Method and apparatus for geometric rotor stacking and balancing

Data processing: measuring – calibrating – or testing – Measurement system – Orientation or position

Reexamination Certificate

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C702S147000

Reexamination Certificate

active

07877223

ABSTRACT:
A computer method or corresponding system for optimally balancing a rotor assembly. The computer system defines a theoretical centerline based on a mathematical model of the rotor assembly. For each disc or component of the rotor assembly, the invention system calculates rotor blade or bolt and washer distribution, based on calculated centerline deviations and angular locations of the discs and effective weights of rotor blade or bolt-and-washer sets. The rotor blade or bolt-and-washer distribution provides locations for placement of the rotor blades or bolts-and-washers so as to offset the centerline deviations and thus correct imbalance of the rotor assembly.

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Axiam Incorporated Product Brochure of GMX 4000 Smart Stack™ Systems, “For Assembly of Aircraft Jet Engines and Industrial Gas Turbines” (1991 —publication month not available).
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International Search Report for International Application No. PCT/US2007/001448, date mailed Oct. 2, 2007.
International Preliminary Report on Patentability, PCT/US2007/001448, date of mailing Apr. 9, 2009.

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