Fluid temperature control installation for rotorcraft, associating a system for cooling a power plant with a system for heating a cabin
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United States of America Patent
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Oct 18, 2016
Grant Date -
Dec 26, 2013
app pub date -
Jan 15, 2013
filing date -
Jan 24, 2012
priority date (Note) -
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Abstract
A fluid temperature control installation for a rotorcraft, the installation comprising a system for cooling a main transmission (3) and a system for temperature control of the ambient air (32) of a cabin (16). A heat exchanger (8) is fitted with a bladeless ventilator (9). A source air stream (11) generated by an accessory compressor (5) driven by the main transmission (3) passes through the heat exchanger (8) where it takes heat. The source air stream (11) is distributed selectively to the bladeless ventilator (9) to generate a cooling air stream (13) passing through the heat exchanger (8), and/or is distributed to the cabin (16) after passing through the heat exchanger (8) in order to heat the ambient air (32) of the cabin.
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