GB383792A - Improvements in or relating to the cooling and cowling of aircraft or other propeller driving engines - Google Patents
Improvements in or relating to the cooling and cowling of aircraft or other propeller driving enginesInfo
- Publication number
- GB383792A GB383792A GB103632A GB103632A GB383792A GB 383792 A GB383792 A GB 383792A GB 103632 A GB103632 A GB 103632A GB 103632 A GB103632 A GB 103632A GB 383792 A GB383792 A GB 383792A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinders
- air
- spinner
- casing
- cooling
- 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)
- Transmission Devices (AREA)
- Toys (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
383,792. Cooling cylinders. STEVENS A. H., 5, Quality Court, Chancery Lane, London.- (Wright Aeronautical Corporation; Paterson, New Jersey, U.S.A.) Jan. 13, 1932, No. 1086. [Class 7 (ii).] A centrifugal blower for cooling air is arranged in the spinner of an aircraft propeller, the air being used either directly, or through a radiator. The spinner comprises a stream-lined casing 27 having an air entrance 30, reinforced by radial spokes, and a dished back-plate 24 having circumferential ports through which the air, rotated by the roots of the propeller blades, is forced on to curved guide vanes 20 arranged between radial cylinders of the engine. The spaces between adjacent cylinders are closed by baffles 34, which may be attached to the cylinder fins and extend behind individual cylinders, and the air finally issues, with engine exhaust from ports 16, through an annular opening between two fixed fairings 14, 17, a guide 18 being provided. The spinner may include helical blower vanes extending from the hub to the casing 27 and the plate 24 may be replaced by a transverse bar member having arcuate ends closing slots formed in the casing 27 for the propeller blades. Casings; cylinders, pipes for.-The sectioned engine cowling 14 is supported on a ring 21 having angle section and lugs 23 on an annular exhaust manifold having outlets 16 ; alternatively the fairing 14 may be formed in two hinged parts which are clamped together to embrace overhead valve-gear covers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB103632A GB383792A (en) | 1932-01-13 | 1932-01-13 | Improvements in or relating to the cooling and cowling of aircraft or other propeller driving engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB103632A GB383792A (en) | 1932-01-13 | 1932-01-13 | Improvements in or relating to the cooling and cowling of aircraft or other propeller driving engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB383792A true GB383792A (en) | 1932-11-24 |
Family
ID=9715017
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB103632A Expired GB383792A (en) | 1932-01-13 | 1932-01-13 | Improvements in or relating to the cooling and cowling of aircraft or other propeller driving engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB383792A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767871C (en) * | 1937-07-02 | 1954-03-22 | Messerschmitt Boelkow Blohm | Device for the improved utilization of the energy of the exhaust gases in internal combustion engines for propulsion of aircraft |
GB2369161B (en) * | 2000-11-20 | 2004-11-10 | Ajoy Kumar Kundu | Spinner for a propeller |
CN109941425A (en) * | 2019-04-08 | 2019-06-28 | 涂常青 | A kind of two dimensional fluid aircraft |
CN113513399A (en) * | 2021-05-26 | 2021-10-19 | 珠海天晴航空航天科技有限公司 | Aircraft engine and heat dissipation control method thereof |
-
1932
- 1932-01-13 GB GB103632A patent/GB383792A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767871C (en) * | 1937-07-02 | 1954-03-22 | Messerschmitt Boelkow Blohm | Device for the improved utilization of the energy of the exhaust gases in internal combustion engines for propulsion of aircraft |
GB2369161B (en) * | 2000-11-20 | 2004-11-10 | Ajoy Kumar Kundu | Spinner for a propeller |
CN109941425A (en) * | 2019-04-08 | 2019-06-28 | 涂常青 | A kind of two dimensional fluid aircraft |
CN109941425B (en) * | 2019-04-08 | 2023-12-12 | 涂常青 | Two-dimensional fluid aircraft |
CN113513399A (en) * | 2021-05-26 | 2021-10-19 | 珠海天晴航空航天科技有限公司 | Aircraft engine and heat dissipation control method thereof |
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