Pulsed turbine rotor engine

Power plants – Combustion products used as motive fluid – Rotating combustion products generator and turbine

Reexamination Certificate

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Reexamination Certificate

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06907723

ABSTRACT:
A pulsed turbine rotary engine comprising a fixed section, an output shaft, a plurality of nozzle openings, an air supply system, a fuel supply system, and an ignition system. The fixed section defines a plurality of intake openings each defining an intake axis. The output shaft is supported by the fixed section for rotation about a shaft axis. The nozzle housings are operatively connected to the output shaft for rotation about the shaft axis. Each nozzle housing defines a nozzle chamber in fluid communication with a nozzle inlet and a nozzle outlet defining a thrust axis. The air and fuel supply systems direct air and fuel through the intake openings. The ignition system comprises spark plugs for igniting fuel within the nozzle chambers.

REFERENCES:
patent: 903657 (1908-11-01), Beckmann
patent: 2486990 (1949-11-01), Sharpe
patent: 3089307 (1963-05-01), Kollander
patent: 3375657 (1968-04-01), Sherwood et al.
patent: 4590761 (1986-05-01), Zettner
patent: 4807440 (1989-02-01), Salem
patent: 5138831 (1992-08-01), Cowan, Sr.
patent: 5660038 (1997-08-01), Stone
patent: 5709088 (1998-01-01), Acaster

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