Method and device for regulating the cooling of oil in a turbomachine
AssigneeSafran Aircraft Engines
InventorsSebastien Gameiro, Brice Andre, Guillaume Mathon Margueritte, Nicolas Potel
Life of this patent
Estimating the term…
Loading patent…
AssigneeSafran Aircraft Engines
InventorsSebastien Gameiro, Brice Andre, Guillaume Mathon Margueritte, Nicolas Potel
Estimating the term…
A method for regulating oil cooling within an oil cooling device of a turbomachine including a first heat exchanger mounted in series with a second heat exchanger, the first heat exchanger being an oil/air exchanger while the second heat exchanger is an oil/fuel exchanger, each heat exchanger having an oil inlet and an oil outlet, a bypass directly connecting the oil inlet of the first heat exchanger to the oil outlet of the first heat exchanger, and a flow regulator to regulate the flow rate of oil flowing through the bypass. Circulation of oil though the bypass is allowed by means of the flow regulator when the oil temperature is less than or equal to a predetermined temperature comprised between 70° C. and 90° C., preferably equal to about 80° C.
A method for regulating oil cooling within an oil cooling device of a turbomachine including a first heat exchanger mounted in series with a second heat exchanger, the first heat exchanger being an oil/air exchanger and the second heat exchanger being an oil/fuel exchanger, each heat exchanger having an oil inlet and an oil outlet, a bypass directly connecting the oil inlet of the first heat exchanger to the oil outlet of the first heat exchanger, and a flow regulator to regulate a flow rate of oil flowing through the bypass, the flow regulator including a thermal valve and a pressure valve arranged in parallel, the method comprising:
An oil cooling device for a turbomachine comprising:
Dependencies are inferred from the claim text.