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

2006-08-22

2006-08-22

Casaregola, Louis J. (Department: 3746)

Fluid reaction surfaces (i.e., impellers)

Rotor having flow confining or deflecting web, shroud or...

Axially extending shroud ring or casing

C060S226100

Reexamination Certificate

active

07094033

ABSTRACT:
A method for assembling a fan platform for a gas turbine engine is provided. The method includes determining an area of vulnerability to impact and erosion damage across the platform, forming a sheet of cladding metal to substantially conform to a contour of the identified area of vulnerability of the platform, and bonding the cladding metal to the identified area of vulnerability.

REFERENCES:
patent: 3155536 (1964-11-01), Fremann et al.
patent: 3494539 (1970-02-01), Littleford
patent: 5836744 (1998-11-01), Zipps et al.
patent: 6217283 (2001-04-01), Ravenhall et al.
patent: 6832896 (2004-12-01), Goga 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-3635012