GB547371A - Improvements in and relating to apparatus for the prevention of ice formation on aeroplane propellers - Google Patents
Improvements in and relating to apparatus for the prevention of ice formation on aeroplane propellersInfo
- Publication number
- GB547371A GB547371A GB6475/41A GB647541A GB547371A GB 547371 A GB547371 A GB 547371A GB 6475/41 A GB6475/41 A GB 6475/41A GB 647541 A GB647541 A GB 647541A GB 547371 A GB547371 A GB 547371A
- Authority
- GB
- United Kingdom
- Prior art keywords
- freedom
- ring
- swivel
- joints
- blade
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
Abstract
547,371. De-icing aircraft propellers. BRITISH THOMSON-HOUSTON CO., Ltd., and CLARK, L. T. May 20, 1941, No. 6475. [Class 114] In apparatus fo de-icing the blade of variable-pitch aircraft propellers a rigid ring 6 i supported from the root of each blade 2 by means of ; strap 11 and a swivel joint 8 having two degrees of freedom The ring 6 carrie one or more bracket 12 with a swive joint 13, having two degrees of freedom for one end of a radius arm or tube 7, the other end o which is carried by a swivel joint 14 having a single degree of freedom, carried by the propeller hub. The conductors 4 from the terminal block of a hubmounted generator 5 run along or through the arm or tube 7 and across the swivel joints 14, 8 with sufficient free length to permit flexure about the joints, to supply current to heaters 3 mounted on the blades 2. The brackets 12 may be eliminated by mounting the swivel joints 13 directly on the ring 6. Specifications 525,452 and 545,298 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB6475/41A GB547371A (en) | 1941-05-20 | 1941-05-20 | Improvements in and relating to apparatus for the prevention of ice formation on aeroplane propellers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB6475/41A GB547371A (en) | 1941-05-20 | 1941-05-20 | Improvements in and relating to apparatus for the prevention of ice formation on aeroplane propellers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB547371A true GB547371A (en) | 1942-08-25 |
Family
ID=9815151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6475/41A Expired GB547371A (en) | 1941-05-20 | 1941-05-20 | Improvements in and relating to apparatus for the prevention of ice formation on aeroplane propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB547371A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2564325A (en) * | 1946-04-04 | 1951-08-14 | Goodrich Co B F | Heated propeller covering |
US3042346A (en) * | 1959-04-15 | 1962-07-03 | Gen Motors Corp | Wiring harness for electrically heated variable pitch propeller blade |
CN112088129A (en) * | 2018-05-07 | 2020-12-15 | 赛峰航空器发动机 | Aircraft propulsion assembly provided with a rotary transformer for supplying electrical energy to the blades |
-
1941
- 1941-05-20 GB GB6475/41A patent/GB547371A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2564325A (en) * | 1946-04-04 | 1951-08-14 | Goodrich Co B F | Heated propeller covering |
US3042346A (en) * | 1959-04-15 | 1962-07-03 | Gen Motors Corp | Wiring harness for electrically heated variable pitch propeller blade |
CN112088129A (en) * | 2018-05-07 | 2020-12-15 | 赛峰航空器发动机 | Aircraft propulsion assembly provided with a rotary transformer for supplying electrical energy to the blades |
CN112088129B (en) * | 2018-05-07 | 2023-06-27 | 赛峰航空器发动机 | Aircraft propulsion assembly provided with a resolver for providing electric energy to the blades |
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