Title:
COOLING SYSTEM AND METHOD FOR EXPELLING HEAT FROM A HEAT SOURCE LOCATED IN THE INTERIOR OF AN AIRCRAFT
Document Type and Number:
WIPO Patent Application WO2005063566
Kind Code:
A3
Abstract:
With a cooling system for expelling heat from a heat source (30) located in the interior of an aircraft to a heat reducer (32), with a piping system (10) sealed against the surrounding atmosphere which is thermally coupled to a heat intake section (14) with the heat source (38) and to a heat output section (22) with the heat reducer (32), and which preferably has an essentially adiabate transport section (21), it is proposed that the piping system (10) is filled with a heat conveyance medium (12) which, when taking in heat from the heat source (38) in the heat intake section (14) undergoes a transition from the liquid phase to the gaseous phase, then flows into the heat output section (22), and here, when discharging heat to the heat reducer (32) condenses once again, and flows back into the heat intake section (14).
Inventors:
MUEHLTHALER GEORG (DE)
MARKWART MICHAEL (DE)
EDOM ANDREAS (DE)
MARKWART MICHAEL (DE)
EDOM ANDREAS (DE)
Application Number:
PCT/EP2004/014860
Publication Date:
September 22, 2005
Filing Date:
December 30, 2004
Export Citation:
Assignee:
AIRBUS GMBH (DE)
MUEHLTHALER GEORG (DE)
MARKWART MICHAEL (DE)
EDOM ANDREAS (DE)
MUEHLTHALER GEORG (DE)
MARKWART MICHAEL (DE)
EDOM ANDREAS (DE)
International Classes:
B64D11/04; B64D13/08; F28D15/02; (IPC1-7): F28D15/02; B64D13/08; B64D11/04
Foreign References:
| US2499736A | 1950-03-07 | |||
| US5966951A | 1999-10-19 | |||
| GB1526160A | 1978-09-27 | |||
| GB1595961A | 1981-08-19 | |||
| US20030159808A1 | 2003-08-28 | |||
| US6220338B1 | 2001-04-24 | |||
| US5267608A | 1993-12-07 |
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