Method of making aerofoil blisks

Metal fusion bonding – Process – Using dynamic frictional energy

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C029S889210

Reexamination Certificate

active

07410089

ABSTRACT:
A method of making an aerofoil blisk (10) comprising a plurality of aerofoil blades (12) joined to a disc (14) to extend radially outwardly therefrom includes the step of forming a blade member (28) having a stub (30) for joining to the disc (14), the stub (30) having a taper ratio of less than 2. The stub (30) of the blade member (28) may be joined to the disc (14) by linear friction welding, and excess material may subsequently be machined from the blade member (28) to form the blade (12).

REFERENCES:
patent: 4934583 (1990-06-01), Patsfall
patent: 5492581 (1996-02-01), Searle
patent: 5791878 (1998-08-01), Wainauski et al.
patent: 5797182 (1998-08-01), Furlan
patent: 5865364 (1999-02-01), Trask et al.
patent: 6095402 (2000-08-01), Brownell et al.
patent: 6106233 (2000-08-01), Walker
patent: 6219916 (2001-04-01), Walker et al.
patent: 6478545 (2002-11-01), Crall et al.
patent: 6542843 (2003-04-01), Metzinger et al.
patent: 6669447 (2003-12-01), Norris et al.
patent: 6688512 (2004-02-01), Trask
patent: 2002/0070492 (2002-06-01), Collot
patent: 0 624 418 (1994-11-01), None
patent: 0 850 718 (1998-07-01), None
patent: 0 887 143 (1998-12-01), None
patent: 0 924 016 (1999-06-01), None
patent: 1 239 116 (2002-09-01), None
patent: 1 312 766 (2003-05-01), None

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

Method of making aerofoil blisks does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of making aerofoil blisks, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of making aerofoil blisks will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4016013

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