Heat exchanger especially for spacecraft
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United States of America Patent
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Oct 4, 1994
Grant Date -
N/A
app pub date -
Oct 30, 1992
filing date -
Nov 2, 1991
priority date (Note) -
Expired
status (Latency Note)
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Abstract
A heat exchanger for a spacecraft utilizes a droplet radiator, whereby the droplet collector has the shape of a rotation symmetrical ring body that is rotatable about a central rotational axis. Preferably, the rotation symmetric ring body has the shape of a wheel, whereby the droplet generator is arranged near the rotational axis of symmetry and the collector forms a wheel rim. The return flow of the coolant takes place either through the spokes of the wheel which connect the droplet collector wheel rim to the hub or through a separate suction conduit. A secondary coolant flow circuit may be integrated into the droplet collector.
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