SU1403538A1 - AIR-HEAT ANTI-FRONT SYSTEM OF AIRPLANE ENGINE - Google Patents

AIR-HEAT ANTI-FRONT SYSTEM OF AIRPLANE ENGINE

Info

Publication number
SU1403538A1
SU1403538A1 SU4116333/23A SU4116333A SU1403538A1 SU 1403538 A1 SU1403538 A1 SU 1403538A1 SU 4116333/23 A SU4116333/23 A SU 4116333/23A SU 4116333 A SU4116333 A SU 4116333A SU 1403538 A1 SU1403538 A1 SU 1403538A1
Authority
SU
USSR - Soviet Union
Prior art keywords
air
engine
front system
control unit
airplane engine
Prior art date
Application number
SU4116333/23A
Other languages
Russian (ru)
Inventor
Ю.А. Куранов
О.Н. Кашелевский
Original Assignee
Ю.А. Куранов
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Ю.А. Куранов filed Critical Ю.А. Куранов
Priority to SU4116333/23A priority Critical patent/SU1403538A1/en
Application granted granted Critical
Publication of SU1403538A1 publication Critical patent/SU1403538A1/en

Links

Abstract

Воздушно-тепловая противообледенительная система двигателя самолета, содержащая блок управления, трубопровод отбора воздуха от компрессора двигателя, в котором установлены заслонка с приводом, датчик избыточного давления и эжектор, соединенный с противообледенителем, отличающаяся тем, что, с целью повышения экономичности системы путем уменьшения расхода воздуха, отбираемого от двигателя, система снабжена датчиком оборотов двигателя и переключателем режимов, которые соединены с соответствующими входами блока управления, выход которого соединен с приводом заслонки.Air-thermal de-icing system of an aircraft engine, comprising a control unit, an air extraction pipe from an engine compressor, in which a motorized damper is installed, an overpressure sensor and an ejector connected to an anti-icer, characterized in that, in order to increase the system efficiency by reducing air flow taken from the engine, the system is equipped with an engine speed sensor and a mode switch, which are connected to the corresponding inputs of the control unit, the output is It is connected to the flap drive.

SU4116333/23A 1986-06-30 1986-06-30 AIR-HEAT ANTI-FRONT SYSTEM OF AIRPLANE ENGINE SU1403538A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4116333/23A SU1403538A1 (en) 1986-06-30 1986-06-30 AIR-HEAT ANTI-FRONT SYSTEM OF AIRPLANE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4116333/23A SU1403538A1 (en) 1986-06-30 1986-06-30 AIR-HEAT ANTI-FRONT SYSTEM OF AIRPLANE ENGINE

Publications (1)

Publication Number Publication Date
SU1403538A1 true SU1403538A1 (en) 2005-02-20

Family

ID=60535906

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4116333/23A SU1403538A1 (en) 1986-06-30 1986-06-30 AIR-HEAT ANTI-FRONT SYSTEM OF AIRPLANE ENGINE

Country Status (1)

Country Link
SU (1) SU1403538A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2604921C2 (en) * 2015-05-06 2016-12-20 Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") Method of ice and snow removing from aircraft surface

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2604921C2 (en) * 2015-05-06 2016-12-20 Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") Method of ice and snow removing from aircraft surface

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