FR2935353B1 - Mat pour la suspension d'un turbomoteur sous une aile d'aeronef - Google Patents
Mat pour la suspension d'un turbomoteur sous une aile d'aeronefInfo
- Publication number
- FR2935353B1 FR2935353B1 FR0804831A FR0804831A FR2935353B1 FR 2935353 B1 FR2935353 B1 FR 2935353B1 FR 0804831 A FR0804831 A FR 0804831A FR 0804831 A FR0804831 A FR 0804831A FR 2935353 B1 FR2935353 B1 FR 2935353B1
- Authority
- FR
- France
- Prior art keywords
- turbomoteur
- mat
- suspension
- under
- aircraft wing
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0804831A FR2935353B1 (fr) | 2008-09-03 | 2008-09-03 | Mat pour la suspension d'un turbomoteur sous une aile d'aeronef |
US12/550,454 US8336813B2 (en) | 2008-09-03 | 2009-08-31 | Engine pylon for the suspension of a turbo engine under an aircraft wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0804831A FR2935353B1 (fr) | 2008-09-03 | 2008-09-03 | Mat pour la suspension d'un turbomoteur sous une aile d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2935353A1 FR2935353A1 (fr) | 2010-03-05 |
FR2935353B1 true FR2935353B1 (fr) | 2010-09-10 |
Family
ID=40513746
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0804831A Active FR2935353B1 (fr) | 2008-09-03 | 2008-09-03 | Mat pour la suspension d'un turbomoteur sous une aile d'aeronef |
Country Status (2)
Country | Link |
---|---|
US (1) | US8336813B2 (fr) |
FR (1) | FR2935353B1 (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2958624B1 (fr) * | 2010-04-08 | 2012-06-08 | Airbus Operations Sas | Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence |
US8651426B2 (en) | 2010-07-01 | 2014-02-18 | Rolls-Royce Plc | Jet engine installation |
GB201011056D0 (en) | 2010-07-01 | 2010-08-18 | Rolls Royce Plc | Pylon for attaching a gas turbine engine |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
US9533754B2 (en) * | 2014-04-19 | 2017-01-03 | The Boeing Company | Wing aerial refueling system |
FR3040043B1 (fr) | 2015-08-12 | 2019-04-12 | Sogeclair Sa | Mat de moteur d'aeronef a ossature multifonctionnelle integree |
US9908631B2 (en) | 2015-11-30 | 2018-03-06 | Embraer S.A. | Optimized aircraft pylon fairing |
US20180237120A1 (en) * | 2017-02-22 | 2018-08-23 | General Electric Company | Aircraft with Under Wing Direct Drive Low Pressure Turbine |
US11421627B2 (en) * | 2017-02-22 | 2022-08-23 | General Electric Company | Aircraft and direct drive engine under wing installation |
WO2019075555A1 (fr) * | 2017-10-19 | 2019-04-25 | Bombardier Inc. | Carénage de pylône d'aéronef |
US11174004B2 (en) * | 2019-05-20 | 2021-11-16 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11535362B2 (en) | 2019-05-20 | 2022-12-27 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11072416B2 (en) | 2019-05-20 | 2021-07-27 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11613345B2 (en) | 2019-05-20 | 2023-03-28 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11873078B2 (en) | 2019-05-20 | 2024-01-16 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11235857B2 (en) | 2019-05-20 | 2022-02-01 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11591097B2 (en) | 2019-05-20 | 2023-02-28 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11745860B2 (en) | 2019-05-20 | 2023-09-05 | The Boeing Company | Aircraft nacelles having adjustable chines |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2995320A (en) * | 1958-04-14 | 1961-08-08 | Eldon W Gottschalk | Supersonic aircraft having extensible nose cone |
US4449683A (en) * | 1979-01-03 | 1984-05-22 | The Boeing Company | Aerodynamically contoured, low drag wing engine and engine nacelle combination |
US4540143A (en) * | 1983-08-04 | 1985-09-10 | The Boeing Company | Nacelle/wing assembly with wake control device |
FR2555960B1 (fr) * | 1983-12-06 | 1986-09-19 | Aerospatiale | Aile d'aeronef en fleche pourvue d'un systeme hypersustentateur et d'un mat de suspension de moteur, ainsi que mat de suspension de moteur pour une telle aile |
US4801058A (en) * | 1987-02-05 | 1989-01-31 | Rolls-Royce Plc | Aircraft and powerplant combinations |
US5443230A (en) * | 1993-12-21 | 1995-08-22 | United Technologies Corporation | Aircraft wing/nacelle combination |
US6978971B1 (en) * | 2004-06-15 | 2005-12-27 | The Boeing Company | Methods and apparatuses for controlling airflow proximate to engine/airfoil systems |
FR2876658B1 (fr) * | 2004-10-15 | 2007-01-19 | Airbus France Sas | Empennage vertical pour aeronef et aeronef muni d'un tel empennage |
US7721999B2 (en) * | 2005-05-20 | 2010-05-25 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
FR2899201B1 (fr) * | 2006-03-31 | 2009-02-13 | Airbus France Sas | Agencement d'aile d'aeronef comportant un mat d'accrochage de moteur definissant en zone avant un canal lateral d'ecoulement d'air |
FR2905930B1 (fr) * | 2006-09-18 | 2009-05-15 | Airbus France Sa | Generateur de tourbillon en sortie de gaz chauds |
FR2958624B1 (fr) * | 2010-04-08 | 2012-06-08 | Airbus Operations Sas | Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence |
-
2008
- 2008-09-03 FR FR0804831A patent/FR2935353B1/fr active Active
-
2009
- 2009-08-31 US US12/550,454 patent/US8336813B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2935353A1 (fr) | 2010-03-05 |
US20100051744A1 (en) | 2010-03-04 |
US8336813B2 (en) | 2012-12-25 |
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Legal Events
Date | Code | Title | Description |
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CD | Change of name or company name | ||
CA | Change of address |
Effective date: 20120313 |
|
CD | Change of name or company name |
Owner name: AIRBUS OPERATIONS, FR Effective date: 20120313 Owner name: AIRBUS OPERATIONS LIMITED, GB Effective date: 20120313 |
|
CJ | Change in legal form |
Effective date: 20120313 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20130322 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
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Year of fee payment: 9 |
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