08-12 | Honeywell International Inc. | Electrical thrust reverser tertiary lock system including a voltage limiting circuit |
FR2890644B1 (fr) * | 2005-09-15 | 2007-11-02 | Aircelle Sa | Dispostif d'accrochage a autoverrouillage dynamique |
FR2913080B1 (fr) | 2007-02-22 | 2009-04-03 | Aircelle Sa | Verin a dispositif de verrouillage integre |
US8715132B2 (en) | 2010-12-31 | 2014-05-06 | Woodward Hrt, Inc. | Linear actuator and method of operation thereof |
FR2970521B1 (fr) | 2011-01-17 | 2013-01-04 | Aircelle Sa | Inverseur de poussee pour turboreacteur d'aeronef a nombre de verrous reduit |
-
2013
- 2013-03-14 US US13/827,192 patent/US9109536B2/en active Active
-
2014
- 2014-03-05 WO PCT/US2014/020557 patent/WO2014158852A1/en active Application Filing
- 2014-03-05 CA CA2905325A patent/CA2905325C/en active Active
- 2014-03-05 JP JP2016500632A patent/JP6060309B2/ja not_active Expired - Fee Related
- 2014-03-05 CN CN201480027898.XA patent/CN105190004B/zh active Active
- 2014-03-05 EP EP14712472.1A patent/EP2971732B1/en active Active
- 2014-03-05 BR BR112015022654A patent/BR112015022654A8/pt not_active Application Discontinuation
-
2015
- 2015-06-12 US US14/738,139 patent/US9790892B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2971732B1 (en) | 2018-10-17 |
US9790892B2 (en) | 2017-10-17 |
US9109536B2 (en) | 2015-08-18 |
CA2905325A1 (en) | 2014-10-02 |
US20150275821A1 (en) | 2015-10-01 |
JP6060309B2 (ja) | 2017-01-11 |
JP2016514234A (ja) | 2016-05-19 |
CA2905325C (en) | 2017-10-24 |
WO2014158852A1 (en) | 2014-10-02 |
EP2971732A1 (en) | 2016-01-20 |
BR112015022654A8 (pt) | 2019-11-26 |
CN105190004B (zh) | 2017-07-07 |
US20140270935A1 (en) | 2014-09-18 |
CN105190004A (zh) | 2015-12-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
B08G | Application fees: restoration [chapter 8.7 patent gazette] | ||
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B11B | Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements |