SU398155A2 - Air pressure control system in the aircraft pressurized cabin - Google Patents

Air pressure control system in the aircraft pressurized cabin

Info

Publication number
SU398155A2
SU398155A2 SU1452622/23A SU1452622A SU398155A2 SU 398155 A2 SU398155 A2 SU 398155A2 SU 1452622/23 A SU1452622/23 A SU 1452622/23A SU 1452622 A SU1452622 A SU 1452622A SU 398155 A2 SU398155 A2 SU 398155A2
Authority
SU
USSR - Soviet Union
Prior art keywords
air pressure
control system
pressure control
pressurized cabin
aircraft
Prior art date
Application number
SU1452622/23A
Other languages
Russian (ru)
Inventor
Ю.Н. Абросимов
Г.Н. Андреев
В.Г. Воронин
М.Г. Зазнобин
В.И. Логинов
А.А. Медведев
Д.Д. Усков
Ю.А. Ксенофонтов
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 SU1452622/23A priority Critical patent/SU398155A2/en
Application granted granted Critical
Publication of SU398155A2 publication Critical patent/SU398155A2/en

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  • Control Of Fluid Pressure (AREA)

Abstract

Система регулирования давления воздуха в гермокабине летательного аппарата по авт. св. № 229966, отличающаяся тем, что, с целью повышения надежности, электропневмопреобразователь и дополнительно установленный в систему автономный задатчик давления соединены с управляющей полостью исполнительного механизма через переключатель, в цепь управления которого последовательно включены контакты датчика - реле предельного перепада давлений на стенке кабины и датчика - реле разгерметизации.The system of regulation of air pressure in the pressurized cabin of the aircraft on the bus. St. No. 229966, characterized in that, in order to increase reliability, an electropneumatic converter and an autonomous pressure setting device additionally installed in the system are connected to the control cavity of the actuator via a switch, in the control circuit of which the sensor contacts are connected in series - the limit pressure switch on the cabin wall and the sensor - relay depressurization.

SU1452622/23A 1970-07-13 1970-07-13 Air pressure control system in the aircraft pressurized cabin SU398155A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1452622/23A SU398155A2 (en) 1970-07-13 1970-07-13 Air pressure control system in the aircraft pressurized cabin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1452622/23A SU398155A2 (en) 1970-07-13 1970-07-13 Air pressure control system in the aircraft pressurized cabin

Publications (1)

Publication Number Publication Date
SU398155A2 true SU398155A2 (en) 2006-01-20

Family

ID=60514518

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1452622/23A SU398155A2 (en) 1970-07-13 1970-07-13 Air pressure control system in the aircraft pressurized cabin

Country Status (1)

Country Link
SU (1) SU398155A2 (en)

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