RU96120104A - POWER SUPPLY SYSTEM OF DISCONTINUOUS AIRCRAFT SCREW ELEMENTS - Google Patents

POWER SUPPLY SYSTEM OF DISCONTINUOUS AIRCRAFT SCREW ELEMENTS

Info

Publication number
RU96120104A
RU96120104A RU96120104/11A RU96120104A RU96120104A RU 96120104 A RU96120104 A RU 96120104A RU 96120104/11 A RU96120104/11 A RU 96120104/11A RU 96120104 A RU96120104 A RU 96120104A RU 96120104 A RU96120104 A RU 96120104A
Authority
RU
Russia
Prior art keywords
stator
control unit
propeller
power supply
supply system
Prior art date
Application number
RU96120104/11A
Other languages
Russian (ru)
Other versions
RU2098323C1 (en
Inventor
В.М. Комаров
Б.А. Гречушкин
Ю.А. Судник
В.В. Кушнерев
Original Assignee
Йелстаун Корпорейшн Н.В. (Нидерландские Антильские острова)
Filing date
Publication date
Application filed by Йелстаун Корпорейшн Н.В. (Нидерландские Антильские острова) filed Critical Йелстаун Корпорейшн Н.В. (Нидерландские Антильские острова)
Priority to RU96120104A priority Critical patent/RU2098323C1/en
Priority claimed from RU96120104A external-priority patent/RU2098323C1/en
Priority to AU21073/97A priority patent/AU2107397A/en
Priority to PCT/RU1997/000047 priority patent/WO1997024261A1/en
Publication of RU96120104A publication Critical patent/RU96120104A/en
Application granted granted Critical
Publication of RU2098323C1 publication Critical patent/RU2098323C1/en

Links

Claims (1)

Система электропитания противообледенительных элементов винта летательного аппарата, содержащая измерительный преобразователь частоты вращения винта и блок контроля неисправностей, соединенные с блоком управления, электрический генератор с индуктором на статоре и роторной якорной обмоткой, размещенной на валу винта и соединенной с резистивными тепловыми элементами, встроенными в части винта, отличающаяся тем, что она дополнительно снабжена измерительным преобразователем частоты вращения статора и тормозной муфтой, соединенными с блоком управления, причем статор разделен на две части, первая из которых состоит из магнитных элементов, выполнена свободно вращающейся относительно вала вращения винта и соединена с тормозной муфтой и измерительным преобразователем частоты вращения статора, а вторая закреплена неподвижно и имеет обмотку контроля, соединенную с блоком контроля неисправностей.The power supply system of the anti-icing elements of the aircraft propeller screw, comprising a propeller speed measuring transducer and a fault control unit connected to a control unit, an electric generator with an inductor on the stator and a rotor anchor winding located on the propeller shaft and connected to resistive thermal elements integrated into the propeller parts characterized in that it is additionally equipped with a stator speed measuring transducer and a brake clutch connected to the control unit, and the stator is divided into two parts, the first of which consists of magnetic elements, made freely rotating relative to the shaft of rotation of the screw and connected to the brake clutch and the measuring converter of the rotational speed of the stator, and the second is fixed motionless and has a control winding connected to the control unit malfunctions.
RU96120104A 1996-10-17 1996-10-17 Electric power supply system for anti-icing members of aircraft propeller RU2098323C1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
RU96120104A RU2098323C1 (en) 1996-10-17 1996-10-17 Electric power supply system for anti-icing members of aircraft propeller
AU21073/97A AU2107397A (en) 1996-10-17 1997-03-03 System for supplying electrical power to de-icing elements in an aircraft propeller
PCT/RU1997/000047 WO1997024261A1 (en) 1996-10-17 1997-03-03 System for supplying electrical power to de-icing elements in an aircraft propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96120104A RU2098323C1 (en) 1996-10-17 1996-10-17 Electric power supply system for anti-icing members of aircraft propeller

Publications (2)

Publication Number Publication Date
RU96120104A true RU96120104A (en) 1997-09-10
RU2098323C1 RU2098323C1 (en) 1997-12-10

Family

ID=20186349

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96120104A RU2098323C1 (en) 1996-10-17 1996-10-17 Electric power supply system for anti-icing members of aircraft propeller

Country Status (3)

Country Link
AU (1) AU2107397A (en)
RU (1) RU2098323C1 (en)
WO (1) WO1997024261A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060094105A1 (en) * 1998-04-24 2006-05-04 University Hospitals Of Cleveland Mixed cell diagnostic systems for detection of respiratory, herpes and enteric viruses
WO2007107731A2 (en) * 2006-03-17 2007-09-27 Ultra Electronics Limited Ice protection power supply
US9884685B2 (en) * 2014-05-28 2018-02-06 The Boeing Company External case heater for an angle of attack sensor
RU207639U1 (en) * 2021-08-09 2021-11-08 Акционерное общество «Аэроэлектромаш» AIRCRAFT ANTI-ICE DEVICE WITH ADVANCED EMERGENCY PROTECTION

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2281273A1 (en) * 1974-08-05 1976-03-05 Bronzavia Sa Aircraft propeller anti-icing system - has hub mounted generator connected directly to heating elements
FR2355716A2 (en) * 1976-06-23 1978-01-20 Bronzavia Sa Indicator for anti-icing system - is for aircraft propellers to signal that system is working and is independent of rotation speed
SU669638A1 (en) * 1976-12-30 1986-10-07 Предприятие П/Я В-2323 Anti-icing system of flying vehicle
DE3515839A1 (en) * 1984-05-11 1985-11-14 United Technologies Corp., Hartford, Conn. ARRANGEMENT FOR PREVENTING AN ICE PLANE PROPELLER

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