DE69723534D1 - Redundantes, vorderes Aufhängungssystem für ein Turbotriebwerk - Google Patents
Redundantes, vorderes Aufhängungssystem für ein TurbotriebwerkInfo
- Publication number
- DE69723534D1 DE69723534D1 DE69723534T DE69723534T DE69723534D1 DE 69723534 D1 DE69723534 D1 DE 69723534D1 DE 69723534 T DE69723534 T DE 69723534T DE 69723534 T DE69723534 T DE 69723534T DE 69723534 D1 DE69723534 D1 DE 69723534D1
- Authority
- DE
- Germany
- Prior art keywords
- suspension system
- front suspension
- turbo engine
- redundant front
- redundant
- 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
- 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
-
- 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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- 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
- B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
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 |
---|---|---|---|
FR9614189 | 1996-11-21 | ||
FR9614189A FR2755942B1 (fr) | 1996-11-21 | 1996-11-21 | Suspension avant redondante pour turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69723534D1 true DE69723534D1 (de) | 2003-08-21 |
DE69723534T2 DE69723534T2 (de) | 2004-04-15 |
Family
ID=9497842
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69723534T Expired - Lifetime DE69723534T2 (de) | 1996-11-21 | 1997-11-20 | Redundantes, vorderes Aufhängungssystem für ein Turbotriebwerk |
Country Status (4)
Country | Link |
---|---|
US (1) | US5871175A (de) |
EP (1) | EP0844173B1 (de) |
DE (1) | DE69723534T2 (de) |
FR (1) | FR2755942B1 (de) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2793769B1 (fr) * | 1999-05-19 | 2001-09-07 | Aerospatiale Airbus | Dispositif d'accrochage d'un moteur d'aeronef a un mat |
GB9927425D0 (en) * | 1999-11-20 | 2000-01-19 | Rolls Royce Plc | A gas turbine engine mounting arrangement |
FR2818614B1 (fr) * | 2000-12-21 | 2003-01-31 | Snecma Moteurs | Piece de suspension d'un turboreacteur |
GB2375513B (en) * | 2001-05-19 | 2005-03-23 | Rolls Royce Plc | A mounting arrangement for a gas turbine engine |
GB0507721D0 (en) * | 2005-04-16 | 2005-05-25 | Rolls Royce Plc | Gas turbine engine mounting arrangement |
FR2915177B1 (fr) * | 2007-04-20 | 2009-07-10 | Airbus France Sa | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif |
FR2917710A1 (fr) * | 2007-06-22 | 2008-12-26 | Aircelle Sa | Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef |
US11149650B2 (en) | 2007-08-01 | 2021-10-19 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US20150377123A1 (en) | 2007-08-01 | 2015-12-31 | United Technologies Corporation | Turbine section of high bypass turbofan |
US11346289B2 (en) | 2007-08-01 | 2022-05-31 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11242805B2 (en) | 2007-08-01 | 2022-02-08 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US8844265B2 (en) | 2007-08-01 | 2014-09-30 | United Technologies Corporation | Turbine section of high bypass turbofan |
US11486311B2 (en) | 2007-08-01 | 2022-11-01 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US8256707B2 (en) * | 2007-08-01 | 2012-09-04 | United Technologies Corporation | Engine mounting configuration for a turbofan gas turbine engine |
US8118251B2 (en) * | 2008-01-18 | 2012-02-21 | United Technologies Corporation | Mounting system for a gas turbine engine |
US8167237B2 (en) * | 2008-03-21 | 2012-05-01 | United Technologies Corporation | Mounting system for a gas turbine engine |
US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8807477B2 (en) | 2008-06-02 | 2014-08-19 | United Technologies Corporation | Gas turbine engine compressor arrangement |
US8695920B2 (en) | 2008-06-02 | 2014-04-15 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8511605B2 (en) | 2008-06-02 | 2013-08-20 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8800914B2 (en) | 2008-06-02 | 2014-08-12 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8128021B2 (en) * | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
GB0810585D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
GB0810589D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
FR2989952B1 (fr) | 2012-04-27 | 2014-04-18 | Aircelle Sa | Nacelle de turboreacteur a section aval |
EP3058202A4 (de) | 2013-10-16 | 2017-06-28 | United Technologies Corporation | Turbogebläsemotor mit gezielter modularer wirkung |
US9617918B2 (en) * | 2014-01-13 | 2017-04-11 | The Boeing Company | Bracket for mounting/removal of actuators for active vibration control |
CN105270638A (zh) * | 2015-11-17 | 2016-01-27 | 江西洪都航空工业集团有限责任公司 | 一种飞机发动机安装装置 |
FR3096028B1 (fr) * | 2019-05-14 | 2021-05-21 | Airbus Operations Sas | Attache moteur arriere pour un moteur d’aeronef |
FR3097204B1 (fr) * | 2019-06-17 | 2021-06-18 | Airbus Operations Sas | Attache moteur pour un moteur d’un aeronef comportant une bielle et un systeme anti-basculement de la bielle |
CN114136634B (zh) * | 2021-11-30 | 2024-04-05 | 中国航发湖南动力机械研究所 | 一种发动机挂架导向定位装置 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3844115A (en) * | 1973-02-14 | 1974-10-29 | Gen Electric | Load distributing thrust mount |
US3907220A (en) * | 1974-03-14 | 1975-09-23 | United Aircraft Corp | Rear engine redundant mount |
GB1521847A (en) * | 1976-04-30 | 1978-08-16 | Rolls Royce | Attachment for attaching jet propulsion engines to vehicle structure |
GB8300748D0 (en) * | 1983-01-12 | 1983-02-16 | British Aerospace | Power plant attachment for aircraft wings |
FR2599708A1 (fr) * | 1986-06-10 | 1987-12-11 | Snecma | Dispositif d'accrochage arriere de securite d'un turboreacteur sur un mat d'avion |
FR2680353B1 (fr) * | 1991-08-14 | 1993-10-15 | Snecma | Structure d'accrochage arriere d'un turboreacteur. |
GB9125011D0 (en) * | 1991-11-25 | 1992-01-22 | Rolls Royce Plc | A mounting arrangement for a gas turbine engine |
US5303880A (en) * | 1992-10-28 | 1994-04-19 | General Electric Company | Aircraft engine pin mount |
-
1996
- 1996-11-21 FR FR9614189A patent/FR2755942B1/fr not_active Expired - Fee Related
-
1997
- 1997-11-19 US US08/974,423 patent/US5871175A/en not_active Expired - Lifetime
- 1997-11-20 DE DE69723534T patent/DE69723534T2/de not_active Expired - Lifetime
- 1997-11-20 EP EP97402789A patent/EP0844173B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2755942A1 (fr) | 1998-05-22 |
DE69723534T2 (de) | 2004-04-15 |
EP0844173B1 (de) | 2003-07-16 |
US5871175A (en) | 1999-02-16 |
FR2755942B1 (fr) | 1998-12-24 |
EP0844173A1 (de) | 1998-05-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: SNECMA, PARIS, FR |