GB525452A - Improvements in and relating to means for heating parts of aircraft - Google Patents
Improvements in and relating to means for heating parts of aircraftInfo
- Publication number
- GB525452A GB525452A GB5778/39A GB577839A GB525452A GB 525452 A GB525452 A GB 525452A GB 5778/39 A GB5778/39 A GB 5778/39A GB 577839 A GB577839 A GB 577839A GB 525452 A GB525452 A GB 525452A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fixed
- aircraft
- rotating
- attached
- heaters
- 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
525,452. Electric heating; de-icing. BRITISH THOMSON-HOUSTON CO., Ltd., and CLARK. .L. J. Feb. 21, 1939, No. 5778. [Class 39 (iii)] [Also in Groups XXXIII and XXXV] The rotating parts of an aircraft are heated to prevent ice formation by electric heaters 7 fixed to or embedded in the spinner 3 the airscrew blades 2 or other rotating part and supplied with current from a transformer having a secondary coil 10 attached to the hub of the screw, and a primary coil 11 attached to the engine or other fixed part. The coils are surrounded by a magnetic core 13. The coil windings may be arranged in slots in concentric cylindrical cores similar to the stator and rotor of an induction motor, or they may be wound on salient poles formed on the fixed or rotating core. In place of resistance wires, the heaters may be formed of films of paint having conducting material in colloidal form held in suspension.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5778/39A GB525452A (en) | 1939-02-21 | 1939-02-21 | Improvements in and relating to means for heating parts of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5778/39A GB525452A (en) | 1939-02-21 | 1939-02-21 | Improvements in and relating to means for heating parts of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB525452A true GB525452A (en) | 1940-08-28 |
Family
ID=9802442
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5778/39A Expired GB525452A (en) | 1939-02-21 | 1939-02-21 | Improvements in and relating to means for heating parts of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB525452A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2440115A (en) * | 1948-04-20 | Deiging system foi | ||
US2444557A (en) * | 1943-02-04 | 1948-07-06 | United Aircraft Corp | Propeller anti-icer |
US2503451A (en) * | 1944-01-11 | 1950-04-11 | Curtiss Wright Corp | Deicing system for aircraft surfaces |
US2699303A (en) * | 1947-10-24 | 1955-01-11 | Rotol Ltd | Means for electrically heating the spinners of airscrews |
FR2961176A1 (en) * | 2010-06-15 | 2011-12-16 | Hispano Suiza Sa | ELECTRICAL SUPPLY OF EQUIPMENT FITTED BY THE ROTOR OF AN AIRCRAFT ENGINE |
CN114291270A (en) * | 2021-12-10 | 2022-04-08 | 武汉航空仪表有限责任公司 | A transmission of electricity structure for paddle anti-icing ice |
-
1939
- 1939-02-21 GB GB5778/39A patent/GB525452A/en not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2440115A (en) * | 1948-04-20 | Deiging system foi | ||
US2444557A (en) * | 1943-02-04 | 1948-07-06 | United Aircraft Corp | Propeller anti-icer |
US2503451A (en) * | 1944-01-11 | 1950-04-11 | Curtiss Wright Corp | Deicing system for aircraft surfaces |
US2699303A (en) * | 1947-10-24 | 1955-01-11 | Rotol Ltd | Means for electrically heating the spinners of airscrews |
FR2961176A1 (en) * | 2010-06-15 | 2011-12-16 | Hispano Suiza Sa | ELECTRICAL SUPPLY OF EQUIPMENT FITTED BY THE ROTOR OF AN AIRCRAFT ENGINE |
WO2011157924A1 (en) * | 2010-06-15 | 2011-12-22 | Hispano-Suiza | Electric power supply for apparatuses supported by the rotor of an aircraft engine |
JP2013531579A (en) * | 2010-06-15 | 2013-08-08 | イスパノ・シユイザ | Power supply to equipment supported by aircraft engine rotors |
US9458729B2 (en) | 2010-06-15 | 2016-10-04 | Labinal Power Systems | Electric power supply for apparatuses supported by the rotor of an aircraft engine |
CN114291270A (en) * | 2021-12-10 | 2022-04-08 | 武汉航空仪表有限责任公司 | A transmission of electricity structure for paddle anti-icing ice |
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