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

2007-10-09

2007-10-09

Kershteyn, Igor (Department: 3745)

Rotary kinetic fluid motors or pumps

Working fluid passage or distributing means associated with...

Plural distributing means immediately upstream of runner

C415S196000, C415S208200, C029S889210

Reexamination Certificate

active

10982050

ABSTRACT:
A gas turbine engine compressor including a stator assembly and a method of assembling the same are provided. The method includes providing a compressor casing including at least two stator vane casing rails extending from the casing, coupling a rail liner within each respective casing rail, and coupling a stator vane assembly including two dovetails, and at least two stator vanes coupled together within the casing rails within the liner such that a first dovetail is received within a first casing rail and a first rail liner, and a second dovetail is received within a second casing rail and a second rail liner.

REFERENCES:
patent: 2945290 (1960-07-01), Walsh
patent: 3072381 (1963-01-01), Lameris
patent: 4155680 (1979-05-01), Linko et al.
patent: 4270256 (1981-06-01), Ewing
patent: 5182855 (1993-02-01), Martin
patent: 5188507 (1993-02-01), Sweeney
patent: 5192185 (1993-03-01), Leonard
patent: 5333995 (1994-08-01), Jacobs et al.
patent: 6179557 (2001-01-01), Dodd et al.
patent: 6609880 (2003-08-01), Powis et al.
patent: 6729842 (2004-05-01), Drerup et al.
patent: 6808364 (2004-10-01), O'Reilly et al.
patent: 2003/0057263 (2003-03-01), Beedon et al.

Affiliated with

Also associated with

Rating

Methods and apparatus for assembling gas turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Methods and apparatus for assembling gas turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Methods and apparatus for assembling gas turbine engines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3896018