Turbine combustor cooling system

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60757, F02C 712

Patent

active

053297733

ABSTRACT:
A gas turbine engine has a low cost combustor liner cooling system combining the benefits of high internal heat removal with improved film cooling by employing a large number of strategically positioned, laser-drilled cooling passages. Cooling air flows through these specially tailored passages to absorb heat from the liner prior to injection as a protective film on the interior surface. The passages are set in staggered rows on a thickened portion of the liner and have a rough internal heat transfer surface and an exit with a steep injection angle to evenly distribute the cooling film along the interior surface of the liner.

REFERENCES:
patent: 2785878 (1957-03-01), Conrad
patent: 3353359 (1967-11-01), Webb
patent: 3420058 (1969-01-01), Howald et al.
patent: 3623711 (1971-11-01), Thorstenson
patent: 3706203 (1972-12-01), Goldberg et al.
patent: 3737152 (1973-06-01), Wilson
patent: 3811276 (1974-05-01), Caruel et al.
patent: 3995422 (1976-12-01), Stamm
patent: 4242871 (1981-01-01), Breton
patent: 4622821 (1986-11-01), Madden
patent: 4684323 (1987-08-01), Field
patent: 4708750 (1987-11-01), Field et al.
patent: 4773593 (1988-09-01), Auxier et al.
Comparison of Advanced Cooling Concepts Using Color Thermography, G. Myers et al, AIAA Paper No. 85-1289, Jul. 1985.
Evaluation of Laminated Porous Wall Materials for Combustor Liner Cooling, D. Nealy et al, ASME Paper No. 79-GT-100, Dec. 1978.

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

Turbine combustor cooling system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine combustor cooling system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine combustor cooling system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-512486

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