JPS5035898A - - Google Patents
Info
- Publication number
- JPS5035898A JPS5035898A JP49066439A JP6643974A JPS5035898A JP S5035898 A JPS5035898 A JP S5035898A JP 49066439 A JP49066439 A JP 49066439A JP 6643974 A JP6643974 A JP 6643974A JP S5035898 A JPS5035898 A JP S5035898A
- Authority
- JP
- Japan
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US00369692A US3836100A (en) | 1973-06-13 | 1973-06-13 | Engine mounting arrangement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5035898A true JPS5035898A (ja) | 1975-04-04 |
Family
ID=23456505
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP49066439A Pending JPS5035898A (ja) | 1973-06-13 | 1974-06-11 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3836100A (ja) |
| JP (1) | JPS5035898A (ja) |
| CA (1) | CA985251A (ja) |
| DE (1) | DE2417065A1 (ja) |
| FR (1) | FR2233227B1 (ja) |
| GB (1) | GB1467468A (ja) |
| IL (1) | IL44603A (ja) |
| IT (1) | IT1014823B (ja) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000179359A (ja) * | 1998-12-17 | 2000-06-27 | United Technol Corp <Utc> | ギアボックス用の可変剛性位置決めリンク |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3983602A (en) * | 1975-06-11 | 1976-10-05 | Barry Robert L | Implement holder for a safety helmet |
| FR2441902A2 (fr) * | 1978-11-15 | 1980-06-13 | Aerospatiale | Dispositif de suspension multidirectionnelle pour giravion |
| CA1151626A (en) * | 1980-04-11 | 1983-08-09 | Leon L. Hulett | Vibration isolator |
| US4725019A (en) * | 1986-08-11 | 1988-02-16 | The Boeing Company | Aircraft engine mount with vertical vibration isolation |
| 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 |
| US5065959A (en) * | 1989-11-21 | 1991-11-19 | The Boeing Company | Vibration damping aircraft engine attachment |
| US5551650A (en) * | 1994-06-16 | 1996-09-03 | Lord Corporation | Active mounts for aircraft engines |
| US6328293B1 (en) | 1998-09-18 | 2001-12-11 | Lord Corporation | Multi-linkage suspension system including outboard isolators |
| DE60228137D1 (ja) * | 2002-09-17 | 2008-09-18 | Bell Helicopter Textron Inc | |
| FR2872784B1 (fr) * | 2004-07-09 | 2007-10-12 | Eurocopter France | Systeme de suspension d'un moteur d'aeronef a voilure tournante |
| US8042793B2 (en) * | 2006-09-06 | 2011-10-25 | Honda Motor Co., Ltd. | Solid engine mount |
| US7784773B1 (en) | 2009-08-04 | 2010-08-31 | Itt Manufacturing Enterprises, Inc. | Isolator useful for in-line mounting with a strut |
| US9783312B2 (en) | 2014-07-10 | 2017-10-10 | Honeywell International Inc. | Method and apparatus for reducing high transient mount load in aircraft engine mounting systems |
| US10336459B2 (en) | 2016-02-01 | 2019-07-02 | Bell Helicopter Textron Inc. | Clamped splines for aircraft engine mount assemblies |
| US10384790B2 (en) | 2016-02-01 | 2019-08-20 | Bell Textron Inc. | Engine mount assemblies for aircraft |
| CN109264003B (zh) * | 2018-09-04 | 2021-11-12 | 西北工业大学 | 一种脉冲爆震发动机的推力转换器 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2380274A (en) * | 1940-11-04 | 1945-07-10 | Eleanor J Trott | Airplane engine mounting |
| US2753140A (en) * | 1951-07-28 | 1956-07-03 | United Aircraft Corp | Engine mount |
| US3056569A (en) * | 1954-09-29 | 1962-10-02 | Textron Inc | Airplane engine suspension system |
| US2936978A (en) * | 1957-03-29 | 1960-05-17 | United Aircraft Corp | Rear engine mount |
| GB969806A (en) * | 1962-05-16 | 1964-09-16 | Rolls Royce | Improvements relating to the installation of jet engines in engine bays |
| US3288404A (en) * | 1964-08-24 | 1966-11-29 | Lord Corp | Engine mounting system |
-
1973
- 1973-06-13 US US00369692A patent/US3836100A/en not_active Expired - Lifetime
-
1974
- 1974-03-29 CA CA196,415A patent/CA985251A/en not_active Expired
- 1974-04-08 DE DE2417065A patent/DE2417065A1/de not_active Ceased
- 1974-04-10 IL IL44603A patent/IL44603A/en unknown
- 1974-05-07 FR FR7416375A patent/FR2233227B1/fr not_active Expired
- 1974-05-17 GB GB2208374A patent/GB1467468A/en not_active Expired
- 1974-06-06 IT IT23667/74A patent/IT1014823B/it active
- 1974-06-11 JP JP49066439A patent/JPS5035898A/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000179359A (ja) * | 1998-12-17 | 2000-06-27 | United Technol Corp <Utc> | ギアボックス用の可変剛性位置決めリンク |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1467468A (en) | 1977-03-16 |
| IT1014823B (it) | 1977-04-30 |
| FR2233227B1 (ja) | 1978-01-20 |
| IL44603A (en) | 1977-10-31 |
| US3836100A (en) | 1974-09-17 |
| IL44603A0 (en) | 1974-07-31 |
| FR2233227A1 (ja) | 1975-01-10 |
| DE2417065A1 (de) | 1975-01-09 |
| CA985251A (en) | 1976-03-09 |