Methods and apparatus for assembling gas turbine engines

Details Methods and apparatus for assembling gas turbine engines Methods and apparatus for assembling gas turbine engines

2005-10-04

2005-10-04

Gartenberg, Ehud (Department: 3746)

Power plants

Combustion products used as motive fluid

Having mounting or supporting structure

C029S889220

Reexamination Certificate

active

06951112

ABSTRACT:
A method for assembling a gas turbine engine includes coupling an outer structure within the gas turbine engine, wherein the outer structure includes a socket extending from a radially inner surface of the outer structure, and coupling an inner structure to the outer structure by inserting a radial pin through the inner structure and into the socket such that the inner structure is aligned axially, circumferentially, and with respect to an engine centerline axis extending through the gas turbine engine.

REFERENCES:
patent: 4614082 (1986-09-01), Sterman et al.
patent: 5211541 (1993-05-01), Fledderjohn et al.
patent: 5483792 (1996-01-01), Czachor et al.
patent: 5622475 (1997-04-01), Hayner et al.
patent: 2003/0185674 (2003-10-01), Alford et al.

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