Cooling system for rotorcraft laser system
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United States of America Patent
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Aug 20, 2019
Grant Date -
Sep 13, 2018
app pub date -
Dec 10, 2015
filing date -
Jan 21, 2015
priority date (Note) -
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Abstract
A cooling system for a rotorcraft laser system is provided. The cooling system includes at least one laser carrying component operatively coupling a laser turret and a laser generating assembly. The cooling system also includes at least one fuel line fluidly coupled to a fuel tank containing a fuel. The cooling system further includes a heat exchanger containing a portion of the laser carrying component and the fuel line to transfer heat therebetween to cool the laser carrying component.
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