Method of maintaining aircraft gas turbine engine

Details Method of maintaining aircraft gas turbine engine Method of maintaining aircraft gas turbine engine

G - Physics

01

M

G01M 15/00 (2006.01) B64F 5/00 (2006.01) F01D 21/00 (2006.01) G01M 15/14 (2006.01) G06Q 90/00 (2006.01)

Patent

CA 2572444

A method for maintaining a civil-certified aircraft engine rotating part subject to fatigue failure during service use, the method comprising the steps of providing an assembly including the rotating part and at least one other component mounted to the rotating part; determining a maximum safe operating life for the assembly; and specifying a life limit for the assembly based on the maximum safe operating life, the life limit being the maximum number of cycles the assembly may be used before replacement.

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