GB530385A - Aircraft engine mounting - Google Patents
Aircraft engine mountingInfo
- Publication number
- GB530385A GB530385A GB16988/39A GB1698839A GB530385A GB 530385 A GB530385 A GB 530385A GB 16988/39 A GB16988/39 A GB 16988/39A GB 1698839 A GB1698839 A GB 1698839A GB 530385 A GB530385 A GB 530385A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- band
- engine mounting
- aircraft engine
- aero
- 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
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
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
530,385. Aero-engine mountings. POTEZ, H. C. A. June 9, 1939, No. 16988. Convention date, March 23, 1939. [Class 4] An aero-engine mounting includes a band or strap 5, 6 connected at its outer ends 3, 4 to the aircraft structure and to the ports which directly support the engine. As shown, the engine is resiliently or otherwise secured on bearers 11, 12 rigidly or pivotally secured to the band and connected at 16, 17 to the aircraft structure. The band may be in two parts pivotally ccnnected together.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR530385X | 1939-03-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB530385A true GB530385A (en) | 1940-12-11 |
Family
ID=8923244
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16988/39A Expired GB530385A (en) | 1939-03-23 | 1939-06-09 | Aircraft engine mounting |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB530385A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3259099A (en) * | 1964-06-08 | 1966-07-05 | Kiekhaefer Corp | Aligned inboard engine suspension for inboard-outboard drives |
US5467941A (en) * | 1993-12-30 | 1995-11-21 | The Boeing Company | Pylon and engine installation for ultra-high by-pass turbo-fan engines |
-
1939
- 1939-06-09 GB GB16988/39A patent/GB530385A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3259099A (en) * | 1964-06-08 | 1966-07-05 | Kiekhaefer Corp | Aligned inboard engine suspension for inboard-outboard drives |
US5467941A (en) * | 1993-12-30 | 1995-11-21 | The Boeing Company | Pylon and engine installation for ultra-high by-pass turbo-fan engines |
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