GB484481A - Improvements in and relating to elastic suspension arrangements, more particularly the suspension of aeroplane engines - Google Patents
Improvements in and relating to elastic suspension arrangements, more particularly the suspension of aeroplane enginesInfo
- Publication number
- GB484481A GB484481A GB29834/36A GB2983436A GB484481A GB 484481 A GB484481 A GB 484481A GB 29834/36 A GB29834/36 A GB 29834/36A GB 2983436 A GB2983436 A GB 2983436A GB 484481 A GB484481 A GB 484481A
- Authority
- GB
- United Kingdom
- Prior art keywords
- suspension
- rings
- relating
- metal rings
- aeroplane engines
- 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
- 239000000725 suspension Substances 0.000 title abstract 4
- 239000002184 metal Substances 0.000 abstract 3
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)
- Springs (AREA)
- Vibration Prevention Devices (AREA)
Abstract
484,481. Resilient mountings. GOLDSCHMIDT, M. Nov. 2, 1936, No. 29834. Convention date, Npv. 2, 1935. [Class 108 (iii)] An elastic suspension between a loading and a supporting part and particularly for aeroplane engines, includes a number of concentrically-arranged cylindrical metal rings and rubber disposed between the rings and vulcanized thereto, the metal rings being connected alternately to the loading and supporting parts. As shown, metal rings 6, 13 surround a spigot 1 in a housing 8. Alternate rings 6, 13, respectively, are connected to arms 2, 3 and 10, 11 carried respectively on the spigot and housing. A plurality of the suspension units may be disposed end-to-end to form a unitary mounting.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE484481X | 1935-11-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB484481A true GB484481A (en) | 1938-05-02 |
Family
ID=6543134
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29834/36A Expired GB484481A (en) | 1935-11-02 | 1936-11-02 | Improvements in and relating to elastic suspension arrangements, more particularly the suspension of aeroplane engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB484481A (en) |
-
1936
- 1936-11-02 GB GB29834/36A patent/GB484481A/en not_active Expired
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