High performance redundant liquid cooling for power modules
AssigneeLockheed Martin Corporation
InventorEmre Gurpinar
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AssigneeLockheed Martin Corporation
InventorEmre Gurpinar
Estimating the term…
A power converter system for use in an aircraft includes a plurality of power converter module assemblies and a cooling system. Each power converter module assembly of the plurality of power converter module assemblies includes a semiconductor package, a first flow manifold, and a second flow manifold. The semiconductor package defines a heat transfer surface. The first flow manifold and the second flow manifold are thermally coupled to the heat transfer surface. The cooling system includes a first flow circuit and a second flow circuit. The first flow circuit is fluidly coupled in series flow arrangement to the first flow manifold of each of the plurality of power converter module assemblies. The second flow circuit is fluidly coupled to the second flow manifold of each of the plurality of power converter module assemblies.
A power converter system comprising:
A power converter system comprising:
A method comprising:
Dependencies are inferred from the claim text.