SU873599A2 - AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN - Google Patents

AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN

Info

Publication number
SU873599A2
SU873599A2 SU2943207/23A SU2943207A SU873599A2 SU 873599 A2 SU873599 A2 SU 873599A2 SU 2943207/23 A SU2943207/23 A SU 2943207/23A SU 2943207 A SU2943207 A SU 2943207A SU 873599 A2 SU873599 A2 SU 873599A2
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
air pressure
contacts
open position
supply circuit
Prior art date
Application number
SU2943207/23A
Other languages
Russian (ru)
Inventor
Е.Е. Гавриленков
Л.Р. Егоров
К.П. Ефимов
М.Г. Зазнобин
А.А. Колесников
А.А. Медведев
В.Ф. Хаврошин
Original Assignee
Е.Е. Гавриленков
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 Е.Е. Гавриленков filed Critical Е.Е. Гавриленков
Priority to SU2943207/23A priority Critical patent/SU873599A2/en
Application granted granted Critical
Publication of SU873599A2 publication Critical patent/SU873599A2/en

Links

Abstract

Система регулирования давления воздуха в гермокабине летательного аппарата по авт. св. № 766127, отличающаяся тем, что, с целью повышения надежности работы путем обеспечения своевременности включения и отключения вспомогательного регулятора, в систему введены коммутирующее устройство и сигнализатор открытого положения исполнительного клапана, а узел разрешения выполнен с электроприводом, при этом размыкающие контакты преобразователя и замыкающие контакты сигнализатора открытого положения исполнительного клапана последовательно включены в цепь питания коммутирующего устройства, первые замыкающие контакты которого включены в цепь питания электропривода узла разрешения, а вторые - в цепь питания коммутирующего устройства параллельно с замыкающими контактами сигнализатора открытого положения исполнительного клапана.The system of regulation of air pressure in the pressurized cabin of the aircraft on the bus. St. No. 766127, characterized in that, in order to increase reliability by ensuring timeliness of switching on and off of the auxiliary regulator, a switching device and an open position indicator of the actuating valve are inserted into the system, and the resolution node is electrically operated, while the breaker contacts and the signaling contacts are closed the open position of the actuating valve is connected in series to the power supply circuit of the switching device, the first closing contacts of which are yucheny in motor unit permits the power supply circuit, and the second - in the supply circuit of the switching device in parallel with the make contacts signaling the open position of the valve.

SU2943207/23A 1980-06-19 1980-06-19 AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN SU873599A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2943207/23A SU873599A2 (en) 1980-06-19 1980-06-19 AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2943207/23A SU873599A2 (en) 1980-06-19 1980-06-19 AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN

Publications (1)

Publication Number Publication Date
SU873599A2 true SU873599A2 (en) 2008-05-27

Family

ID=60525294

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2943207/23A SU873599A2 (en) 1980-06-19 1980-06-19 AIR PRESSURE REGULATION SYSTEM IN THE AIRCRAFT GERMAN CABIN

Country Status (1)

Country Link
SU (1) SU873599A2 (en)

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