SU318515A2 - Air pressure control system in the aircraft pressurized cabin - Google Patents

Air pressure control system in the aircraft pressurized cabin

Info

Publication number
SU318515A2
SU318515A2 SU1416308/23A SU1416308A SU318515A2 SU 318515 A2 SU318515 A2 SU 318515A2 SU 1416308/23 A SU1416308/23 A SU 1416308/23A SU 1416308 A SU1416308 A SU 1416308A SU 318515 A2 SU318515 A2 SU 318515A2
Authority
SU
USSR - Soviet Union
Prior art keywords
pressurized cabin
pressure control
air pressure
cabin
pressure
Prior art date
Application number
SU1416308/23A
Other languages
Russian (ru)
Inventor
В.С. Лебедев
В.Г. Воронин
М.Г. Зазнобин
Ю.Н. Абросимов
Д.Д. Усков
Original Assignee
В.С. Лебедев
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 В.С. Лебедев filed Critical В.С. Лебедев
Priority to SU1416308/23A priority Critical patent/SU318515A2/en
Application granted granted Critical
Publication of SU318515A2 publication Critical patent/SU318515A2/en

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  • Measuring Fluid Pressure (AREA)

Abstract

Система регулирования давления воздуха в гермокабине летательного аппарата по авт. св. № 229966, отличающаяся тем, что, с целью повышения точности регулирования давления, датчик абсолютного давления в гермокабине и выход первого устройства сравнения подсоединены ко входам второго устройства сравнения через н.з. контакты реле, соединенного с сигнализатором выпуска шасси летательного аппарата, а через н.р. контакты реле ко входам второго устройства сравнения подключены датчик разности давления в гермокабине и атмосферного давления и задатчик разности этих давлений, связанный с сигнализатором расхода воздуха линии наддува гермокабины.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 improve the accuracy of pressure control, the absolute pressure sensor in the pressure cabin and the output of the first comparator are connected to the inputs of the second comparator via n.W. the contacts of the relay connected to the aircraft landing gear warning device, and through N. p. the relay contacts to the inputs of the second comparator are connected to a differential pressure sensor in the pressurized cabin and atmospheric pressure, and a unit for the difference of these pressures connected to the air flow indicator of the pressurization line of the pressurized cabin.

SU1416308/23A 1970-03-12 1970-03-12 Air pressure control system in the aircraft pressurized cabin SU318515A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1416308/23A SU318515A2 (en) 1970-03-12 1970-03-12 Air pressure control system in the aircraft pressurized cabin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1416308/23A SU318515A2 (en) 1970-03-12 1970-03-12 Air pressure control system in the aircraft pressurized cabin

Publications (1)

Publication Number Publication Date
SU318515A2 true SU318515A2 (en) 2006-02-10

Family

ID=60514787

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1416308/23A SU318515A2 (en) 1970-03-12 1970-03-12 Air pressure control system in the aircraft pressurized cabin

Country Status (1)

Country Link
SU (1) SU318515A2 (en)

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