GB501006A - Improvements in devices for the mounting of an engine or like apparatus on its support - Google Patents
Improvements in devices for the mounting of an engine or like apparatus on its supportInfo
- Publication number
- GB501006A GB501006A GB22284/37A GB2228437A GB501006A GB 501006 A GB501006 A GB 501006A GB 22284/37 A GB22284/37 A GB 22284/37A GB 2228437 A GB2228437 A GB 2228437A GB 501006 A GB501006 A GB 501006A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- members
- support
- mounting
- aug
- 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
- 241001247986 Calotropis procera Species 0.000 abstract 2
- 238000013016 damping Methods 0.000 abstract 1
- 230000009699 differential effect Effects 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 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 POWERÂ PLANTSÂ 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)
- Vibration Prevention Devices (AREA)
Abstract
501,006. Resilient supports; dashpots. BENAUX. E. P., and RENAUX, L. J. Aug. 13, 1937, No. 22284. Convention date, Aug. 17, 1936. [Class 108 (iii)] [Also in Groups XXXIII and XXXI] An engine or other apparatus having parts rotating or oscillating about an axis is mounted on a support or frame by means which include at least one member mounted through the intermediary of an elastic ring adapted to damp vibrations of small amplitude on an axle substantially parallel to the axis of rotation, the member being connected with the apparatus and formed with an arm connected with a damping device carried by the support and adapted to damp vibrations of large amplitude. In one form, an aircraft engine 1 is supported in a cradle 2, 3. The members 2 are arranged parallel to the engine crankshaft and are connected by rubber bushes 7 to shafts 5 which are connected by links 8 and rubber bushes to beams 13 forming part of the aircraft framework 14. One or more of the links 8 are provided with extensions 15 connected to members 16, 17 between which and members 21 are disposed pneumatic members 18. In a modification the mounting is applied to a radial aero-engine in which case the engine mounting ring acts through gear teeth arranged between the mounting ring and the arm engaging the member. The pneumatic member may be replaced by a dashpot having a piston centralized by springs and provided with a metering orifice and a non-return valve in order to give a differential action.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR501006X | 1936-08-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB501006A true GB501006A (en) | 1939-02-13 |
Family
ID=8905437
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB22284/37A Expired GB501006A (en) | 1936-08-17 | 1937-08-13 | Improvements in devices for the mounting of an engine or like apparatus on its support |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB501006A (en) |
-
1937
- 1937-08-13 GB GB22284/37A patent/GB501006A/en not_active Expired
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