GB507681A - Improvements in and relating to the mounting of power units in vehicles - Google Patents
Improvements in and relating to the mounting of power units in vehiclesInfo
- Publication number
- GB507681A GB507681A GB4623/38A GB462338A GB507681A GB 507681 A GB507681 A GB 507681A GB 4623/38 A GB4623/38 A GB 4623/38A GB 462338 A GB462338 A GB 462338A GB 507681 A GB507681 A GB 507681A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vehicle
- engine
- secured
- mounting
- feb
- 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
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 230000005484 gravity Effects 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)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Vibration Prevention Devices (AREA)
Abstract
507,681. Mounting motors. VOIGT, C A. Feb. 15, 1938, No. 4623. Convention date, Feb. 15, 1937. [Class 79 (iii)] , [Also in Group XXXIII] A power-unit is resiliently mounted in a vehicle by attachment to the free end of a carrier-member or members secured to the vehicle by rubber-mountings spaced-apart longitudinally of the vehicle. In one form, the member 3, Fig. 1, is anchored in the motor block at 4 and held by a mounting plate 5. The member passes into an aircraft and is mounted in rubber sleeves 7, 13 supported in the end walls of the fuselage 9 and in a bulkhead 11. In a modification, the member 3 telescopes into or onto a tube built into the vehicle body. In a further modification, an aero-engine 1, Fig. 3, is secured to a frusto-conical member 14 mounted through the Intermediary of rubber sleeves 19, 20 on the wing spars 21, 22. In a further form, the member 3 is housed in a recess in the body. In a still further form, a member 24, Fig. 6, projects from the body and is resiliently secured to the member 3, the axis of which passes through the centre of gravity S of the engine unit. The engine may be supported by two laterally-spaced members.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT507681X | 1937-02-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB507681A true GB507681A (en) | 1939-06-20 |
Family
ID=3675499
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4623/38A Expired GB507681A (en) | 1937-02-15 | 1938-02-15 | Improvements in and relating to the mounting of power units in vehicles |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB507681A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2446399A (en) * | 1947-01-10 | 1948-08-03 | Bell Aircraft Corp | Aircraft engine support |
| US3003718A (en) * | 1959-01-19 | 1961-10-10 | David G Peterson | Engine mount for aircraft |
| US4318516A (en) * | 1978-05-30 | 1982-03-09 | Greenmeadow Engineers Limited | Attachment of masses to aircraft and spacecraft |
-
1938
- 1938-02-15 GB GB4623/38A patent/GB507681A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2446399A (en) * | 1947-01-10 | 1948-08-03 | Bell Aircraft Corp | Aircraft engine support |
| US3003718A (en) * | 1959-01-19 | 1961-10-10 | David G Peterson | Engine mount for aircraft |
| US4318516A (en) * | 1978-05-30 | 1982-03-09 | Greenmeadow Engineers Limited | Attachment of masses to aircraft and spacecraft |
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