Pratt-Whitney Canada Corp

Harry Harris

Jiemin Wang

Ronald Robinson

Richard Benoit

Bruce Calvert

Cameron Todd Walters

Alphonse Bellemare

Jieming Wang

Cameron T Walters

Richar Benoit

Ronald Leslie Robinson

Methods of assembling a rotor assembly of a gas turbine engine having a plurality of components. The method comprises, in one aspect, determining a static unbalance force of each component using the mass and the center of mass location, and determining an optimum assembly arrangement minimizing static unbalance forces. Optimal component stacking positions, among other things, may then be established.

Gas turbine rotor assembly balancing method

Gas turbine rotor assembly method

A method of balancing an assembly of rotary parts of a gas turbine engine comprising measuring at least one of the concentricity and parallelism of each component and considering globally all possible component stacking positions to generate an optimized stacking position for each component of the assembly to minimize assembly unbalance.

Method of balancing a gas turbine engine rotor

Growing community of inventors

Georgetown, Canada

Harry Harris