SU547084A1 - Air conditioning system on the plane - Google Patents
Air conditioning system on the planeInfo
- Publication number
- SU547084A1 SU547084A1 SU2175067/23A SU2175067A SU547084A1 SU 547084 A1 SU547084 A1 SU 547084A1 SU 2175067/23 A SU2175067/23 A SU 2175067/23A SU 2175067 A SU2175067 A SU 2175067A SU 547084 A1 SU547084 A1 SU 547084A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- line
- air
- purge
- cooling
- conditioning system
- Prior art date
Links
Landscapes
- Central Air Conditioning (AREA)
Abstract
Система кондиционирования воздуха на самолете, содержащая первичный радиатор с линией продувки на встречном потоке и регенератор, установленный на линии сброса охлаждающего воздуха из расположенного за ним теплообменника вентиляции снаряжения и кабины, а также турбохолодильник с обводной линией и исполнительные органы регулятора температуры охлаждаемого воздуха, установленные в линиях продувки и подачи охлаждающего и горячего воздуха, отличающаяся тем, что, с целью повышения экономичности, участок линии охлаждающего воздуха после теплообменника вентиляции снаряжения и места сброса воздуха из кабины выполнен с сужением, формирующим камеру смешения эжектора, сопло которого соединено с входом линии продувки первичного радиатора при помощи трубопровода, оборудованного заслонкой регулятора температуры охлаждаемого воздуха.The air conditioning system on the aircraft, containing a primary radiator with a purge line on the counter-flow and a regenerator installed on the cooling air discharge line from the equipment and cabin ventilation heat exchanger behind it, as well as a turbo-refrigerator with a bypass line and the cooling air regulator control units installed in cooling and hot air purge and supply lines, characterized in that, in order to improve efficiency, the section of the cooling air line after The heat exchanger of the equipment ventilation and the place of air discharge from the cabin is made with a constriction that forms the mixing chamber of the ejector, the nozzle of which is connected to the inlet of the purge line of the primary radiator by means of a pipeline equipped with a gate of the cooled air temperature controller.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2175067/23A SU547084A1 (en) | 1975-09-25 | 1975-09-25 | Air conditioning system on the plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2175067/23A SU547084A1 (en) | 1975-09-25 | 1975-09-25 | Air conditioning system on the plane |
Publications (1)
Publication Number | Publication Date |
---|---|
SU547084A1 true SU547084A1 (en) | 2006-01-27 |
Family
ID=60520675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2175067/23A SU547084A1 (en) | 1975-09-25 | 1975-09-25 | Air conditioning system on the plane |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU547084A1 (en) |
-
1975
- 1975-09-25 SU SU2175067/23A patent/SU547084A1/en active
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