Thrust augmentation technique and apparatus

Power plants – Reaction motor – Method of operation

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Details

60264, 60269, F23R 100

Patent

active

040302890

ABSTRACT:
A thrust augmentation technique wherein a primary gas stream is directionally switched at a high rate to produce flow discontinuities in the interest of increasing efficiency. Apparatus in accordance with the invention includes a fluidic switch, particularly a controlled expansion thrust vector control nozzle, which delivers a pulsating primary gas stream to an eductor or lift surface.

REFERENCES:
patent: 3420060 (1969-01-01), Ostroff et al.

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