GB651085A - Resilient mountings - Google Patents
Resilient mountingsInfo
- Publication number
- GB651085A GB651085A GB7747/48A GB774748A GB651085A GB 651085 A GB651085 A GB 651085A GB 7747/48 A GB7747/48 A GB 7747/48A GB 774748 A GB774748 A GB 774748A GB 651085 A GB651085 A GB 651085A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- mountings
- resilient mountings
- mounting
- ring
- 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/04—Aircraft characterised by the type or position of power plant of piston type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K5/00—Arrangement or mounting of internal-combustion or jet-propulsion units
- B60K5/12—Arrangement of engine supports
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Testing Of Engines (AREA)
Abstract
651,085. Aero-engine mountings. LORD MANUFACTURING CO. March 15, 1948, No. 7747. Convention date, April 17, 1947. [Class 4] [Also in Group XXXII] An aircraft engine is supported on a mounting ring 1, by means of resilient mountings (see Group XXXII), such that a link 7 connecting each mounting with the ring 1 is focused at a point 13 in front of the centre of gravity 4 of the engine.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US651085XA | 1947-04-17 | 1947-04-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB651085A true GB651085A (en) | 1951-03-14 |
Family
ID=22060389
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7747/48A Expired GB651085A (en) | 1947-04-17 | 1948-03-15 | Resilient mountings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB651085A (en) |
-
1948
- 1948-03-15 GB GB7747/48A patent/GB651085A/en not_active Expired
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