Cooling medium path structure for gas turbine blade

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416 95, 416 96R, 416220R, 415115, 415135, 415136, F01D 508

Patent

active

059846372

ABSTRACT:
A cooling medium path structure for cooling a gas turbine blade. The structure includes a disk-side cooling medium path, a blade-side cooling medium path formed at the root portion of the blade and a delivery block disposed between the two cooling medium paths so as to establish communication therebetween. The delivery block is provided with an elastic engaging section which comes into elastic and line-contact with the disk-side cooling medium path and the blade-side cooling medium path. Thus, the sealing property of the contact portions of the structure is secured so as to allow a cooling medium to be supplied without leaking from the cooling medium paths. The heat of the cooling medium, generated as a result of cooling the high-temperature portion of the gas turbine, can be recovered so as to make the best use of the heated medium.

REFERENCES:
patent: 4118136 (1978-10-01), Corsmeier et al.
patent: 4136516 (1979-01-01), Corsmeier
patent: 4190398 (1980-02-01), Corsmeier et al.
patent: 5318404 (1994-06-01), Carreno et al.
patent: 5593274 (1997-01-01), Carreno et al.
patent: 5795130 (1998-08-01), Suenaga et al.
patent: 5823743 (1998-10-01), Faulkner
patent: 5846048 (1998-12-01), Tomita 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

Cooling medium path structure for gas turbine blade 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 medium path structure for gas turbine blade, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling medium path structure for gas turbine blade will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1316367

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