B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 31/00 (2006.01) F02C 9/00 (2006.01) F02C 9/18 (2006.01)
Patent
CA 2584438
A controller (24) for operating a gas turbine engine (10), wherein the gas turbine engine is installed in an aircraft, wherein the gas turbine engine includes a compressor (14), a turbine (16), and a shaft (18) connecting the turbine to the compressor. The controller includes a program which instructs the controller to run a computer dynamic model of the gas turbine engine, wherein the computer dynamic model has inputs including engine operating conditions and installation platform operating conditions. The controller also is programmed to calculate a dynamic limit on mechanical power extraction from the shaft based at least on the running of the computer dynamic model of the gas turbine engine. A method for operating a gas turbine engine (10) installed in an aircraft includes running a computer dynamic model of the engine and calculating a dynamic limit on mechanical power extraction from a shaft (18) of the engine based at least on the running of the model.
Carlson William
Sheldon Karl Edward
Turco John Biagio
Wiegman Herman Lucas Norbert
Company General Electric
Craig Wilson And Company
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