Thrust augmenting fluid rectifier for a pulsed combustor

Details Thrust augmenting fluid rectifier for a pulsed combustor Thrust augmenting fluid rectifier for a pulsed combustor

1975-08-21

1977-07-05

Croyle, Carlton R.

Power plants

Reaction motor

Intermittent combustion

60 3977, F02K 702

Patent

active

040331202

ABSTRACT:
A thrust augmenting fluid rectifier for a pulsed combustor comprising ducting having a converging inlet section, a flow redirecting section and a diffuser section, the inlet of the ducting being spaced upstream from the combustor inlet to define a thrust augmentor utilizing the backflow from the combustor inlet as primary fluid. In one embodiment the rectifier ducting extends rearwardly to a chamber that combines it with the combustor outlet. Substantial pressure gain is obtainable making the invention suitable for gas turbine applications.

REFERENCES:
patent: 2738646 (1956-03-01), Kadosch et al.
patent: 2812635 (1957-11-01), LeFoll et al.
patent: 2834183 (1958-05-01), Bertin et al.
patent: 2919542 (1960-01-01), Servanty et al.

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