GB531299A - De-icing apparatus for the airscrews of air-cooled aircraft engines - Google Patents
De-icing apparatus for the airscrews of air-cooled aircraft enginesInfo
- Publication number
- GB531299A GB531299A GB20780/39A GB2078039A GB531299A GB 531299 A GB531299 A GB 531299A GB 20780/39 A GB20780/39 A GB 20780/39A GB 2078039 A GB2078039 A GB 2078039A GB 531299 A GB531299 A GB 531299A
- Authority
- GB
- United Kingdom
- Prior art keywords
- airscrews
- annular channel
- airscrew
- air
- pipes
- 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
- 239000012530 fluid Substances 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
- 238000007710 freezing Methods 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
531,299. De-icing airscrews ; engine accessories. VEREINIGTE DEUTSCHE METALLWERKE AKT.-GES. July 17, 1939, No. 20780. Convention date, Feb. 20. [Classes 4 and 114] De-icing apparatus for the airscrews of aircraft having air-cooled engines with cooling fans mounted in front thereof comprises an annular channel on the fan fed with anti-freezing fluid from a fixed reservoir on the aircraft, branch pipes from the channel leading to the usual annular channel on the airscrew from which pipes lead to the blades. A fan b is shown, driven at a higher speed than the airscrew by gearing f, f<1>, and enclosed by a cowling c. Antifreezing fluid is fed from a pipe n to an annular channel m from which pipes o, o<1> lead to the annular channel i on the airscrew.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE531299X | 1939-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB531299A true GB531299A (en) | 1941-01-01 |
Family
ID=6554893
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20780/39A Expired GB531299A (en) | 1939-02-20 | 1939-07-17 | De-icing apparatus for the airscrews of air-cooled aircraft engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB531299A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2832528A (en) * | 1953-10-01 | 1958-04-29 | Gen Motors Corp | Alcohol mist icing prevention |
-
1939
- 1939-07-17 GB GB20780/39A patent/GB531299A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2832528A (en) * | 1953-10-01 | 1958-04-29 | Gen Motors Corp | Alcohol mist icing prevention |
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