Title:
REDUNDANT AIRCRAFT COOLING SYSTEM FOR REDUNDANT AIRCRAFT COMPONENTS
Document Type and Number:
WIPO Patent Application WO2008071319
Kind Code:
B1
Abstract:
An aircraft cooling system (1) according to the invention comprises a first coolant stream (4a) which cools at least one first heat load (2a), and a second coolant stream (4b) which cools at least one second heat load (2b), wherein the aircraft cooling system (1) is formed such that the first heat load (2a) and the second heat load (2b) are thermally coupled together. The first heat load (2a) and the second heat load (2b) are formed by two mutually redundant- aircraft components. A third coolant stream (12) can thermally couple the first heat load (2a) and the second heat load (2b) together. The third coolant stream (12) can be cooled by a heat sink (16).
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Inventors:
CASAS NORIEGA WILSON WILLY (DE)
EBIGT WOLFGANG (DE)
FREY ANDREAS (DE)
EBIGT WOLFGANG (DE)
FREY ANDREAS (DE)
Application Number:
PCT/EP2007/010473
Publication Date:
August 07, 2008
Filing Date:
December 03, 2007
Export Citation:
Assignee:
AIRBUS GMBH (DE)
CASAS NORIEGA WILSON WILLY (DE)
EBIGT WOLFGANG (DE)
FREY ANDREAS (DE)
CASAS NORIEGA WILSON WILLY (DE)
EBIGT WOLFGANG (DE)
FREY ANDREAS (DE)
International Classes:
B64D13/06; F25B25/00; F25D17/02
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