Gas turbine engine combustor

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

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Details

60752, F02C 314

Patent

active

053985095

ABSTRACT:
A gas turbine engine combustor comprises a combustion chamber the walls of which have a plurality of holes extending therethrough for the flow of cooling air into the interior of the chamber. The holes are so configured and arranged that cooling air is exhausted from them in a flow direction which is normal or oblique to the general direction of gas flow through the chamber and oblique to the portion of the chamber wall local thereto.

REFERENCES:
patent: 2659201 (1953-11-01), Krejci
patent: 4429538 (1984-02-01), Sato et al.
patent: 4702073 (1987-10-01), Malconian
patent: 5129231 (1992-07-01), Becker
patent: 5226278 (1993-07-01), Meylan et al.
patent: 5233828 (1993-08-01), Napoli

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