DE69822134D1 - Flugzeug-triebwerksanlage mit sicherheitseinrichtungen für das stellen und festhalten von den gebläsehauben - Google Patents
Flugzeug-triebwerksanlage mit sicherheitseinrichtungen für das stellen und festhalten von den gebläsehaubenInfo
- Publication number
- DE69822134D1 DE69822134D1 DE69822134T DE69822134T DE69822134D1 DE 69822134 D1 DE69822134 D1 DE 69822134D1 DE 69822134 T DE69822134 T DE 69822134T DE 69822134 T DE69822134 T DE 69822134T DE 69822134 D1 DE69822134 D1 DE 69822134D1
- Authority
- DE
- Germany
- Prior art keywords
- fastening
- fixing
- engine system
- safety devices
- airplane engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- 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
- 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/08—Inspection panels for power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9715930A FR2772342B1 (fr) | 1997-12-16 | 1997-12-16 | Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef |
FR9715930 | 1997-12-16 | ||
PCT/FR1998/002718 WO1999030969A1 (fr) | 1997-12-16 | 1998-12-14 | Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69822134D1 true DE69822134D1 (de) | 2004-04-08 |
DE69822134T2 DE69822134T2 (de) | 2004-09-16 |
Family
ID=9514667
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69822134T Expired - Lifetime DE69822134T2 (de) | 1997-12-16 | 1998-12-14 | Flugzeug-triebwerksanlage mit sicherheitseinrichtungen für das stellen und festhalten von den gebläsehauben |
Country Status (7)
Country | Link |
---|---|
US (1) | US6334588B1 (de) |
EP (1) | EP0960051B1 (de) |
CA (1) | CA2281619C (de) |
DE (1) | DE69822134T2 (de) |
ES (1) | ES2216332T3 (de) |
FR (1) | FR2772342B1 (de) |
WO (1) | WO1999030969A1 (de) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6220546B1 (en) * | 1999-12-29 | 2001-04-24 | The Boeing Company | Aircraft engine and associated aircraft engine cowl |
FR2835870B1 (fr) * | 2002-02-14 | 2005-03-11 | Airbus France | Systeme de fermeture interpose entre deux elements |
FR2856379B1 (fr) * | 2003-06-18 | 2006-11-24 | Airbus France | Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit |
FR2896481B1 (fr) * | 2006-01-23 | 2009-12-04 | Aircelle Sa | Systeme de fixation pour element constitutif d'une nacelle de turboreacteur |
FR2903666B1 (fr) * | 2006-07-11 | 2008-10-10 | Airbus France Sas | Ensemble moteur pour aeronef comprenant un capotage aerodynamique de jonction monte sur deux elements distincts |
FR2903665B1 (fr) * | 2006-07-11 | 2008-10-10 | Airbus France Sas | Ensemble moteur pour aeronef comprenant un berceau de support de capot de soufflante monte sur deux elements distincts |
FR2907759B1 (fr) * | 2006-10-31 | 2008-12-12 | Aircelle Sa | Nacelle pour turboreacteur a ouverture laterale |
FR2916426B1 (fr) * | 2007-05-22 | 2010-04-02 | Aircelle Sa | Ensemble arriere de nacelle pour turboreacteur. |
US7843363B2 (en) * | 2007-07-12 | 2010-11-30 | Rosemount Aerospace Inc. | Mechanical latch locking detection sensors |
FR2920140B1 (fr) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | Nacelle de turboreacteur, destinee a equiper un aeronef |
FR2920141B1 (fr) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | Nacelle de turboreacteur, destinee a equiper un aeronef |
US20090049842A1 (en) * | 2007-08-23 | 2009-02-26 | General Electric Company | Enclosure for a gas turbine and method for enclosing the same |
US7661321B2 (en) | 2007-09-25 | 2010-02-16 | Rosemount Aerospace Inc. | Force sensing clevis insert |
US20090173823A1 (en) * | 2008-01-07 | 2009-07-09 | Rohr, Inc. | Method and component for determining load on a latch assembly |
US8220738B2 (en) * | 2008-11-26 | 2012-07-17 | Mra Systems, Inc. | Nacelle and method of assembling the same |
US9188026B2 (en) * | 2008-11-26 | 2015-11-17 | Mra Systems, Inc. | Apparatus for facilitating access to a nacelle interior and method of assembling the same |
US9188025B2 (en) * | 2008-11-26 | 2015-11-17 | Mra Systems, Inc. | Apparatus for facilitating access to a nacelle interior |
FR2942492B1 (fr) * | 2009-02-20 | 2011-03-04 | Aircelle Sa | Procede de fermeture d'un element mobile de nacelle |
US8272595B2 (en) * | 2009-11-27 | 2012-09-25 | Rohr, Inc. | Fan cowl support for a turbofan engine |
FR2955312B1 (fr) * | 2010-01-20 | 2013-05-31 | Airbus Operations Sas | Dispositif de liaison fusible entre une partie mobile et une partie fixe d'une nacelle d'aeronef |
US8607640B2 (en) | 2010-07-19 | 2013-12-17 | Odd Harald Steen Eriksen | Sensor for measuring large mechanical strains in shear or lateral translation |
US8933713B2 (en) | 2010-07-19 | 2015-01-13 | Goodrich Corporation | Capacitive sensors for monitoring loads |
US8659307B2 (en) | 2010-08-17 | 2014-02-25 | Rosemount Aerospace Inc. | Capacitive sensors for monitoring load bearing on pins |
US8627727B2 (en) | 2010-07-19 | 2014-01-14 | United Technologies Corporation | Sensor for measuring large mechanical strains with fine adjustment device |
US8359932B2 (en) | 2010-07-19 | 2013-01-29 | Goodrich Corporation | Systems and methods for mounting landing gear strain sensors |
US8286508B2 (en) | 2010-07-19 | 2012-10-16 | Goodrich Corporation | Systems and methods for measuring angular motion |
US10131419B2 (en) | 2010-10-15 | 2018-11-20 | Goodrich Corporation | Systems and methods for detecting landing gear ground loads |
US9567097B2 (en) | 2012-02-03 | 2017-02-14 | Rosemount Aerospace Inc. | System and method for real-time aircraft performance monitoring |
FR3008072B1 (fr) * | 2013-07-03 | 2017-08-18 | Airbus Operations Sas | Nacelle d'un ensemble propulsif d'aeronef comportant un capot et un mecanisme d'ecartement de volets du capot |
US9873504B2 (en) * | 2013-10-18 | 2018-01-23 | Rohr, Inc. | Propulsion system nacelle with reduced number of external split lines |
FR3012114B1 (fr) * | 2013-10-18 | 2017-02-24 | Airbus Operations Sas | Ensemble propulsif d'aeronef comportant une nacelle pourvue d'un mecanisme de verrouillage et de fermeture des capots |
US9366202B2 (en) * | 2013-11-27 | 2016-06-14 | Rohr, Inc. | System and method for captured inner fixed structure |
EP3000734B1 (de) * | 2014-09-29 | 2018-03-14 | Airbus Defence and Space, S.A. | Ausrichtungs- und Sicherheitsvorrichtung für die Hauben von Flugzeugtriebwerksgondeln |
DE102015226543A1 (de) * | 2015-12-22 | 2017-06-22 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung |
US10605198B2 (en) * | 2016-04-15 | 2020-03-31 | Rohr, Inc. | Nacelle thrust reverser |
US10578204B2 (en) | 2016-08-23 | 2020-03-03 | United Technologies Corporation | Fused pilot for boss-mounted gearbox link |
CN108953379B (zh) * | 2018-08-02 | 2020-06-19 | 上海船舶研究设计院(中国船舶工业集团公司第六0四研究院) | 挡水轴套及吊舱推进敞水试验设备 |
FR3085353A1 (fr) * | 2018-09-04 | 2020-03-06 | Airbus Operations | Ensemble turbomachine d'aeronef comportant un capot articule |
US11414200B2 (en) | 2019-04-29 | 2022-08-16 | Rohr, Inc. | Fan cowl securement retainers |
US11268406B2 (en) * | 2019-08-12 | 2022-03-08 | The Boeing Company | Movement-limiting device for a turbine engine and associated method |
US11866189B2 (en) * | 2020-03-26 | 2024-01-09 | Hartwell Corporation | Latching system with movable anti-shear mechanism |
CN113928573B (zh) * | 2021-11-19 | 2023-04-18 | 中国直升机设计研究所 | 一种具备导向缓冲功能的滑动整流罩 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2379433A1 (fr) * | 1977-02-08 | 1978-09-01 | Snecma | Systeme de securite pour capotage de nacelle de turboreacteur |
US4365775A (en) * | 1980-12-08 | 1982-12-28 | The Boeing Company | Cowl structure alignment and shear device |
US4613099A (en) * | 1982-02-05 | 1986-09-23 | The Boeing Company | Latch signal and cowling structure |
US4679750A (en) * | 1984-06-20 | 1987-07-14 | The Boeing Company | Latch system |
US4629146A (en) * | 1985-01-30 | 1986-12-16 | Rohr Industries, Inc. | Hold open rod for hinged section of nacelle system |
GB9120658D0 (en) * | 1991-09-27 | 1991-11-06 | Short Brothers Plc | Ducted fan turbine engine |
GB2267122B (en) * | 1992-05-22 | 1995-06-14 | Short Brothers Plc | Closure default indicator |
GB9407632D0 (en) * | 1994-04-18 | 1994-06-08 | Short Brothers Plc | An aircraft propulsive power unit |
FR2734540B1 (fr) * | 1995-05-24 | 1997-08-08 | Aerospatiale | Nacelle de moteur d'aeronef comportant un capot de nacelle |
FR2756323B1 (fr) * | 1996-11-28 | 1998-12-31 | Hispano Suiza Sa | Dispositif de liaison d'un inverseur de poussee a un turbomoteur |
-
1997
- 1997-12-16 FR FR9715930A patent/FR2772342B1/fr not_active Expired - Lifetime
-
1998
- 1998-12-14 ES ES98959978T patent/ES2216332T3/es not_active Expired - Lifetime
- 1998-12-14 WO PCT/FR1998/002718 patent/WO1999030969A1/fr active IP Right Grant
- 1998-12-14 EP EP98959978A patent/EP0960051B1/de not_active Expired - Lifetime
- 1998-12-14 DE DE69822134T patent/DE69822134T2/de not_active Expired - Lifetime
- 1998-12-14 US US09/341,573 patent/US6334588B1/en not_active Expired - Lifetime
- 1998-12-14 CA CA002281619A patent/CA2281619C/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
WO1999030969A1 (fr) | 1999-06-24 |
CA2281619A1 (fr) | 1999-06-24 |
ES2216332T3 (es) | 2004-10-16 |
FR2772342B1 (fr) | 2000-02-18 |
DE69822134T2 (de) | 2004-09-16 |
FR2772342A1 (fr) | 1999-06-18 |
US6334588B1 (en) | 2002-01-01 |
EP0960051A1 (de) | 1999-12-01 |
EP0960051B1 (de) | 2004-03-03 |
CA2281619C (fr) | 2007-09-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
R082 | Change of representative |
Ref document number: 960051 Country of ref document: EP Representative=s name: BETTEN & RESCH, 80333 MUENCHEN, DE |