FR2939102B1 - Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale - Google Patents
Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinaleInfo
- Publication number
- FR2939102B1 FR2939102B1 FR0858169A FR0858169A FR2939102B1 FR 2939102 B1 FR2939102 B1 FR 2939102B1 FR 0858169 A FR0858169 A FR 0858169A FR 0858169 A FR0858169 A FR 0858169A FR 2939102 B1 FR2939102 B1 FR 2939102B1
- Authority
- FR
- France
- Prior art keywords
- resumption
- aircraft
- longitudinal direction
- rigid structure
- moment according
- 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 - Fee Related
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
- 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
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
- B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type within, or attached to, fuselages
-
- 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
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Body Structure For Vehicles (AREA)
- Connection Of Plates (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0858169A FR2939102B1 (fr) | 2008-12-01 | 2008-12-01 | Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale |
PCT/FR2009/052331 WO2010063925A1 (fr) | 2008-12-01 | 2009-11-30 | Structure rigide de mât d'aéronef équipée d'une extension de nervure pour la reprise du moment selon la direction longitudinale |
US13/131,999 US8864066B2 (en) | 2008-12-01 | 2009-11-30 | Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0858169A FR2939102B1 (fr) | 2008-12-01 | 2008-12-01 | Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2939102A1 FR2939102A1 (fr) | 2010-06-04 |
FR2939102B1 true FR2939102B1 (fr) | 2011-01-21 |
Family
ID=40873353
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0858169A Expired - Fee Related FR2939102B1 (fr) | 2008-12-01 | 2008-12-01 | Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale |
Country Status (3)
Country | Link |
---|---|
US (1) | US8864066B2 (fr) |
FR (1) | FR2939102B1 (fr) |
WO (1) | WO2010063925A1 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2915175B1 (fr) * | 2007-04-20 | 2009-07-17 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson |
FR2943623B1 (fr) * | 2009-03-30 | 2011-04-29 | Airbus France | Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
FR3014840B1 (fr) * | 2013-12-17 | 2017-10-13 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage |
FR3014841B1 (fr) * | 2013-12-17 | 2017-12-08 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage |
FR3015431B1 (fr) | 2013-12-19 | 2017-12-15 | Airbus Operations Sas | Structure primaire de mat d'accrochage renforcee. |
FR3015433B1 (fr) | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
FR3032942B1 (fr) | 2015-02-19 | 2018-11-23 | Safran Aircraft Engines | Ensemble propulsif pour aeronef comprenant un turboreacteur a soufflante non carenee et un pylone d'accrochage |
FR3060531B1 (fr) * | 2016-12-20 | 2019-05-31 | Airbus Operations | Partie arriere d'aeronef comprenant un cadre de fuselage supportant deux moteurs partiellement enterres |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4854525A (en) * | 1987-05-19 | 1989-08-08 | The Boeing Company | Engine mounting assembly |
US5064144A (en) * | 1987-05-19 | 1991-11-12 | The Boeing Company | Engine mounting assembly |
US4821980A (en) * | 1987-09-29 | 1989-04-18 | The Boeing Company | Vibration isolating engine mount |
US5065959A (en) * | 1989-11-21 | 1991-11-19 | The Boeing Company | Vibration damping aircraft engine attachment |
ES2341514B1 (es) * | 2007-10-03 | 2011-04-18 | Airbus España S.L. | Configuracion estructural para el montaje de un motor sobre la estructura de una aeronave. |
-
2008
- 2008-12-01 FR FR0858169A patent/FR2939102B1/fr not_active Expired - Fee Related
-
2009
- 2009-11-30 US US13/131,999 patent/US8864066B2/en active Active
- 2009-11-30 WO PCT/FR2009/052331 patent/WO2010063925A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
FR2939102A1 (fr) | 2010-06-04 |
US20110309189A1 (en) | 2011-12-22 |
WO2010063925A1 (fr) | 2010-06-10 |
US8864066B2 (en) | 2014-10-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
ST | Notification of lapse |
Effective date: 20200906 |