Means for calculating turbine inlet temperature of a gas turbine

Details Means for calculating turbine inlet temperature of a gas turbine Means for calculating turbine inlet temperature of a gas turbine

1976-09-15

1977-11-01

Queisser, Richard C.

Measuring and testing

Vehicle chassis

Steering

73346, G01M 1500

Patent

active

040559971

ABSTRACT:
Turbine inlet temperature of a gas turbine engine is calculated from compressor discharge temperature, total and static pressures and total fuel metered to the engine by combining a sensed engine temperature with a derived fuel/air ratio and from the empirical burner can temperature rise equation solving for the turbine inlet temperature value.

REFERENCES:
patent: 2809492 (1957-10-01), Arkawy
patent: 3377848 (1968-04-01), Marvin
patent: 3789665 (1974-02-01), Hohenberg

Affiliated with

Also associated with

Rating

Means for calculating turbine inlet temperature of a gas turbine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Means for calculating turbine inlet temperature of a gas turbine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Means for calculating turbine inlet temperature of a gas turbine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1931