Aircraft turbomachine comprising a heat exchanger of the precooler type
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United States of America Patent
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Jul 13, 2021
Grant Date -
Jan 5, 2017
app pub date -
Dec 15, 2014
filing date -
Dec 19, 2013
priority date (Note) -
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Abstract
An aircraft turbomachine including a nacelle and an engine further including at least one outflowing jet of air, wherein a heat exchanger of the precooler type for supplying air to the aircraft is mounted in the nacelle. The exchanger includes a primary circuit, the inlet of which is connected to a supply of compressed air from the engine and the outlet of which is connected to an air supply for supplying air to the aircraft, and a secondary circuit supplied with air taken from said air flow.
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