Combustion chamber liner insert

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

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Details

60759, 60760, F23R 304

Patent

active

048753394

ABSTRACT:
An air admission insert particularly adapted for air admission holes in a combustor liner in a gas turbine combustion system comprises a pair of sleeve members, one of which is inserted in the other in axial but eccentric relationship so that the sides of the sleeves contact each other with the intervening space between the sleeves being crescent shaped. The insert is positioned concentrically in a combustor liner air admission hole. Combustion air flows through the insert and into the combustor liner and axially through the crescent space to cool the insert as well as the liner hold perimeter.

REFERENCES:
patent: 2510645 (1950-06-01), McMahan
patent: 3899882 (1975-08-01), Parker
patent: 4622821 (1986-11-01), Madden
patent: 4653279 (1987-03-01), Reynolds
patent: 4700544 (1987-10-01), Fucci

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