Turbine airfoil cooling system with perimeter cooling and...

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

Reexamination Certificate

active

07547191

ABSTRACT:
A cooling system for a turbine airfoil of a turbine engine having a perimeter cooling channel formed from a portion of a serpentine cooling channel, an airfoil tip cooling channel, and a leading edge cooling channel. The cooling system also includes cooling channels enabling cooling fluids to be discharged into the root of the airfoil to cool rim cavities and purge air therein. The cooling system may be configured such that the cooling fluids may pass into a mid-chord serpentine cooling channel, flow through the serpentine cooling channel generally in a chordwise direction from the leading edge toward the trailing edge, flow toward the tip section and along the trailing edge, flow from the trailing edge toward the leading edge in the airfoil tip cooling channel, flow along the leading edge in the leading edge cooling channel, through the root of the blade, and be exhausted into a rim cavity.

REFERENCES:
patent: 4073599 (1978-02-01), Allen et al.
patent: 4136516 (1979-01-01), Corsmeier
patent: 4775296 (1988-10-01), Schwarzmann et al.
patent: 5253976 (1993-10-01), Cunha
patent: 5403159 (1995-04-01), Green et al.
patent: 5601399 (1997-02-01), Okpara et al.
patent: 5772397 (1998-06-01), Morris et al.
patent: 5915923 (1999-06-01), Tomita et al.
patent: 5975850 (1999-11-01), Abuaf et al.
patent: 6019579 (2000-02-01), Fukuno et al.
patent: 6036440 (2000-03-01), Tomita et al.
patent: 6142734 (2000-11-01), Lee
patent: 6241467 (2001-06-01), Zelesky et al.
patent: 6254333 (2001-07-01), Merry
patent: 6257830 (2001-07-01), Matsuura et al.
patent: 6595748 (2003-07-01), Flodman et al.
patent: 6672836 (2004-01-01), Merry
patent: 6872047 (2005-03-01), Tanioka
patent: 6974308 (2005-12-01), Halfmann 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 airfoil cooling system with perimeter cooling and... 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 cooling system with perimeter cooling and..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine airfoil cooling system with perimeter cooling and... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4120886

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