SU1269415A1 - AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE - Google Patents

AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE

Info

Publication number
SU1269415A1
SU1269415A1 SU3865302/23A SU3865302A SU1269415A1 SU 1269415 A1 SU1269415 A1 SU 1269415A1 SU 3865302/23 A SU3865302/23 A SU 3865302/23A SU 3865302 A SU3865302 A SU 3865302A SU 1269415 A1 SU1269415 A1 SU 1269415A1
Authority
SU
USSR - Soviet Union
Prior art keywords
fan
turbine
recirculation channel
aircraft
air conditioning
Prior art date
Application number
SU3865302/23A
Other languages
Russian (ru)
Inventor
Е.И. Васькович
Ю.П. Лачаев
Original Assignee
Е.И. Васькович
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.И. Васькович filed Critical Е.И. Васькович
Priority to SU3865302/23A priority Critical patent/SU1269415A1/en
Application granted granted Critical
Publication of SU1269415A1 publication Critical patent/SU1269415A1/en

Links

Abstract

Система кондиционирования воздуха гермокабины летательного аппарата, содержащая источник сжатого воздуха, теплообменники, турбохолодильную установку с турбиной и вентилятором, и рециркуляционный канал, замкнутый через гермокабину, в котором установлены вентилятор, фильтр и теплообменник, отличающаяся тем, что, с целью повышения экономичности и уменьшения массы системы, вентилятор рециркуляционного канала установлен на одном валу с турбиной и вентилятором турбохолодильной установки, при этом вход турбины дополнительно соединен через рециркуляционный канал с гермокабиной, выход турбины дополнительно соединен с входом холодной полости теплообменника рециркуляционного канала, а выход холодной полости теплообменника соединен с атмосферой.Air conditioning system of the aircraft pressurized cabin containing a source of compressed air, heat exchangers, a turbo-refrigeration unit with a turbine and a fan, and a recirculation channel closed through the pressurized cabin in which a fan, filter and heat exchanger are installed, characterized in system, the fan of the recirculation channel is mounted on the same shaft with the turbine and the fan of the turbo-refrigerating installation, and the turbine inlet is additionally connected through A recirculation channel with a pressurized cabin, the turbine outlet is additionally connected to the cold cavity inlet of the heat exchanger of the recirculation channel, and the cold cavity outlet of the heat exchanger is connected to the atmosphere.

SU3865302/23A 1985-03-11 1985-03-11 AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE SU1269415A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3865302/23A SU1269415A1 (en) 1985-03-11 1985-03-11 AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3865302/23A SU1269415A1 (en) 1985-03-11 1985-03-11 AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE

Publications (1)

Publication Number Publication Date
SU1269415A1 true SU1269415A1 (en) 2004-12-20

Family

ID=60519135

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3865302/23A SU1269415A1 (en) 1985-03-11 1985-03-11 AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE

Country Status (1)

Country Link
SU (1) SU1269415A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8272930B2 (en) 2005-01-26 2012-09-25 Airbus Operations Gmbh Air system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8272930B2 (en) 2005-01-26 2012-09-25 Airbus Operations Gmbh Air system

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