SU252028A1 - The system of automatic pressure control in autonomous hermetic cabins of aircraft - Google Patents

The system of automatic pressure control in autonomous hermetic cabins of aircraft

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Publication number
SU252028A1
SU252028A1 SU1273626/23A SU1273626A SU252028A1 SU 252028 A1 SU252028 A1 SU 252028A1 SU 1273626/23 A SU1273626/23 A SU 1273626/23A SU 1273626 A SU1273626 A SU 1273626A SU 252028 A1 SU252028 A1 SU 252028A1
Authority
SU
USSR - Soviet Union
Prior art keywords
hermetic
autonomous
cabins
aircraft
pressure control
Prior art date
Application number
SU1273626/23A
Other languages
Russian (ru)
Inventor
Г.И. Воронин
М.И. Взоров
Н.А. Вишняков
А.Л. Крицын
Л.Я. Переплетчиков
Original Assignee
Г.И. Воронин
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 Г.И. Воронин filed Critical Г.И. Воронин
Priority to SU1273626/23A priority Critical patent/SU252028A1/en
Application granted granted Critical
Publication of SU252028A1 publication Critical patent/SU252028A1/en

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  • Safety Devices In Control Systems (AREA)

Abstract

Система автоматического регулирования давления в автономных герметических кабинах летательных аппаратов, имеющих не менее двух автономных герметических кабин, включающая дублирующие работу друг друга регуляторы давления каждой кабины, исполнительные клапаны, сигнализаторы давления и срабатывающие от них переключающие устройства, отличающаяся тем, что, с целью повышения надежности работы системы, командные полости упомянутых регуляторов сообщены между собой таким образом, что надмембранные полости "повторителей" исполнительных клапанов каждой герметической кабины через нормально-закрытые каналы упомянутых перекрывающих устройств подключены к командной полости регулятора, управляющего группой исполнительных клапанов другой герметической кабины.The system of automatic pressure control in autonomous hermetic cabins of aircraft, having at least two autonomous hermetic cabs, including duplicating each other's pressure regulators of each cockpit, actuating valves, pressure alarms and switching devices operating from them, in order to improve reliability system operation, the command cavities of the mentioned regulators are communicated with each other in such a way that the overmembrane cavities of the “repeaters” executive The boards of each hermetic cabin through the normally-closed channels of the above-mentioned closing devices are connected to the command chamber of the regulator, which controls the group of actuating valves of the other hermetic cabin.

SU1273626/23A 1968-09-27 1968-09-27 The system of automatic pressure control in autonomous hermetic cabins of aircraft SU252028A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1273626/23A SU252028A1 (en) 1968-09-27 1968-09-27 The system of automatic pressure control in autonomous hermetic cabins of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1273626/23A SU252028A1 (en) 1968-09-27 1968-09-27 The system of automatic pressure control in autonomous hermetic cabins of aircraft

Publications (1)

Publication Number Publication Date
SU252028A1 true SU252028A1 (en) 2006-02-10

Family

ID=60514292

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1273626/23A SU252028A1 (en) 1968-09-27 1968-09-27 The system of automatic pressure control in autonomous hermetic cabins of aircraft

Country Status (1)

Country Link
SU (1) SU252028A1 (en)

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