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

Info

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

Links

Landscapes

  • 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)

Similar Documents

Publication Publication Date Title
FR2104861B1 (en)
GB1435203A (en) Aircraft automatic flight control system
GB1194972A (en) Aircraft Pressurization Outflow Valve
GB1104425A (en) Liquid flush control valves
GB1213864A (en) Improvements in or relating to pressure control systems
SU252028A1 (en) The system of automatic pressure control in autonomous hermetic cabins of aircraft
GB1365429A (en) Multiple lift aircraft control system
GB1487684A (en) Aircraft control system
SU400157A1 (en) Pressure control system
ES198375U (en) Receiving security valve device commanded by a pilot valve. (Machine-translation by Google Translate, not legally binding)
CA683183A (en) Dual valve control for cabin pressurization systems
SU268824A2 (en) Actuator valve for pressure control systems in airtight cockpits of aircraft
GB789979A (en) Improvements in or relating to aircraft autopilots
SU415940A1 (en) DEVICE FOR REGULATING THE PRESSURE OF AIR IN THE AIRCRAFT HERMOCABINE
SU871440A2 (en) AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN
GB1019307A (en) Improvements in or relating to gas supply control devices
GB1374160A (en) Pilot operated control valve
SU217969A1 (en) The executive valve of the pressure regulator in the pressurized cabin of the aircraft
SU302980A2 (en) Pressure control device
SU473412A1 (en) PRESSURE REGULATION SYSTEM ON AIRPLANE
SU226362A2 (en) Device for regulating the pressure in the pressurized cabin of aircraft
SU468481A1 (en) PRESSURE CONTROL SYSTEM
GB874486A (en) Improvements in servo systems
SU287474A1 (en) Executive valve for systems of automatic control of air pressure in the aircraft press cage
SU293481A1 (en) Pneumatic pressure control system in the pressurized cabin of the aircraft