TURBOJET ENGINE FOR AIRCRAFT
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United States of America Patent
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N/A
Issued Date -
Dec 2, 2010
app pub date -
Jun 18, 2008
filing date -
Jun 25, 2007
priority date (Note) -
Abandoned
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Abstract
A turbojet engine for an aircraft that includes an engine provided in a nacelle and at least one heat exchanger for cooling down a hot fluid collected in the propulsion system of the turbojet engine before re-injecting the aforementioned partially-cooled hot flow into the aforementioned propulsion system, wherein at least one heat exchanger is a radial heat exchanger extending in the lower portion of the turbojet engine at a lower branching of the turbojet engine.
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