GB455248A - Improvements in cowls for air-cooled aircraft engines - Google Patents
Improvements in cowls for air-cooled aircraft enginesInfo
- Publication number
- GB455248A GB455248A GB2254535A GB2254535A GB455248A GB 455248 A GB455248 A GB 455248A GB 2254535 A GB2254535 A GB 2254535A GB 2254535 A GB2254535 A GB 2254535A GB 455248 A GB455248 A GB 455248A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flaps
- members
- bristol
- slots
- cowling
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P7/00—Controlling of coolant flow
- F01P7/02—Controlling of coolant flow the coolant being cooling-air
- F01P7/023—Cowlings for airplane engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Automatic Assembly (AREA)
- Testing Of Engines (AREA)
Abstract
455,248. Propelling aircraft. BRISTOL AEROPLANE CO.,Ltd., Bristol, and FEDDEN, A. H. R., Filton House, and COPLEY, J. W., 44, Norton Road, Knowle, both in Bristol. Aug. 9, 1935, No. 22545. [Class 4] [See also Group XXVII] Adjustable flaps 14, at the rear of an aircraft engine cowling 11, are mounted in slots in the sides of actuating members 19 and thus present a continuous rear edge in all positions of adjustment. The flaps are retained by spring-pressed T-shaped members 28 which engage recesses in their edges. The members 19 are pivoted to brackets 16, mounted on a rectangular-sectioned metal ring 12 which supports the cowling by connections 13 from the cylinder head. End flaps 41 on each side of the exhaust pipe 40 are supported on one side only by pins 44 which engage L-shaped slots in the flaps by spring clips engaging the underside of the members 19. The flaps are operated as described in Specification 455,249, [Group XXVII], by an endless chain 49, rotated by a handle 58, or by electric, or hydraulic power. The movement may be controlled by a thermal device. The Provisional Specification describes fixing the flaps by dowel pins adjacent the pivots.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2254535A GB455248A (en) | 1935-08-09 | 1935-08-09 | Improvements in cowls for air-cooled aircraft engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2254535A GB455248A (en) | 1935-08-09 | 1935-08-09 | Improvements in cowls for air-cooled aircraft engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB455248A true GB455248A (en) | 1936-10-16 |
Family
ID=10181140
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2254535A Expired GB455248A (en) | 1935-08-09 | 1935-08-09 | Improvements in cowls for air-cooled aircraft engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB455248A (en) |
-
1935
- 1935-08-09 GB GB2254535A patent/GB455248A/en not_active Expired
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