SU297314A1 - Test complex for the air conditioning system of the aircraft airtight cabins - Google Patents
Test complex for the air conditioning system of the aircraft airtight cabinsInfo
- Publication number
- SU297314A1 SU297314A1 SU1339808/23A SU1339808A SU297314A1 SU 297314 A1 SU297314 A1 SU 297314A1 SU 1339808/23 A SU1339808/23 A SU 1339808/23A SU 1339808 A SU1339808 A SU 1339808A SU 297314 A1 SU297314 A1 SU 297314A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- air
- fuel
- radiators
- air conditioning
- conditioning system
- Prior art date
Links
Landscapes
- Testing Of Engines (AREA)
Abstract
1. Испытательный комплекс для систем кондиционирования воздуха гермокабин самолетов, содержащий барокамеру с системами имитации окружающей температуры и давления, имитации отбора воздуха от двигателя, подготовки и подачи хладагента для испарения и с измерительной аппаратурой, отличающийся тем, что, с целью имитации скоростного напора воздуха от воздухозаборника самолета, он оборудован подогревателем и турбохолодильником, установленными на трубопроводах, подключенных к воздухо-воздушным радиаторам испытуемой системы и снабженных дроссельными задвижками, обеспечивающими поочередную работу подогревателя и турбохолодильника.2. Комплекс по п.1, отличающийся тем, что, с целью имитации подачи топлива к двигателям, в нем установлены топливные баки с насосами, подающими топливо в топливо-воздушные радиаторы испытуемой системы, и радиаторы для охлаждения топлива, установленные в сливных трубопроводах, сообщающих топливо-воздушные радиаторы с топливным баком.1. A test complex for air conditioning systems of an air-tight chamber of airplanes, containing a pressure chamber with systems for simulating ambient temperature and pressure, simulating air bleeding from the engine, preparing and supplying refrigerant for evaporation, and with instrumentation equipment, characterized in that the air intake of the aircraft, it is equipped with a heater and a turbo-cooler installed on pipelines connected to the air-to-air radiators of the system under test and equipped with others sselnymi valves that provide alternate operation of the heater and turboholodilnika.2. A complex according to claim 1, characterized in that, in order to imitate the supply of fuel to the engines, it has fuel tanks with pumps that supply fuel to the air-to-air radiators of the system under test, and radiators for cooling the fuel installed in the drain pipes that tell -air radiators with fuel tank.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1339808/23A SU297314A1 (en) | 1969-05-26 | 1969-05-26 | Test complex for the air conditioning system of the aircraft airtight cabins |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1339808/23A SU297314A1 (en) | 1969-05-26 | 1969-05-26 | Test complex for the air conditioning system of the aircraft airtight cabins |
Publications (1)
Publication Number | Publication Date |
---|---|
SU297314A1 true SU297314A1 (en) | 2006-02-27 |
Family
ID=60514405
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1339808/23A SU297314A1 (en) | 1969-05-26 | 1969-05-26 | Test complex for the air conditioning system of the aircraft airtight cabins |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU297314A1 (en) |
-
1969
- 1969-05-26 SU SU1339808/23A patent/SU297314A1/en active
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