Methods and apparatus for assembling turbine engines

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received in well or slot

Reexamination Certificate

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Reexamination Certificate

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06893224

ABSTRACT:
A method of assembling a turbine comprises coupling at least one bucket assembly. The bucket assembly including an upstream side, a downstream side, a blade extending therebetween and a dovetail extending radially inwardly from the blade to a rotor. The method further comprises fixedly securing the at least one bucket assembly to the rotor with a shear pin that extends from the bucket assembly upstream side to the bucket assembly downstream side.

REFERENCES:
patent: 2220918 (1940-11-01), Smith
patent: 2445154 (1948-07-01), Reed
patent: 2800298 (1957-07-01), Schellens
patent: 2805838 (1957-09-01), Pickup
patent: 4676723 (1987-06-01), Kiger et al.
patent: 4702673 (1987-10-01), Hansen et al.
patent: 4711007 (1987-12-01), Conrad
patent: 4767247 (1988-08-01), Partington et al.
patent: 4767273 (1988-08-01), Partington
patent: 4767275 (1988-08-01), Brown
patent: 4915587 (1990-04-01), Pisz et al.
patent: 5720596 (1998-02-01), Pepperman
patent: 6030178 (2000-02-01), Caruso
patent: 6168377 (2001-01-01), Wolfe et al.
patent: 6287079 (2001-09-01), Gosling et al.
patent: 6416286 (2002-07-01), Roberts et al.
patent: 6438837 (2002-08-01), Berry et al.
patent: 6439844 (2002-08-01), Turnquist et al.

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