SU430614A1 - AIR CONDITIONING SYSTEM ON AIRCRAFT - Google Patents

AIR CONDITIONING SYSTEM ON AIRCRAFT

Info

Publication number
SU430614A1
SU430614A1 SU1750530/23A SU1750530A SU430614A1 SU 430614 A1 SU430614 A1 SU 430614A1 SU 1750530/23 A SU1750530/23 A SU 1750530/23A SU 1750530 A SU1750530 A SU 1750530A SU 430614 A1 SU430614 A1 SU 430614A1
Authority
SU
USSR - Soviet Union
Prior art keywords
conditioning system
air conditioning
aircraft
cabin
air
Prior art date
Application number
SU1750530/23A
Other languages
Russian (ru)
Inventor
Н.Ф. Наумов
Ю.М. Петров
И.П. Шаманин
Ю.В. Яременко
Original Assignee
Н.Ф. Наумов
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 Н.Ф. Наумов filed Critical Н.Ф. Наумов
Priority to SU1750530/23A priority Critical patent/SU430614A1/en
Application granted granted Critical
Publication of SU430614A1 publication Critical patent/SU430614A1/en

Links

Landscapes

  • Air Conditioning Control Device (AREA)

Abstract

Система кондиционирования воздуха на летательном аппарате, содержащая установленные на магистрали подачи воздуха в кабину теплообменники предварительного охлаждения и турбохолодильник, загрузочный вентилятор которого включен в оборудованный воздуховоздушным радиатором циркуляционый контур, соединенный с атмосферой при помощи снабженного приводом переключателя, и установленный в кабине датчик температуры, отличающаяся тем, что, с целью упрощения системы и повышения надежности ее работы, радиатор циркуляционного контура установлен на магистрали подачи воздуха в кабину, а привод переключателя соединен с датчиком температуры.Air conditioning system on an aircraft containing pre-cooling heat exchangers and a turbo-cooler installed on the cabin air supply line; that, in order to simplify the system and increase the reliability of its operation, the radiator of the circulation circuit has n on the air line to the cabin, and the actuator switch is connected to the temperature sensor.

SU1750530/23A 1972-02-21 1972-02-21 AIR CONDITIONING SYSTEM ON AIRCRAFT SU430614A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1750530/23A SU430614A1 (en) 1972-02-21 1972-02-21 AIR CONDITIONING SYSTEM ON AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1750530/23A SU430614A1 (en) 1972-02-21 1972-02-21 AIR CONDITIONING SYSTEM ON AIRCRAFT

Publications (1)

Publication Number Publication Date
SU430614A1 true SU430614A1 (en) 2005-05-10

Family

ID=60521997

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1750530/23A SU430614A1 (en) 1972-02-21 1972-02-21 AIR CONDITIONING SYSTEM ON AIRCRAFT

Country Status (1)

Country Link
SU (1) SU430614A1 (en)

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