FR2955311B1 - Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef - Google Patents
Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronefInfo
- Publication number
- FR2955311B1 FR2955311B1 FR1050265A FR1050265A FR2955311B1 FR 2955311 B1 FR2955311 B1 FR 2955311B1 FR 1050265 A FR1050265 A FR 1050265A FR 1050265 A FR1050265 A FR 1050265A FR 2955311 B1 FR2955311 B1 FR 2955311B1
- Authority
- FR
- France
- Prior art keywords
- turbopropulser
- attaching
- preferably under
- aircraft
- vessel
- 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
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
- B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1050265A FR2955311B1 (fr) | 2010-01-15 | 2010-01-15 | Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef |
US13/004,369 US8474751B2 (en) | 2010-01-15 | 2011-01-11 | Device for fastening a turboprop, preferably under an aircraft wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1050265A FR2955311B1 (fr) | 2010-01-15 | 2010-01-15 | Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2955311A1 FR2955311A1 (fr) | 2011-07-22 |
FR2955311B1 true FR2955311B1 (fr) | 2012-03-23 |
Family
ID=42537612
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1050265A Active FR2955311B1 (fr) | 2010-01-15 | 2010-01-15 | Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef |
Country Status (2)
Country | Link |
---|---|
US (1) | US8474751B2 (fr) |
FR (1) | FR2955311B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2947528B1 (fr) * | 2009-07-03 | 2011-06-24 | Airbus Operations Sas | Systeme d'attache d'un moteur a helices |
WO2015074043A2 (fr) | 2013-11-18 | 2015-05-21 | Lord Corporation | Systèmes et procédés de fixation d'un groupe motopropulseur |
US9238511B2 (en) | 2014-03-04 | 2016-01-19 | Mra Systems, Inc. | Engine pylon structure |
FR3054202B1 (fr) | 2016-07-25 | 2018-07-13 | Safran Aircraft Engines | Berceau pour turbopropulseur a manche d'entree d'air integree |
US11674414B2 (en) * | 2021-03-19 | 2023-06-13 | Pratt & Whitney Canada Corp. | Gas turbine engine and mount assembly therefor |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2145280A (en) * | 1936-01-07 | 1939-01-31 | Wilbur E Stitz | Engine mounting |
GB798832A (en) * | 1955-02-04 | 1958-07-30 | Rolls Royce | Improvements in or relating to flexible mounting systems for vibrating bodies |
US4875655A (en) * | 1987-03-13 | 1989-10-24 | General Electric Company | Vibration isolating engine mount |
US5918833A (en) * | 1997-01-16 | 1999-07-06 | Applied Power Inc. | Hydraulic torque restraint system |
DE19713365C1 (de) * | 1997-04-01 | 1998-10-22 | Deutsch Zentr Luft & Raumfahrt | Triebwerksaufhängung, insbesondere für Propellerflugzeuge, mit einem Stabwerk zur Befestigung eines Triebwerks |
FR2862945B1 (fr) * | 2003-12-01 | 2006-04-28 | Airbus France | Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef. |
FR2916736B1 (fr) * | 2007-06-04 | 2009-09-04 | Airbus France Sa | Dispositif d'accrochage d'un turbopropulseur d'aeronef comprenant des moyens de fixation hydrauliques. |
FR2917710A1 (fr) * | 2007-06-22 | 2008-12-26 | Aircelle Sa | Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef |
-
2010
- 2010-01-15 FR FR1050265A patent/FR2955311B1/fr active Active
-
2011
- 2011-01-11 US US13/004,369 patent/US8474751B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2955311A1 (fr) | 2011-07-22 |
US8474751B2 (en) | 2013-07-02 |
US20110174918A1 (en) | 2011-07-21 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 15 |