Gas turbine engine assembly and methods of assembling same

Power plants – Combustion products used as motive fluid – With lubricators

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C415S170100, C384S099000, C384S474000, C384S475000, C384S537000, C384S584000

Reexamination Certificate

active

07574854

ABSTRACT:
A method for assembling a gas turbine engine is provided. The method includes coupling a high-pressure compressor to a high-pressure turbine using a first shaft, coupling a fan assembly to a low-pressure turbine using a second shaft, and coupling a differential squeeze film damper assembly between the first and second shafts.

REFERENCES:
patent: 3910651 (1975-10-01), Pearce et al.
patent: 4214796 (1980-07-01), Monzel et al.
patent: 4378197 (1983-03-01), Cattaneo et al.
patent: 5048978 (1991-09-01), Singh
patent: 5085521 (1992-02-01), Singh
patent: 5169241 (1992-12-01), Singh
patent: 5178400 (1993-01-01), Singh
patent: 5188375 (1993-02-01), Pope et al.
patent: 5197807 (1993-03-01), Kuznar
patent: 5201585 (1993-04-01), Gans et al.
patent: 5228784 (1993-07-01), Bobo
patent: 5251985 (1993-10-01), Monzel
patent: 5316391 (1994-05-01), Monzel
patent: 5320134 (1994-06-01), Singh
patent: 5344239 (1994-09-01), Stallone et al.
patent: 5813214 (1998-09-01), Moniz et al.
patent: 5867976 (1999-02-01), Ziegler, Jr.
patent: 6036413 (2000-03-01), Chandrasekar
patent: 6135639 (2000-10-01), Dede
patent: 2003/0097844 (2003-05-01), Seda
patent: 2004/0062460 (2004-04-01), Dusserre-Telmon et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Gas turbine engine assembly and methods of assembling same does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine engine assembly and methods of assembling same, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine engine assembly and methods of assembling same will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4062318

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.