Cooled airfoil component

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

08007237

ABSTRACT:
A gas turbine engine airfoil component having an airfoil body with a core cavity, an end opening in communication with the core cavity, and a wall having a plurality of cooling holes defined therein, each cooling hole being oriented such that the respective hole axis extends out of the core cavity through the end opening.

REFERENCES:
patent: 4118146 (1978-10-01), Dierberger
patent: 4762464 (1988-08-01), Vertz et al.
patent: 4767260 (1988-08-01), Clevenger et al.
patent: 4808785 (1989-02-01), Vertz et al.
patent: 5281084 (1994-01-01), Noe et al.
patent: 6420677 (2002-07-01), Emer et al.
patent: 6781091 (2004-08-01), Byrd et al.
patent: 7019257 (2006-03-01), Stevens
patent: 7041933 (2006-05-01), Forrester et al.
patent: 2003/0068222 (2003-04-01), Cunha et al.
patent: 2005/0058546 (2005-03-01), Cooper

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

Cooled airfoil component does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Cooled airfoil component, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooled airfoil component will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2634218

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