Bell-shaped fan cooling holes for turbine airfoil

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C415S115000

Reexamination Certificate

active

07374401

ABSTRACT:
A turbine airfoil a plurality of cooling holes formed in the external surface of the airfoil in fluid communication with a cooling circuit. The cooling holes have a metering section and a diffuser section opening to the external surface of the airfoil. The diffuser section has top, bottom and opposed side walls, where at least the opposed side walls and one or the other of the top and bottom walls of the diffuser section have a downstream diverging, bell-shaped configuration for achieving a flow of the cooling film from the cooling circuit with enhanced spread, enhanced attachment and less turbulence to a downstream surface of the airfoil local to each respective cooling hole.

REFERENCES:
patent: 4650949 (1987-03-01), Field
patent: 4664597 (1987-05-01), Auxier et al.
patent: 4684323 (1987-08-01), Field
patent: 4922076 (1990-05-01), Cross et al.
patent: 5486093 (1996-01-01), Auxier et al.
patent: 5609779 (1997-03-01), Crow et al.
patent: 5683600 (1997-11-01), Kelley et al.
patent: 6283199 (2001-09-01), Nakamura et al.
patent: 6287075 (2001-09-01), Kercher
patent: 6368060 (2002-04-01), Fehrenbach 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

Bell-shaped fan cooling holes for turbine airfoil does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Bell-shaped fan cooling holes for turbine airfoil, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Bell-shaped fan cooling holes for turbine airfoil will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3984236

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