GB584563A - Improvements relating to the prevention of ice formation on the rotating parts of aircraft - Google Patents
Improvements relating to the prevention of ice formation on the rotating parts of aircraftInfo
- Publication number
- GB584563A GB584563A GB82/45A GB8245A GB584563A GB 584563 A GB584563 A GB 584563A GB 82/45 A GB82/45 A GB 82/45A GB 8245 A GB8245 A GB 8245A GB 584563 A GB584563 A GB 584563A
- Authority
- GB
- United Kingdom
- Prior art keywords
- airscrew
- aircraft
- prevention
- rotating parts
- improvements relating
- 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
- 230000015572 biosynthetic process Effects 0.000 title 1
- 230000002265 prevention Effects 0.000 title 1
- 238000004804 winding Methods 0.000 abstract 4
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)
- Transformer Cooling (AREA)
Abstract
584,563. De-icing aircraft propellers. BRITISH THOMSON-HOUSTON CO., Ltd., and CLARK, L. J. Jan. 1, 1945, No. 82. Addition to 525,452. [Class 114] Electrical de-icing equipment for contrarotating airscrews of aircraft consists of electric heaters 11 on the forward airscrew 1 and the boss 18, the heaters being supplied with electrical energy from a rotary transformer having its secondary winding 14 mounted to rotate with the airscrew 1, and its primary winding 15 mounted on a part carrying the rear airscrew 2, this primary winding 15 being energized from the secondary winding of a rotary transformer 17, the primary of which is fixed and is connected to a source of alternating of direct current. This source also supplies energy to the heater in the rear airscrew 2. The transformers are constructed according to the claims of the parent Specification. Specification 545,298 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB82/45A GB584563A (en) | 1945-01-01 | 1945-01-01 | Improvements relating to the prevention of ice formation on the rotating parts of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB82/45A GB584563A (en) | 1945-01-01 | 1945-01-01 | Improvements relating to the prevention of ice formation on the rotating parts of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB584563A true GB584563A (en) | 1947-01-17 |
Family
ID=9698087
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB82/45A Expired GB584563A (en) | 1945-01-01 | 1945-01-01 | Improvements relating to the prevention of ice formation on the rotating parts of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB584563A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2218643A1 (en) * | 2009-02-04 | 2010-08-18 | Alenia Aeronautica S.p.A. | Antiicing system for aircraft propellers |
EP2528203A1 (en) | 2011-05-24 | 2012-11-28 | Eurocopter | Device for supplying electric power to at least one device of a rotating rotor of an aircraft and aircraft |
EP2629407A1 (en) * | 2012-02-17 | 2013-08-21 | Bell Helicopter Textron Inc. | Electrical generator for rotating structure |
EP2664545A1 (en) | 2012-05-16 | 2013-11-20 | Eurocopter | Device for supplying electric power to at least one device of an aircraft rotor and aircraft |
EP2977314A1 (en) * | 2014-07-23 | 2016-01-27 | Hamilton Sundstrand Corporation | Propeller in-hub power generation and control |
FR3057029A1 (en) * | 2016-10-03 | 2018-04-06 | Safran Helicopter Engines | TURBOPROPULSEUR COMPRISING AN INTEGRATED ELECTRICITY GENERATOR |
WO2018065709A1 (en) | 2016-10-03 | 2018-04-12 | Safran Helicopter Engines | Aircraft turboprop equipped with an electrical machine |
WO2019166703A1 (en) | 2018-02-28 | 2019-09-06 | Safran Helicopter Engines | Turboprop comprising an incorporated electricity generator |
EP2768124B1 (en) * | 2013-02-13 | 2019-09-18 | Bell Helicopter Textron Inc. | Brushless alternator for helicopter transmission install |
-
1945
- 1945-01-01 GB GB82/45A patent/GB584563A/en not_active Expired
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2218643A1 (en) * | 2009-02-04 | 2010-08-18 | Alenia Aeronautica S.p.A. | Antiicing system for aircraft propellers |
US8890378B2 (en) | 2011-05-24 | 2014-11-18 | Airbus Helicopters | Electrical power supply device for electrically powering at least one item of equipment on a rotary rotor of an aircraft, and an aircraft |
EP2528203A1 (en) | 2011-05-24 | 2012-11-28 | Eurocopter | Device for supplying electric power to at least one device of a rotating rotor of an aircraft and aircraft |
EP2629407A1 (en) * | 2012-02-17 | 2013-08-21 | Bell Helicopter Textron Inc. | Electrical generator for rotating structure |
US9725179B2 (en) | 2012-02-17 | 2017-08-08 | Universite Du Quebec A Chicoutimi | Electrical generator for rotating structure |
FR2990812A1 (en) * | 2012-05-16 | 2013-11-22 | Eurocopter France | DEVICE FOR ELECTRICALLY SUPPLYING AT LEAST ONE EQUIPMENT OF A ROTOR OF AN AIRCRAFT AND AN AIRCRAFT |
US9067684B2 (en) | 2012-05-16 | 2015-06-30 | Airbus Helicopters | Electrical power supply device for powering at least one piece of equipment of an aircraft rotor, and an aircraft |
EP2664545A1 (en) | 2012-05-16 | 2013-11-20 | Eurocopter | Device for supplying electric power to at least one device of an aircraft rotor and aircraft |
EP2768124B1 (en) * | 2013-02-13 | 2019-09-18 | Bell Helicopter Textron Inc. | Brushless alternator for helicopter transmission install |
EP2977314A1 (en) * | 2014-07-23 | 2016-01-27 | Hamilton Sundstrand Corporation | Propeller in-hub power generation and control |
US9973058B2 (en) | 2014-07-23 | 2018-05-15 | Hamilton Sundstrand Corporation | Propeller in-hub power generation and control |
FR3057029A1 (en) * | 2016-10-03 | 2018-04-06 | Safran Helicopter Engines | TURBOPROPULSEUR COMPRISING AN INTEGRATED ELECTRICITY GENERATOR |
WO2018065709A1 (en) | 2016-10-03 | 2018-04-12 | Safran Helicopter Engines | Aircraft turboprop equipped with an electrical machine |
US10807724B2 (en) * | 2016-10-03 | 2020-10-20 | Safran Helicopter Engines | Aircraft turboprop engine provided with an electric machine |
WO2019166703A1 (en) | 2018-02-28 | 2019-09-06 | Safran Helicopter Engines | Turboprop comprising an incorporated electricity generator |
US11047312B2 (en) | 2018-02-28 | 2021-06-29 | Safran Helicopter Engines | Turboprop comprising an incorporated electricity generator |
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