Gas turbine with combustor bypass valve

Power plants – Combustion products used as motive fluid – With variable oxidizer control

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60 39464, F02C 918

Patent

active

056923708

ABSTRACT:
An assembly includes a gas turbine with an inlet, a combustion air compressor with an outlet, a combustion chamber, and a common wall between the outlet of the compressor and the inlet of the turbine. A gas valve has a transverse bulkhead serving as a transverse separating wall on at least one side of the common wall, and a slide covering the transverse bulkhead and the common wall in the vicinity of the compressor. The slide has slots formed therein for alternatingly closing corresponding slots formed in the common wall and in the transverse bulkhead.

REFERENCES:
patent: 2837894 (1958-06-01), Kind
patent: 4144016 (1979-03-01), Takahashi et al.
patent: 4211069 (1980-07-01), Kalbfuss
patent: 4860535 (1989-08-01), Mansson et al.

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