BR112014030828A2 - mecanismo para acoplamento e desacoplamento de um eixo de admissão de motor e nacela de motor turbojato. - Google Patents
mecanismo para acoplamento e desacoplamento de um eixo de admissão de motor e nacela de motor turbojato.Info
- Publication number
- BR112014030828A2 BR112014030828A2 BR112014030828A BR112014030828A BR112014030828A2 BR 112014030828 A2 BR112014030828 A2 BR 112014030828A2 BR 112014030828 A BR112014030828 A BR 112014030828A BR 112014030828 A BR112014030828 A BR 112014030828A BR 112014030828 A2 BR112014030828 A2 BR 112014030828A2
- Authority
- BR
- Brazil
- Prior art keywords
- uncoupling
- coupling
- intake shaft
- engine
- nacelle
- 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
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D11/00—Clutches in which the members have interengaging parts
- F16D11/08—Clutches in which the members have interengaging parts actuated by moving a non-rotating part axially
- F16D11/10—Clutches in which the members have interengaging parts actuated by moving a non-rotating part axially with clutching members movable only axially
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D11/00—Clutches in which the members have interengaging parts
- F16D11/14—Clutches in which the members have interengaging parts with clutching members movable only axially
-
- 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
- F05D2250/00—Geometry
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
-
- 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
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D11/00—Clutches in which the members have interengaging parts
- F16D2011/006—Locking or detent means, i.e. means to keep the clutch in engaged condition
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Operated Clutches (AREA)
- One-Way And Automatic Clutches, And Combinations Of Different Clutches (AREA)
- Gear Transmission (AREA)
- Retarders (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1256438A FR2993026B1 (fr) | 2012-07-05 | 2012-07-05 | Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur |
FR1257685 | 2012-08-08 | ||
PCT/FR2013/051554 WO2014006321A1 (fr) | 2012-07-05 | 2013-07-02 | Mécanisme d'accouplement et de désaccouplement pour un dispositif embarqué d'une nacelle de turboréacteur |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014030828A2 true BR112014030828A2 (pt) | 2017-06-27 |
Family
ID=48914337
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014030828A BR112014030828A2 (pt) | 2012-07-05 | 2013-07-02 | mecanismo para acoplamento e desacoplamento de um eixo de admissão de motor e nacela de motor turbojato. |
Country Status (7)
Country | Link |
---|---|
US (1) | US20150083823A1 (pt) |
EP (1) | EP2870349B1 (pt) |
CN (1) | CN104428520A (pt) |
BR (1) | BR112014030828A2 (pt) |
CA (1) | CA2874578A1 (pt) |
RU (1) | RU2015102973A (pt) |
WO (1) | WO2014006321A1 (pt) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3019857B1 (fr) * | 2014-04-11 | 2020-12-25 | Aircelle Sa | Inverseur de poussee de nacelle de turboreacteur comprenant une commande commune pour les capots mobiles et une tuyere variable |
FR3087424B1 (fr) * | 2018-10-22 | 2021-01-22 | Safran Trans Systems | Systeme de couplage/decouplage de boitiers d'accessoires |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4567965A (en) * | 1982-03-22 | 1986-02-04 | Allied Corporation | Propeller brake |
US5609020A (en) * | 1995-05-15 | 1997-03-11 | The Boeing Company | Thrust reverser synchronization shaft lock |
DE19548271C2 (de) * | 1995-12-22 | 2002-07-18 | Claas Kgaa Mbh | Rundballenpresse für Erntegut |
CN1077217C (zh) * | 1996-08-22 | 2002-01-02 | 波音公司 | 反推装置同步轴锁定机构 |
US6786039B2 (en) * | 2001-09-07 | 2004-09-07 | Honeywell International, Inc. | Thrust reverser actuator with an automatic relock and lock drop prevention mechanism |
US6487846B1 (en) * | 2001-09-07 | 2002-12-03 | Honeywell International, Inc. | Thrust reverser actuator including an integrated locking mechanism |
CN1501006A (zh) * | 2002-11-16 | 2004-06-02 | Л | 轴用活套及装置 |
US7225607B2 (en) * | 2004-08-27 | 2007-06-05 | Pratt & Whitney Canada Corp. | Gas turbine braking apparatus and method |
JP5273351B2 (ja) * | 2008-05-12 | 2013-08-28 | セイコーエプソン株式会社 | 記録装置、回転軸のロック装置 |
FR2959488B1 (fr) * | 2010-04-28 | 2012-05-18 | Aircelle Sa | Nacelle pour moteur d'aeronef a inverseur de poussee a grilles et a tuyere adaptative |
-
2013
- 2013-07-02 CA CA2874578A patent/CA2874578A1/fr not_active Abandoned
- 2013-07-02 EP EP13744672.0A patent/EP2870349B1/fr not_active Not-in-force
- 2013-07-02 RU RU2015102973A patent/RU2015102973A/ru not_active Application Discontinuation
- 2013-07-02 WO PCT/FR2013/051554 patent/WO2014006321A1/fr active Application Filing
- 2013-07-02 BR BR112014030828A patent/BR112014030828A2/pt not_active IP Right Cessation
- 2013-07-02 CN CN201380035761.4A patent/CN104428520A/zh active Pending
-
2014
- 2014-12-03 US US14/558,833 patent/US20150083823A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP2870349B1 (fr) | 2016-05-04 |
EP2870349A1 (fr) | 2015-05-13 |
US20150083823A1 (en) | 2015-03-26 |
CN104428520A (zh) | 2015-03-18 |
CA2874578A1 (fr) | 2014-01-09 |
WO2014006321A1 (fr) | 2014-01-09 |
RU2015102973A (ru) | 2016-08-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB201213014D0 (en) | Uncoupling system for an aircraft turbojet engine rotary shaft | |
BR112014001679A2 (pt) | cone de escape para motor turbojato de aeronave | |
BR112015012584A2 (pt) | conjunto de motor de turbina e sistema de aeronave de bicombustivel | |
BRPI0821929A2 (pt) | Nacela para motor turbojato | |
BR112014008570A2 (pt) | reversor de empuxo para uma nacela de um motor turbojato e nacela para uma aeronave turbojato | |
BR112014028731A2 (pt) | reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato. | |
BR112014009939A2 (pt) | dispositivo de reversão de empuxo para uma nacela de motor turbojato e nacela de um motor turbojato | |
BR112012025690A2 (pt) | métodos para operar um motor | |
BR112014017430A2 (pt) | reversor de empuxo do tipo cascata para um motor turbojato de aeronaves e nacela oara um motor turbojato de aeronaves | |
BRPI0908079A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
BRPI0821504A2 (pt) | nacela para motor de avião | |
BRPI0907771A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
BRPI1007029A2 (pt) | conjunto de suspensão para motor turbojato de aeronaves | |
GB2503713B (en) | Engine assembly with an Exhaust Driven Turbine | |
EP2812541A4 (en) | TURBINE ENGINE SHAFT COUPLING | |
BR112015012033A2 (pt) | dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves | |
BRPI0822127A8 (pt) | nacela para motor turbojato e aeronave | |
BR112013023410A2 (pt) | dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente | |
GB2504168B (en) | Power take-off system for an internal combustion engine | |
BR112015005181A2 (pt) | dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato. | |
BR112015003808A2 (pt) | aparelho de invólucro para um motor de turbina a gás e aparelho de hélice para um motor de turbina a gás | |
BR112014006998A2 (pt) | conjunto de propulsão de aeronave compreendendo um motor turbojato | |
BR112014010136A2 (pt) | reversor de empuxo para uma nacela de motor turbojato de aeronave e nacela | |
BRPI0907959A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
BR112015001709A2 (pt) | cascata de reversor de empuxo, reversor de empuxo e nacela de motor de aeronave |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: application dismissed [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 4A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |