DE602004004052D1 - Aufhängung für Mantelstromtriebwerk - Google Patents
Aufhängung für MantelstromtriebwerkInfo
- Publication number
- DE602004004052D1 DE602004004052D1 DE602004004052T DE602004004052T DE602004004052D1 DE 602004004052 D1 DE602004004052 D1 DE 602004004052D1 DE 602004004052 T DE602004004052 T DE 602004004052T DE 602004004052 T DE602004004052 T DE 602004004052T DE 602004004052 D1 DE602004004052 D1 DE 602004004052D1
- Authority
- DE
- Germany
- Prior art keywords
- suspension
- turbofan engine
- turbofan
- 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.)
- Active
Links
- 239000000725 suspension Substances 0.000 title 1
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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0328671 | 2003-12-11 | ||
GBGB0328671.3A GB0328671D0 (en) | 2003-12-11 | 2003-12-11 | Aircraft engine mounting |
Publications (2)
Publication Number | Publication Date |
---|---|
DE602004004052D1 true DE602004004052D1 (de) | 2007-02-15 |
DE602004004052T2 DE602004004052T2 (de) | 2007-04-12 |
Family
ID=30129997
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602004004052T Active DE602004004052T2 (de) | 2003-12-11 | 2004-11-11 | Aufhängung für Mantelstromtriebwerk |
Country Status (4)
Country | Link |
---|---|
US (1) | US7313920B2 (de) |
EP (1) | EP1541468B1 (de) |
DE (1) | DE602004004052T2 (de) |
GB (1) | GB0328671D0 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0607991D0 (en) * | 2006-04-22 | 2006-05-31 | Rolls Royce Plc | Aeroengine mounting |
FR2905975B1 (fr) * | 2006-09-20 | 2008-12-05 | Snecma Sa | Conduite de soufflante pour une turbomachine. |
FR2920198B1 (fr) | 2007-08-20 | 2009-10-30 | Aircelle Sa | Structure pour inverseur de poussee |
FR2928180B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur. |
US8979491B2 (en) | 2009-05-15 | 2015-03-17 | Pratt & Whitney Canada Corp. | Turbofan mounting arrangement |
US8567202B2 (en) * | 2009-05-15 | 2013-10-29 | Pratt & Whitney Canada Corp. | Support links with lockable adjustment feature |
US8313293B2 (en) * | 2009-05-15 | 2012-11-20 | Pratt & Whitney Canada Corp. | Turbofan mounting system |
FR2956164B1 (fr) * | 2010-02-10 | 2012-02-24 | Snecma | Liaison entre le carter d'echappement et un anneau structural de conduit de soufflante d'un turboreacteur |
US9828105B2 (en) | 2011-08-24 | 2017-11-28 | United Technologies Corporation | Nacelle assembly having integrated afterbody mount case |
US9194296B2 (en) | 2012-05-18 | 2015-11-24 | Pratt & Whitney Canada Corp. | Inner bypass duct wall attachment |
DE102013007607A1 (de) * | 2013-05-03 | 2014-11-06 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinentriebwerk mit modularem Nebenstromgehäuse |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
US11585274B2 (en) | 2020-12-28 | 2023-02-21 | General Electric Company | Turbine rear frame link assemblies for turbofan engines |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1074068A (en) | 1964-09-22 | 1967-06-28 | Rolls Royce | Mounting arrangement for gas turbine jet propulsion engines |
US3318554A (en) * | 1964-09-22 | 1967-05-09 | Rolls Royce | Mounting arrangement for engines |
US3398535A (en) * | 1966-05-25 | 1968-08-27 | Gen Electric | Engine supporting structure |
US3397855A (en) * | 1966-12-01 | 1968-08-20 | United Aircraft Canada | Rear mount system for aircraft engines |
GB1318748A (en) * | 1970-08-11 | 1973-05-31 | Secr Defence | Gas turgine ducted fan engines for aircraft |
US3907220A (en) * | 1974-03-14 | 1975-09-23 | United Aircraft Corp | Rear engine redundant mount |
US4266741A (en) * | 1978-05-22 | 1981-05-12 | The Boeing Company | Mounting apparatus for fan jet engine having mixed flow nozzle installation |
SU849694A1 (ru) | 1980-03-12 | 1996-09-20 | А.А. Бобух | Устройство для крепления двухконтурного турбореактивного двигателя |
WO1985002596A1 (en) * | 1983-12-08 | 1985-06-20 | The Boeing Company | Aft engine mount |
WO1991005150A1 (en) * | 1989-09-29 | 1991-04-18 | Sundstrand Corporation, Inc. | Geodesic engine mount structure |
US5076049A (en) * | 1990-04-02 | 1991-12-31 | General Electric Company | Pretensioned frame |
FR2676707B1 (fr) * | 1991-05-23 | 1993-08-13 | Snecma | Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. |
GB2303884B (en) * | 1995-04-13 | 1999-07-14 | Rolls Royce Plc | A mounting for coupling a turbofan gas turbine engine to an aircraft structure |
US5927644A (en) * | 1997-10-08 | 1999-07-27 | General Electric Company | Double failsafe engine mount |
GB2394991B (en) * | 2002-11-06 | 2006-02-15 | Rolls Royce Plc | Mounting arrangement |
FR2855496B1 (fr) * | 2003-05-27 | 2006-09-22 | Snecma Moteurs | Suspension arriere de moteur d'avion avec reprise de poussee |
US7083143B2 (en) * | 2003-10-17 | 2006-08-01 | The Boeing Company | Apparatuses and methods for attaching engines and other structures to aircraft wings |
-
2003
- 2003-12-11 GB GBGB0328671.3A patent/GB0328671D0/en not_active Ceased
-
2004
- 2004-11-11 DE DE602004004052T patent/DE602004004052T2/de active Active
- 2004-11-11 EP EP04257025A patent/EP1541468B1/de not_active Expired - Fee Related
- 2004-12-02 US US11/001,122 patent/US7313920B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB0328671D0 (en) | 2004-01-14 |
DE602004004052T2 (de) | 2007-04-12 |
US20050230532A1 (en) | 2005-10-20 |
EP1541468B1 (de) | 2007-01-03 |
EP1541468A1 (de) | 2005-06-15 |
US7313920B2 (en) | 2008-01-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |