Turbine nozzle segment and method of repairing same

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C415S210100, C416S19300A, C416S195000

Reexamination Certificate

active

06905308

ABSTRACT:
A method is provided for repairing a turbine nozzle segment having at least one vane disposed between outer and inner bands. The method includes separating the inner band from the nozzle segment, and joining the inner band to a newly manufactured replacement casting having an outer band and a vane. The replacement casting includes an airfoil stub. The airfoil stub is received in a recess formed in the inner band. Joining is completed by joining the airfoil stub to the inner band. The replacement casting may be modified from a newly manufactured singlet casting.

REFERENCES:
patent: 3802046 (1974-04-01), Wachtell et al.
patent: 4305697 (1981-12-01), Cohen et al.
patent: 4326833 (1982-04-01), Zelahy et al.
patent: 5248240 (1993-09-01), Correia
patent: 5269057 (1993-12-01), Mendham
patent: 5272809 (1993-12-01), Robertson et al.
patent: 5690469 (1997-11-01), Deal et al.
patent: 5758416 (1998-06-01), Reverman et al.
patent: 5797725 (1998-08-01), Rhodes
patent: 5813832 (1998-09-01), Rasch et al.
patent: 6154959 (2000-12-01), Goodwater et al.
patent: 6173491 (2001-01-01), Goodwater et al.
patent: 6183192 (2001-02-01), Tressler et al.
patent: 6416278 (2002-07-01), Caddell, Jr. 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

Turbine nozzle segment and method of repairing 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 Turbine nozzle segment and method of repairing same, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine nozzle segment and method of repairing same will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3508664

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