Liner cooling construction for gas turbine combustor or the like

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60759, F02C 712, F02C 720

Patent

active

047901403

ABSTRACT:
A liner cooling construction for a gas turbine combustor or the like in which twisted or helical tapes in the spaces defined between the liner walls and the partition walls cause the cooling air to swirl so that the efficient cooling of the liner walls can be ensured.

REFERENCES:
patent: 3307354 (1967-03-01), Macaulay et al.
patent: 3579162 (1971-05-01), Savkar
patent: 4064300 (1977-12-01), Bhargu
patent: 4361010 (1982-11-01), Tanrikut et al.
patent: 4446693 (1984-05-01), Pidcock et al.
patent: 4607487 (1986-08-01), Tilston

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

Liner cooling construction for gas turbine combustor or the like does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Liner cooling construction for gas turbine combustor or the like, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Liner cooling construction for gas turbine combustor or the like will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2189760

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