SU642919A1 - Air Bleed System - Google Patents

Air Bleed System

Info

Publication number
SU642919A1
SU642919A1 SU2505373/23A SU2505373A SU642919A1 SU 642919 A1 SU642919 A1 SU 642919A1 SU 2505373/23 A SU2505373/23 A SU 2505373/23A SU 2505373 A SU2505373 A SU 2505373A SU 642919 A1 SU642919 A1 SU 642919A1
Authority
SU
USSR - Soviet Union
Prior art keywords
valve
air bleed
bleed system
control unit
position indicator
Prior art date
Application number
SU2505373/23A
Other languages
Russian (ru)
Inventor
Ю.Н. Абросимов
Ю.Л. Анохин
В.Г. Воронин
Ю.П. Лачаев
В.П. Лесников
В.В. Никулин
Original Assignee
Ю.Н. Абросимов
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.Н. Абросимов filed Critical Ю.Н. Абросимов
Priority to SU2505373/23A priority Critical patent/SU642919A1/en
Application granted granted Critical
Publication of SU642919A1 publication Critical patent/SU642919A1/en

Links

Landscapes

  • Control And Safety Of Cranes (AREA)

Abstract

Система отбора воздуха на летательном аппарате, содержащая обратный клапан на линии, подключенной к ступени низкого давления компрессора двигателя, оборудованного сигнализатором положения рычага управления, и перекрывной кран на линии, подключенной к ступени высокого давления, датчик которого связан с узлом управления этим краном, отличающаяся тем, что, с целью повышения надежности работы путем снижения динамических забросов давления на входе, в цепь прохождения сигнала между указанным узлом управления и краном включен логический элемент "И", второй вход которого связан с сигнализатором положения рычага управления двигателем.An air bleed system on an aircraft that contains a non-return valve on a line connected to a low pressure stage of an engine compressor equipped with a control lever position indicator and a shut off valve on a line connected to a high pressure stage whose sensor is connected to the control unit of this valve that, in order to increase the reliability of work by reducing the dynamic pressure drops at the inlet, a logical element is included in the signal transmission circuit between the specified control unit and the crane ment "And", the second input of which is connected to the position indicator of the engine control lever.

SU2505373/23A 1977-07-08 1977-07-08 Air Bleed System SU642919A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2505373/23A SU642919A1 (en) 1977-07-08 1977-07-08 Air Bleed System

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2505373/23A SU642919A1 (en) 1977-07-08 1977-07-08 Air Bleed System

Publications (1)

Publication Number Publication Date
SU642919A1 true SU642919A1 (en) 2006-03-27

Family

ID=60520943

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2505373/23A SU642919A1 (en) 1977-07-08 1977-07-08 Air Bleed System

Country Status (1)

Country Link
SU (1) SU642919A1 (en)

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