GB421761A - Cowling for aircraft engines - Google Patents
Cowling for aircraft enginesInfo
- Publication number
- GB421761A GB421761A GB3505433A GB3505433A GB421761A GB 421761 A GB421761 A GB 421761A GB 3505433 A GB3505433 A GB 3505433A GB 3505433 A GB3505433 A GB 3505433A GB 421761 A GB421761 A GB 421761A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cowling
- flange
- air
- flow
- aircraft 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
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)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
421,761. Cooling cylinders. ARMSTRONG SIDDELEY MOTORS, Ltd., and REYNOLDS, R., Park Side, Coventry. Dec. 13, 1933, No. 35054. [Class 7 (ii)] [See also Group XXXIII] An air-cooled star-stype aircraft engine 13 is surrounded by an annular sheet-metal cowling 12 approximating in shape to an N.A.C.A. cowling or Townend ring and which is provided with a radial flange 17 of single thickness or of V or other section in order to prevent excessive flow of air along the inside wall of the cowling, the flange being attached to a circular band 18 lying flat over the cylinder heads. An gap 15 between the cowling and fuselage 14 forms the exit for the flow of air which enters through the open end 19 of the cowling. The flange 17 is cut away to receive the valve mechanism or rocker casings. The cowling may be built up in two or more sections.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3505433A GB421761A (en) | 1933-12-13 | 1933-12-13 | Cowling for aircraft engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3505433A GB421761A (en) | 1933-12-13 | 1933-12-13 | Cowling for aircraft engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB421761A true GB421761A (en) | 1934-12-31 |
Family
ID=10373247
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3505433A Expired GB421761A (en) | 1933-12-13 | 1933-12-13 | Cowling for aircraft engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB421761A (en) |
-
1933
- 1933-12-13 GB GB3505433A patent/GB421761A/en not_active Expired
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