Cooling layout for a turbine blade, turbine blade included...

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

C416S09600A

Reexamination Certificate

active

07658591

ABSTRACT:
A layout for cooling a blade having a cavity surrounded by an internal wall including cooling fins which are spaced apart from each other by a pitch (p) and each have a thickness (e). The blade has, inside the cavity, a jacket passed through by emission holes each having a diameter (d). When the jacket is in place in the cavity of the blade, and in respect of the critical operating point of the turbine engine, each emission hole of the jacket is opposite a place on the internal wall of the blade which is located between cooling fins.

REFERENCES:
patent: 5120192 (1992-06-01), Ohtomo et al.
patent: 5259730 (1993-11-01), Damlis et al.
patent: 5533864 (1996-07-01), Nomoto et al.
patent: 5695321 (1997-12-01), Kercher
patent: 6874988 (2005-04-01), Tiemann
patent: 6997675 (2006-02-01), Dube et al.
patent: 2003/0035726 (2003-02-01), Tiemann
patent: 0 541 207 (1993-05-01), None
Database Inspec [Online], Database Accession No. 7673232, XP-002395911, Shou-Shing Hsieh, et al., “Impingement cooling in a rotating curved square annular duct with crossflow effect from rib-roughened surfaces” vol. 39, No. 2, 2003, 1 page.

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

Cooling layout for a turbine blade, turbine blade included... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Cooling layout for a turbine blade, turbine blade included..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling layout for a turbine blade, turbine blade included... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4180524

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