Cooling system for the cooling of heat-producing devices in an aircraft

A cooling system and equipment technology, applied in lighting and heating equipment, aircraft kitchens, aircraft parts, etc., can solve the problem of inflexible space distribution, and achieve the effect of flexible layout, reliable cooling system, and increased reliability
CN1902087AInactive Publication Date: 2007-01-24AIRBUS OPERATIONS GMBH
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
AIRBUS OPERATIONS GMBH
Publication Date
2007-01-24
Estimated Expiration
Not applicable · inactive patent

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Abstract

A cooling system (10) for the cooling of heat producing devices (44, 46, 48) in an aircraft is designed with a central cold producing device (12), at least one cold consumer (44, 46, 48) and a cold conveyance system (14) which connects the cold producing device (12) and the cold consumer (44, 46, 48). With this cooling system, the cold conveyance system (14) has at least one cooling circuit which supplies a cooled cold carrier medium from the cold producing device (12) to at least one cold consumer (44, 46, 48) and brings this back to the cold producing device (12), so that at least one cold consumer (44, 46, 48) is supplied with the cold produced in the cold producing device (12) by means of the cold carrier medium circulating in the cooling circuit.
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Description

technical field

[0001] The invention relates to a cooling system for cooling heat-generating devices in an aircraft. Background technique

[0002] Inside the aircraft, in addition to the aircraft's air conditioning system, there are various technical devices that generate heat and must be cooled in order to work safely. For this reason, different cooling systems have been provided in aircraft for a long time in order to provide the respective relevant solutions for the corresponding technical equipment to be cooled. Providing an independent system of this type requires a relatively large installation space in the aircraft and requires little flexibility. Furthermore, self-contained systems of this type often use the ambient air directly as a heat sink to remove the heat that is removed from the technical equipment to be cooled. However, this leads to disadvantageous heating of the interior of the aircraft.

[0003] It is current practice, for example according to DE 38 12...

Claims

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