FR2100606B1 - - Google Patents
Info
- Publication number
- FR2100606B1 FR2100606B1 FR707042824A FR7042824A FR2100606B1 FR 2100606 B1 FR2100606 B1 FR 2100606B1 FR 707042824 A FR707042824 A FR 707042824A FR 7042824 A FR7042824 A FR 7042824A FR 2100606 B1 FR2100606 B1 FR 2100606B1
- Authority
- FR
- France
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
- B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
-
- B64D27/40—
-
- B64D27/404—
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Tires In General (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19691960005 DE1960005B (de) | 1969-11-29 | Aufhängung eines Triebwerkes an einem Luftfahrzeug |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2100606A1 FR2100606A1 (fr) | 1972-03-24 |
FR2100606B1 true FR2100606B1 (fr) | 1974-07-12 |
Family
ID=5752467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR707042824A Expired FR2100606B1 (fr) | 1969-11-29 | 1970-11-27 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3727862A (fr) |
JP (1) | JPS5511560B1 (fr) |
FR (1) | FR2100606B1 (fr) |
GB (1) | GB1328410A (fr) |
Families Citing this family (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1411601A (en) * | 1972-03-04 | 1975-10-29 | Rolls Royce | Ducted fan gas turbine engine supported by an aircraft wing mainspar |
US3809340A (en) * | 1972-12-26 | 1974-05-07 | A Dolgy | Devices for mounting an engine on an aircraft pylon |
US3907220A (en) * | 1974-03-14 | 1975-09-23 | United Aircraft Corp | Rear engine redundant mount |
US4044973A (en) * | 1975-12-29 | 1977-08-30 | The Boeing Company | Nacelle assembly and mounting structures for a turbofan jet propulsion engine |
US4603822A (en) * | 1983-12-08 | 1986-08-05 | The Boeing Company | Aft engine mount |
US5028001A (en) * | 1987-03-13 | 1991-07-02 | General Electric Company | Method of vibration isolating an aircraft engine |
US4875655A (en) * | 1987-03-13 | 1989-10-24 | General Electric Company | Vibration isolating engine mount |
US4776533A (en) * | 1987-03-20 | 1988-10-11 | The Jepson Burns Corporation | Aircraft seat track fitting assembly |
US4805851A (en) * | 1987-08-10 | 1989-02-21 | Herbst Paul T | Turbine engine mounting bracket assembly |
US4917331A (en) * | 1988-11-10 | 1990-04-17 | The Boeing Company | Apparatus and methods for reducing aircraft lifting surface flutter |
US5351930A (en) * | 1992-08-11 | 1994-10-04 | Lord Corporation | Mounting for engines and the like |
FR2738034B1 (fr) * | 1995-08-23 | 1997-09-19 | Snecma | Dispositif de suspension d'un turbopropulseur |
JP3714722B2 (ja) * | 1996-05-09 | 2005-11-09 | 本田技研工業株式会社 | 剥離抑制装置 |
US6328293B1 (en) | 1998-09-18 | 2001-12-11 | Lord Corporation | Multi-linkage suspension system including outboard isolators |
JP3980775B2 (ja) | 1998-10-28 | 2007-09-26 | 本田技研工業株式会社 | 飛行機の造波抵抗低減方法 |
EP0995674B1 (fr) | 1998-10-19 | 2003-08-20 | Honda Giken Kogyo Kabushiki Kaisha | Procédé pour la réduction de la résistance d'onde sur des avions |
JP2000118500A (ja) | 1998-10-19 | 2000-04-25 | Honda Motor Co Ltd | 飛行機の造波抵抗低減方法 |
GB2375513B (en) | 2001-05-19 | 2005-03-23 | Rolls Royce Plc | A mounting arrangement for a gas turbine engine |
FR2872784B1 (fr) * | 2004-07-09 | 2007-10-12 | Eurocopter France | Systeme de suspension d'un moteur d'aeronef a voilure tournante |
FR2873986B1 (fr) * | 2004-08-04 | 2007-12-21 | Airbus France Sas | Ensemble moteur pour aeronef |
US7878448B2 (en) | 2005-04-04 | 2011-02-01 | Lord Corporation | Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit |
US8628040B2 (en) | 2006-01-30 | 2014-01-14 | The Boeing Company | Aircraft configuration |
US8016233B2 (en) * | 2006-01-30 | 2011-09-13 | The Boeing Company | Aircraft configuration |
JP4657192B2 (ja) * | 2006-11-08 | 2011-03-23 | 本田技研工業株式会社 | 飛行機の主翼構造 |
US7900865B2 (en) | 2006-12-19 | 2011-03-08 | The Boeing Company | Airplane configuration |
CA2913375A1 (fr) * | 2007-10-19 | 2009-04-30 | Lord Corporation | Systeme de suspension pour groupe auxiliaire d'energie d'avion muni d'un element elastomere |
US7784773B1 (en) | 2009-08-04 | 2010-08-31 | Itt Manufacturing Enterprises, Inc. | Isolator useful for in-line mounting with a strut |
US20130232768A1 (en) | 2012-03-12 | 2013-09-12 | United Technologies Corporation | Turbine engine case mount and dismount |
EP2641831B1 (fr) * | 2012-03-22 | 2014-12-24 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Atterrisseur à patins pour un giravion |
US10384790B2 (en) * | 2016-02-01 | 2019-08-20 | Bell Textron Inc. | Engine mount assemblies for aircraft |
US10220951B2 (en) * | 2016-02-01 | 2019-03-05 | Bell Helicopter Textron Inc. | Sleeved bolt assemblies for aircraft engine mount assemblies |
CN208170542U (zh) | 2017-12-25 | 2018-11-30 | 广东志高暖通设备股份有限公司 | 一种空调窗机及其风门组件 |
US10814995B2 (en) * | 2017-08-29 | 2020-10-27 | Spirit Aerosystems, Inc. | High-mounted aircraft nacelle |
US20220136440A1 (en) | 2020-10-30 | 2022-05-05 | Raytheon Technologies Corporation | Gas turbine engine mounted above wing and with camber |
US11613372B2 (en) * | 2020-11-09 | 2023-03-28 | Rohr, Inc. | Ducted fan case attachment structure |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4C (de) * | 1877-07-05 | J. E. CHRISTOPH zu Niesky | Kontinuirlicher Maischdestillirapparat mit eigenthümlicher Maisch- u. Spirituskolonne, neuem Maischregulator und neuem Schlemperegulator | |
DE89C (de) * | 1877-08-02 | Deutsche Werkzeugmaschinen -Fabrik, vormals SONDERMANN & STIER in Chemnitz | Fleisch-Hackmaschine | |
FR838666A (fr) * | 1937-11-23 | 1939-03-13 | Perfectionnement à la suspension des moteurs d'avions et autres organes sur des supports soumis à des mouvements alternatifs et notamment les ailes | |
US2761638A (en) * | 1953-11-17 | 1956-09-04 | Gordon L Getline | Vibration-isolating power plant mounting system |
US3057582A (en) * | 1959-05-12 | 1962-10-09 | Rolls Royce | Improved engine mounting |
US3288404A (en) * | 1964-08-24 | 1966-11-29 | Lord Corp | Engine mounting system |
-
1970
- 1970-11-25 GB GB5614170A patent/GB1328410A/en not_active Expired
- 1970-11-27 FR FR707042824A patent/FR2100606B1/fr not_active Expired
- 1970-11-28 JP JP10471470A patent/JPS5511560B1/ja active Pending
- 1970-11-30 US US00093737A patent/US3727862A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3727862A (en) | 1973-04-17 |
FR2100606A1 (fr) | 1972-03-24 |
GB1328410A (en) | 1973-08-30 |
JPS5511560B1 (fr) | 1980-03-26 |
DE1960005A1 (de) | 1971-06-09 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |