GB478752A - Improvements in or relating to the mounting of aircraft engines - Google Patents
Improvements in or relating to the mounting of aircraft enginesInfo
- Publication number
- GB478752A GB478752A GB25669/36A GB2566936A GB478752A GB 478752 A GB478752 A GB 478752A GB 25669/36 A GB25669/36 A GB 25669/36A GB 2566936 A GB2566936 A GB 2566936A GB 478752 A GB478752 A GB 478752A
- Authority
- GB
- United Kingdom
- Prior art keywords
- mounting
- relating
- sept
- aircraft engines
- blocks
- 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
- 239000002184 metal Substances 0.000 abstract 1
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)
- Steroid Compounds (AREA)
Abstract
478,752. Resilient mountings. GETEFO GES. FUR TECHNISCHEN FORTSCHRITT. Sept. 21, 1936, No. 25669. Convention date, Sept. 28, 1935. [Class 108 (iii)] [Also in Group XXXIII] A resilient mounting for aero-engines comprises rubber blocks 7, 10 bonded to flanged metal plates 5, 6. The blocks may be of different hardness and may be subject to differing initial stress.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE478752X | 1935-09-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB478752A true GB478752A (en) | 1938-01-25 |
Family
ID=6542297
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25669/36A Expired GB478752A (en) | 1935-09-28 | 1936-09-21 | Improvements in or relating to the mounting of aircraft engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB478752A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4717094A (en) * | 1986-05-19 | 1988-01-05 | The Boeing Company | Aircraft engine mount system with vibration isolators |
-
1936
- 1936-09-21 GB GB25669/36A patent/GB478752A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4717094A (en) * | 1986-05-19 | 1988-01-05 | The Boeing Company | Aircraft engine mount system with vibration isolators |
EP0250659A2 (en) * | 1986-05-19 | 1988-01-07 | The Boeing Company | Aircraft engine mount system with vibration isolators |
EP0250659A3 (en) * | 1986-05-19 | 1989-05-31 | The Boeing Company | Aircraft engine mount system with vibration isolators |
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