Microcircuit cooling for a 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

07097425

ABSTRACT:
A turbine airfoil includes a plurality of cooling circuits embedded within the pressure and suction sidewalls and a first and a second flow passage. The first flow passage feeds the coolant fluid to the cooling circuits that are embedded only within the pressure sidewall and the second flow passage feeds the coolant fluid to the cooling circuits that are embedded only within the suction sidewall. A method embodiment of the present comprises placing the inlets of the cooling circuits embedded within the first sidewall in flow communication with only one of the flow passages and placing the inlets of the cooling circuits embedded within the second sidewall in flow communication with at least one of the other flow passages to minimize the difference in sink pressures of the suction and pressure sidewalls to ensure ingestion of the coolant fluid into the inlets of the respective cooling circuits.

REFERENCES:
patent: 3801218 (1974-04-01), Moore
patent: 4050133 (1977-09-01), Cretilla et al.
patent: 4312624 (1982-01-01), Steinbauer et al.
patent: 6247896 (2001-06-01), Auxier et al.
patent: 6280140 (2001-08-01), Soechting et al.
patent: 6331217 (2001-12-01), Burke et al.
patent: 6402470 (2002-06-01), Kvasnak et al.
patent: 6514042 (2003-02-01), Kvasnak et al.
patent: 2002/0021966 (2002-02-01), Kvasnak et al.
European Patent Office Search Report dated Jun. 22, 2005, received from Frank B. Dehn & Co. on Jul. 5, 2005, three pages.

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

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

Rate now

     

Profile ID: LFUS-PAI-O-3647426

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