FR2676707B1 - Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. - Google Patents
Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.Info
- Publication number
- FR2676707B1 FR2676707B1 FR9106198A FR9106198A FR2676707B1 FR 2676707 B1 FR2676707 B1 FR 2676707B1 FR 9106198 A FR9106198 A FR 9106198A FR 9106198 A FR9106198 A FR 9106198A FR 2676707 B1 FR2676707 B1 FR 2676707B1
- Authority
- FR
- France
- Prior art keywords
- nacelle
- turbo
- wing
- aircraft
- flow type
- 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
- B64D27/40—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
-
- 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
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 |
---|---|---|---|
FR9106198A FR2676707B1 (fr) | 1991-05-23 | 1991-05-23 | Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. |
US07/886,838 US5181675A (en) | 1991-05-23 | 1992-05-22 | Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9106198A FR2676707B1 (fr) | 1991-05-23 | 1991-05-23 | Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2676707A1 FR2676707A1 (fr) | 1992-11-27 |
FR2676707B1 true FR2676707B1 (fr) | 1993-08-13 |
Family
ID=9413034
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9106198A Expired - Fee Related FR2676707B1 (fr) | 1991-05-23 | 1991-05-23 | Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. |
Country Status (2)
Country | Link |
---|---|
US (1) | US5181675A (fr) |
FR (1) | FR2676707B1 (fr) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5277382A (en) * | 1992-10-13 | 1994-01-11 | General Electric Company | Aircraft engine forward mount |
GB2275308B (en) * | 1993-02-20 | 1997-02-26 | Rolls Royce Plc | A mounting for coupling a turbofan gas turbine engine to an aircraft structure |
US5452575A (en) * | 1993-09-07 | 1995-09-26 | General Electric Company | Aircraft gas turbine engine thrust mount |
US5467941A (en) * | 1993-12-30 | 1995-11-21 | The Boeing Company | Pylon and engine installation for ultra-high by-pass turbo-fan engines |
WO1996020111A1 (fr) * | 1994-12-23 | 1996-07-04 | United Technologies Corporation | Ensemble de montage pour turbine a gaz |
US6095456A (en) * | 1996-12-23 | 2000-08-01 | The Boeing Company | Strut-wing interface having dual upper links |
US6189830B1 (en) * | 1999-02-26 | 2001-02-20 | The Boeing Company | Tuned engine mounting system for jet aircraft |
FR2793768B1 (fr) * | 1999-05-17 | 2001-09-07 | Aerospatiale Airbus | Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif |
GB2359052B (en) * | 2000-02-09 | 2003-09-17 | Rolls Royce Plc | Engine arrangement |
WO2004026689A1 (fr) * | 2002-09-17 | 2004-04-01 | Bell Helicopter Textron Inc. | Systeme de montage de moteurs decouples en torsion |
GB0328671D0 (en) * | 2003-12-11 | 2004-01-14 | Rolls Royce Plc | Aircraft engine mounting |
FR2869589B1 (fr) * | 2004-04-28 | 2007-08-10 | Airbus France Sas | Dispositif d'attache d'un moteur sur une aile d'un aeronef |
FR2873985B1 (fr) * | 2004-08-04 | 2006-11-24 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2873986B1 (fr) * | 2004-08-04 | 2007-12-21 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2891246B1 (fr) * | 2005-09-26 | 2007-10-26 | Airbus France Sas | Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur |
FR2891251B1 (fr) * | 2005-09-28 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
SE535991C2 (sv) * | 2011-07-07 | 2013-03-19 | Bae Systems Bofors Ab | Rotationsstabiliserad styrbar projektil och förfarande därför |
FR2989952B1 (fr) * | 2012-04-27 | 2014-04-18 | Aircelle Sa | Nacelle de turboreacteur a section aval |
US8979020B2 (en) | 2013-06-07 | 2015-03-17 | Pratt & Whitney Canada Corp. | Mounting system for mounting engine nacelle components and associated method |
US10144524B2 (en) * | 2013-06-14 | 2018-12-04 | Rohr, Inc. | Assembly for mounting a turbine engine to a pylon |
CA2918320C (fr) | 2013-07-26 | 2018-05-15 | Mra Systems, Inc. | Mat d'accrochage de moteur pour aeronef |
FR3010147B1 (fr) * | 2013-08-28 | 2015-08-21 | Snecma | Suspension isostatique d'un turboreacteur par double support arriere |
FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
US10723471B2 (en) | 2017-06-14 | 2020-07-28 | General Electric Company | Method and system for mounting an aircraft engine |
US10597144B2 (en) * | 2017-12-01 | 2020-03-24 | Hadie Fotouhie | Under the wing-mounted jet engine with pivotal swivel joint to produce directional thrust vectoring thru swivel angle |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3201069A (en) * | 1962-05-31 | 1965-08-17 | Haskin Simon | Jet-propelled aircraft engine mounting |
GB1236917A (en) * | 1967-06-14 | 1971-06-23 | Rolls Royce | Improvements in or relating to means for supporting a gas turbine engine in an aircraft |
US3517897A (en) * | 1968-09-11 | 1970-06-30 | Us Air Force | Multi-module thrust mount |
US3988889A (en) * | 1974-02-25 | 1976-11-02 | General Electric Company | Cowling arrangement for a turbofan engine |
GB1533551A (en) * | 1974-11-08 | 1978-11-29 | Gen Electric | Gas turbofan engines |
US4055041A (en) * | 1974-11-08 | 1977-10-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Integrated gas turbine engine-nacelle |
GB1516980A (en) * | 1974-12-24 | 1978-07-05 | Rolls Royce | Mounting ducted fan gas turbine engines on aircraft |
US4147029A (en) * | 1976-01-02 | 1979-04-03 | General Electric Company | Long duct mixed flow gas turbine engine |
US4458863A (en) * | 1980-03-10 | 1984-07-10 | The Boeing Company | Strut supported inlet |
US4506850A (en) * | 1983-01-04 | 1985-03-26 | The Boeing Company | Engine installation for aircraft |
US4555078A (en) * | 1983-12-27 | 1985-11-26 | Societe Belge D'exploitation De La Navigation Aerienne (Sabena) | Apparatus for the suspension of an aircraft engine cowling |
US4717094A (en) * | 1986-05-19 | 1988-01-05 | The Boeing Company | Aircraft engine mount system with vibration isolators |
US4725019A (en) * | 1986-08-11 | 1988-02-16 | The Boeing Company | Aircraft engine mount with vertical vibration isolation |
FR2606081A1 (fr) * | 1986-10-29 | 1988-05-06 | Snecma | Moteur de propulsion a turbines de travail contrarotatives |
FR2622507B1 (fr) * | 1987-10-28 | 1990-01-26 | Snecma | |
US4917331A (en) * | 1988-11-10 | 1990-04-17 | The Boeing Company | Apparatus and methods for reducing aircraft lifting surface flutter |
-
1991
- 1991-05-23 FR FR9106198A patent/FR2676707B1/fr not_active Expired - Fee Related
-
1992
- 1992-05-22 US US07/886,838 patent/US5181675A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2676707A1 (fr) | 1992-11-27 |
US5181675A (en) | 1993-01-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licences | ||
CD | Change of name or company name | ||
TP | Transmission of property | ||
CD | Change of name or company name | ||
ST | Notification of lapse |
Effective date: 20110131 |