Turbomachine comprising a heat exchanger between a fuel circuit and two lubricant circuits
AssigneeSafran Aircraft Engines
InventorsAnthony Julien Badalamenti, Mohammed-Lamine Boutaleb, Sébastien Oriol
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AssigneeSafran Aircraft Engines
InventorsAnthony Julien Badalamenti, Mohammed-Lamine Boutaleb, Sébastien Oriol
Estimating the term…
A turbomachine includes a heat exchanger, a first circuit of a first fluid, the first circuit including two ducts in the heat exchanger, a second circuit of a second fluid, and a third circuit of a third fluid. The second circuit includes a first channel in the heat exchanger and the third circuit includes a second channel in the heat exchanger, each of the first channel and the second channel are contiguous to one of the two ducts so as to be in thermal contact with one of the two ducts, the first channel and the second channel are contiguous to each other so as to be in thermal contact with each other, and the heat exchanger includes a section in which the two ducts, the first channel and the second channel are locally parallel to each other.
A turbomachine comprising:
A heat exchange method in a turbomachine, the heat exchange method comprising:
Dependencies are inferred from the claim text.