FIELD: air transport.
SUBSTANCE: air cooling device contains the first area of air intake, the first line and the second line. The first area of air intake is purposed for intake of the first flow of cooling air from the first air conditioning unit; it is located in incoming air channel of the first air conditioning unit. The first line is purposed for delivery of cooling air flow to air cooling device. The second line is purposed for direction of delivered air after its cooling to inert gas generation system. The method of air cooling at aircraft includes intake of the first flow of cooling air from the first air conditioning unit in the first area of air intake located in incoming air channel of the first air conditioning unit; further cooling of delivered air by the first flow of cooling air and its delivery after cooling to inert gas generation system.
EFFECT: weight reduction of air cooling device.
13 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE AND METHOD OF AIR FEED FOR INERT GAS GENERATION AND THEIR APPLICATION AT AIRCRAFT | 2005 |
|
RU2392196C2 |
| SYSTEM PRODUCING PROCESS AIR AND ITS APPLICATION | 2005 |
|
RU2372253C2 |
| SYSTEM FOR PRESSURE INCREASING AND AIR CONDITIONING | 2006 |
|
RU2398712C2 |
| TURBO-COMPRESSOR SYSTEM AND METHOD FOR EXTRACTING ENERGY FROM AIRCRAFT ENGINE | 2014 |
|
RU2678234C2 |
| COOLING SYSTEM, AIR CONDITIONING UNIT AND AIR CONDITIONING METHOD | 2019 |
|
RU2711842C1 |
| AIR CONDITIONING SYSTEM OF HERMETIC ZONE OF FLYING APPARATUS | 2016 |
|
RU2637080C1 |
| ENERGY-INTENSIVE AIR CONDITIONING SYSTEM FOR AIRCRAFTS | 2023 |
|
RU2807448C1 |
| AIRCRAFT AIR-CONDITIONING SYSTEM | 1997 |
|
RU2170192C2 |
| METHOD OF CONTROLLING AIRCRAFT CABIN AIR TEMPERATURE AND DEVICE TO THIS END | 2009 |
|
RU2401775C1 |
| AIR CONDITIONING SYSTEM OF PASSENGER COMPARTMENT OF AIRCRAFT | 2012 |
|
RU2595210C2 |
