Heat exchanger differential oil temperature determination
AssigneePratt & Whitney Canada Corp.
InventorsKashif Mohammed, Robin Watt
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorsKashif Mohammed, Robin Watt
Estimating the term…
A gas turbine engine includes a compressor section and a turbine section. A heat exchanger is operable to cool a fluid utilized by a component of the gas turbine engine. The heat exchanger has an inlet and an outlet for the accessory fluid. A strain gauge is associated with the fluid inlet and operable to produce a signal indicative of a temperature of the fluid at the fluid inlet and a strain gauge is associated with the fluid outlet and operable to produce a signal indicative of a temperature of the fluid at the fluid outlet. A controller determines a temperature differential across the heat exchanger by utilizing the signal from the strain gauge at the fluid inlet and the signal from the strain gauge at the fluid outlet. A method and a heat exchanger are also disclosed.
A gas turbine engine comprising:
(canceled)
A method of operating a gas turbine engine comprising:
(canceled)
The method as set forth in claim 129, wherein the diagnostic purpose is determining if the temperature differential is trending in a manner indicating a need for maintenance.
The method as set forth in claim 129, wherein if the strain of the heat exchanger at the fluid outlet indicates a higher temperature than the strain of the heat exchanger at the fluid inlet, the diagnostic purpose is a determining that there may be a fire associated with the gas turbine engine.
The method as set forth in claim 129, wherein the diagnosis purpose is to determine an actual oil temperature.
A heat exchanger comprising:
18-19. (canceled)
Dependencies are inferred from the claim text.