Gas turbine rotor assembly methods

Details Gas turbine rotor assembly methods Gas turbine rotor assembly methods

F - Mech Eng,Light,Heat,Weapons

01

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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 2639080

Method of assembling a rotor assembly of a gas turbine engine having a plurality of components. The method comprises in one aspect calculating the bending forces due to the mass distribution along the rotor. In another aspect, an optimization routine iterates different rotor arrangements, comparing the calculated bending moments to determine a set of component positions that minimizes the bending forces. In another aspect, mass corrections are optimized to balance the rotor assembly.

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