Stable pumped two-phase cooling
AssigneeHamilton Sundstrand Corporation
InventorsJoseph E. Turney, Raphael Mandel, Ram Ranjan
Life of this patent
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AssigneeHamilton Sundstrand Corporation
InventorsJoseph E. Turney, Raphael Mandel, Ram Ranjan
Estimating the term…
Cooling systems include a cold sink having a number of heat load cooling paths and a heat load associated with each cooling path. An inlet is configured to supply a cooling fluid into the cold sink and an outlet is configured to receive the cooling fluid after passing through the plurality of heat load cooling paths of the cold sink. A pressure regulating element is arranged along each cooling path, each pressure regulating element arranged between the inlet and the heat load along each cooling path and configured to cause a pressure drop in the cooling fluid prior to passing the cooling fluid to each heat load. The pressure drop caused by each pressure regulating element is the same and is a pressure drop greater than a maximum pressure drop across each heat load of a system without such pressure regulating elements.
A cooling system comprising:
An aircraft cooling system comprising:
A cooling system comprising:
Dependencies are inferred from the claim text.