SU1144310A1 - Air conditioning system on the aircraft - Google Patents

Air conditioning system on the aircraft

Info

Publication number
SU1144310A1
SU1144310A1 SU3668950/23A SU3668950A SU1144310A1 SU 1144310 A1 SU1144310 A1 SU 1144310A1 SU 3668950/23 A SU3668950/23 A SU 3668950/23A SU 3668950 A SU3668950 A SU 3668950A SU 1144310 A1 SU1144310 A1 SU 1144310A1
Authority
SU
USSR - Soviet Union
Prior art keywords
relay
voltage source
closing
closed position
cabin
Prior art date
Application number
SU3668950/23A
Other languages
Russian (ru)
Inventor
С.И. Евсеев
В.Н. Мироненко
В.М. Митрохин
И.П. Шаманин
Original Assignee
С.И. Евсеев
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 С.И. Евсеев filed Critical С.И. Евсеев
Priority to SU3668950/23A priority Critical patent/SU1144310A1/en
Application granted granted Critical
Publication of SU1144310A1 publication Critical patent/SU1144310A1/en

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Landscapes

  • Air Conditioning Control Device (AREA)

Abstract

Система кондиционирования воздуха на летательном аппарате, содержащая теплообменники, турбохолодильник, распределительное устройство, установленное в линии вентиляции негерметичного отсека и сообщенное трубопроводами с входом и узким сечением трубки Вентури, размещенной в линии вентиляции гермокабины, перед краном с ручным управлением и сигнализатором закрытого положения, регулятор температуры воздуха в гермокабине с линией питания от источника напряжения и заслонку подмеса горячего воздуха с каналами управления открыванием и закрыванием, отличающаяся тем, что, с целью повышения надежности и безопасности эксплуатации системы в широком диапазоне режимов работы, она снабжена электромагнитным клапаном, вход которого соединен с узким сечением трубки Вентури, а выход - с окружающей атмосферой, и реле с размыкающим и замыкающими контактами, подключенное к сигнализатору закрытого положения крана с ручным управлением, при этом обмотка электромагнитного клапана соединена с источником напряжения через замыкающий контакт реле, в линии питания регулятора температуры установлен размыкающий контакт реле, а канал управления закрыванием заслонки подмеса горячего воздуха подключен к источнику напряжения через замыкающий контакт реле.Air conditioning system on an aircraft containing heat exchangers, a turbo-cooler, a switchgear installed in the ventilation line of the unpressurized compartment and communicated by pipelines with an inlet and a narrow section of the Venturi tube located in the ventilation cabin of the pressurized cabin, in front of the hand-operated crane and the closed position warning lamp air in a pressurized cabin with a power line from a voltage source and a hot air mixing gate with opening and snatching, characterized in that, in order to improve the reliability and safety of operating the system in a wide range of operating modes, it is equipped with an electromagnetic valve, the inlet of which is connected to a narrow section of the Venturi tube, and the output to the surrounding atmosphere, and a relay with opening and closing contacts, connected to the detector of the closed position of the crane with manual control, while the solenoid winding is connected to the voltage source through the closing contact of the relay, in the supply line of the temperature regulator Credited relay break contact, and closing the damper control mix with the hot air channel is connected to a voltage source via the normally open contact of the relay.

SU3668950/23A 1983-11-29 1983-11-29 Air conditioning system on the aircraft SU1144310A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3668950/23A SU1144310A1 (en) 1983-11-29 1983-11-29 Air conditioning system on the aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3668950/23A SU1144310A1 (en) 1983-11-29 1983-11-29 Air conditioning system on the aircraft

Publications (1)

Publication Number Publication Date
SU1144310A1 true SU1144310A1 (en) 2006-05-27

Family

ID=60540396

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3668950/23A SU1144310A1 (en) 1983-11-29 1983-11-29 Air conditioning system on the aircraft

Country Status (1)

Country Link
SU (1) SU1144310A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2682808C2 (en) * 2014-08-12 2019-03-21 Зе Боинг Компани Ventilation system with air splitting

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2682808C2 (en) * 2014-08-12 2019-03-21 Зе Боинг Компани Ventilation system with air splitting

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