FIELD: transport.
SUBSTANCE: set of inventions relates to aircraft cooling systems with redundancy. In compliance with this invention, aircraft cooling system includes first heat carrier flow 4a to cool, at least, one first heat load 2a and second heat carrier flow 2b to cool, at least, one second heat load 2b. Said system 1 is configured to allow thermal communication between said first and second loads, 2a, 2b. Said loads may be made up of two mutually redundant components of aircraft. Third heat carrier flow 12 allow thermal communication between said first and second loads. Said third flow may be cooled down by heat absorber 16.
EFFECT: expanded serviceability.
11 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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|
RU2524058C2 |
