3731070 is referenced by 36 patents and cites 2 patents.

The relative health of a gas turbine engine is analyzed and the particular faults are automatically determined by sensing monitored parameters of the gas path of gas turbine engine and electronically computing them into thermodynamically independent variables and comparing the rate of change of this value with a base line value used as a reference datum. A special purpose computer is programmed to include a general influence coefficient matrix containing the independent variables selected to determine the specific fault and serves to thermodynamically simulate the engine's operations.

Gas turbine engine analyzer
Application Number
Publication Number
Application Date
April 27, 1971
Publication Date
May 1, 1973
Urban Louis A
United Aircraft Corporation
G06f 15/32
G06f 15/20
G07C 03/00
F01D 21/00
View Original Source