Turbine airfoil with improved cooling

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C416S09700R

Reexamination Certificate

active

07600966

ABSTRACT:
A turbine airfoil includes an outer wall and a plurality of cooling passages or minicores formed in the outer wall. A web separates each adjacent pair of the minicores. In order to provide more effective, even cooling of the airfoil, a baffle inside the airfoil includes a plurality of outlets aligned with the webs. The fluid outlets direct the cooling fluid directly onto the web. The cooling fluid then flows through the minicores and out through exits in the minicores.

REFERENCES:
patent: 4542867 (1985-09-01), Memmen
patent: 5392515 (1995-02-01), Auxier et al.
patent: 6000908 (1999-12-01), Bunker
patent: 6164912 (2000-12-01), Tabbita et al.
patent: 6282905 (2001-09-01), Sato et al.
patent: 6514042 (2003-02-01), Kvasnak et al.
patent: 6769866 (2004-08-01), Kannefass et al.
patent: 6932571 (2005-08-01), Cunha et al.
patent: 7255534 (2007-08-01), Liang
European Search Report for EP Application No. 06255893.7, Apr. 21, 2008.

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 airfoil with improved cooling 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 airfoil with improved cooling, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine airfoil with improved cooling will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4106469

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