Gas turbine rotor assembly method

Details Gas turbine rotor assembly method Gas turbine rotor assembly method

F - Mech Eng,Light,Heat,Weapons

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F01D 5/02 (2006.01) F01D 5/10 (2006.01) F16F 15/20 (2006.01) F16F 15/22 (2006.01)

Patent

CA 2639086

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.

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