Method for assembling gas turbine engine components

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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C416S09700R, C029S889200

Reexamination Certificate

active

07021892

ABSTRACT:
Method for assembling into turbine sets turbine components having internal cooling passages. The turbine components are classified according to flow capability through the internal cooling passages and turbine sets are assembled in which the turbine components have the same flow capability classification.

REFERENCES:
patent: 5536143 (1996-07-01), Jacala et al.
patent: 6247896 (2001-06-01), Auxier et al.
patent: 6408610 (2002-06-01), Caldwell et al.

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