Cooling apparatus for split shaft gas turbine

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60 3966, 415115, F02C 310, F02C 718

Patent

active

040345580

ABSTRACT:
This invention relates to cooling a section of a split shaft gas turbine engine. Because combustion takes place in the region of the shaft-split, overheating may occur and care must be taken to ensure that this portion of the turbine is sufficiently cooled. This invention is concerned with bleeding a portion of the compressed air from an intermediate stage of the compressor turbine and feeding the compressed air into a manifold. Next the air is fed by means of suitable conduit members into the split-shaft region of the turbine. Provision is made to feed this air to the faces of the power disc for the compressor section and the face of the power disc for the output power section of the turbine. Various other parts of the turbine are also cooled in the split shaft region of the turbine.

REFERENCES:
patent: 2749087 (1956-06-01), Blackman et al.
patent: 3034298 (1962-05-01), White
patent: 3275294 (1966-09-01), Allen et al.
patent: 3945758 (1976-03-01), Lee

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

Rate now

     

Profile ID: LFUS-PAI-O-480854

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