Pulsed combustion turbine engine

Power plants – Reaction motor – Interrelated reaction motors

Reexamination Certificate

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Details

C060S247000, C060S248000, C060S039340, C060S039380, C060S039780

Reexamination Certificate

active

06901738

ABSTRACT:
A turbine engine has a circumferential array of combustion chamber conduits downstream of the compressor and upstream of the turbine. Means are provided for directing oxygen-containing gas from the compressor to the conduits so as to cyclically feed a gas charge into each conduit through its first port and permit discharge of combustion products of the charge and fuel through both the first and second ports.

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