GB585074A - Improvements relating to the prevention of ice-formation on the propellors of aircraft - Google Patents
Improvements relating to the prevention of ice-formation on the propellors of aircraftInfo
- Publication number
- GB585074A GB585074A GB773/45A GB77345A GB585074A GB 585074 A GB585074 A GB 585074A GB 773/45 A GB773/45 A GB 773/45A GB 77345 A GB77345 A GB 77345A GB 585074 A GB585074 A GB 585074A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- energy
- propellors
- ice
- prevention
- 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
- 230000002265 prevention Effects 0.000 title 1
- 238000004804 winding Methods 0.000 abstract 2
- 238000010438 heat treatment 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
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
Abstract
585,074. De-icing propellers. BRITISH THOMSON - HOUSTON CO., Ltd., and CLARK, L. J. Jan 9, 1945, No. 773. Addition to 525,452. [Class 114] An arrangement for heating parts of contrarotating airscrews for aircraft wherein electrical energy for the heater 17 on the forward airscrew 1 is supplied by a rotary transformer has its secondary winding 16 rotating with the hub 2 and its primary winding 15 rotating with a hub 5 on which is mounted the rear airscrew 4, the heater 14 for which is supplied with energy, together with the primary 15, through slip-rings 13 and bushes 11 from a source of energy on the aircraft. Source of energy may be either A.C. as in the parent Specification, or D.C. as in Specification 545,298. Specification 584,563 also is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB773/45A GB585074A (en) | 1945-01-09 | 1945-01-09 | Improvements relating to the prevention of ice-formation on the propellors of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB773/45A GB585074A (en) | 1945-01-09 | 1945-01-09 | Improvements relating to the prevention of ice-formation on the propellors of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB585074A true GB585074A (en) | 1947-01-29 |
Family
ID=9710273
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB773/45A Expired GB585074A (en) | 1945-01-09 | 1945-01-09 | Improvements relating to the prevention of ice-formation on the propellors of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB585074A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2674420A (en) * | 1949-05-06 | 1954-04-06 | Lockheed Aircraft Corp | Antenna installation |
US2742248A (en) * | 1952-02-16 | 1956-04-17 | Curtiss Wright Corp | Propeller blade de-icing |
-
1945
- 1945-01-09 GB GB773/45A patent/GB585074A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2674420A (en) * | 1949-05-06 | 1954-04-06 | Lockheed Aircraft Corp | Antenna installation |
US2742248A (en) * | 1952-02-16 | 1956-04-17 | Curtiss Wright Corp | Propeller blade de-icing |
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