CPC F02C 7/12 (2013.01) [F02C 7/04 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2260/221 (2013.01)] | 20 Claims |
1. A heat exchanger system for a propulsion system inlet duct comprising:
an inlet duct assembly, wherein the inlet duct assembly includes a maximum cross-sectional area defined in a plane taken transverse to a longitudinal length of the inlet duct; and
a heat exchanger assembly disposed in the inlet duct assembly, the heat exchanger assembly having a front facing cross-sectional area that is transverse to the longitudinal length of the inlet duct and that is greater than the maximum cross-sectional area of the inlet duct.
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