SU1269415A1 - AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINE - Google Patents
AIR CONDITIONING SYSTEM OF AIRCRAFT HERMOCABINEInfo
- 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
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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8272930B2 (en) | 2005-01-26 | 2012-09-25 | Airbus Operations Gmbh | Air system |
-
1985
- 1985-03-11 SU SU3865302/23A patent/SU1269415A1/en active
Cited By (1)
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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