Inlet total temperature synthesis for gas turbine engines

Details Inlet total temperature synthesis for gas turbine engines Inlet total temperature synthesis for gas turbine engines

1986-12-08

1988-06-07

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

60 392, 60 39281, F02C 900

Patent

active

047488042

ABSTRACT:
In a gas turbine engine electronic control system the engine total inlet temperature is synthesized from aircraft Mach number and the nozzle expansion ratio. When the engine is in a transient mode of operation the synthesized value of the total inlet temperature is maintained constant at the value calculated just before entering the transient mode. The synthesized temperature is used when the actual measured temperature is unavailable or unreliable.

REFERENCES:
patent: 2809492 (1957-10-01), Arkawy
patent: 3420056 (1969-01-01), Eames
patent: 4058975 (1977-11-01), Gilbert et al.
patent: 4122667 (1978-10-01), Hosaka et al.
patent: 4212161 (1980-07-01), Newirth et al.
patent: 4228650 (1980-10-01), Camp
patent: 4543782 (1985-10-01), Fitzmaurice
patent: 4581888 (1986-04-01), Schmitzer et al.
patent: 4594849 (1986-06-01), Kenison et al.
patent: 4651518 (1987-03-01), McLaughlin et al.

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