Gas turbine engine power plants for aircraft

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60231, 23926523, 244110B, 60224, F02K 302

Patent

active

040473813

ABSTRACT:
Gas turbine engine power plants sometimes are provided with thrust reversing equipment, the outlet of which is close to the power plant air intake. Such arrangements create re-ingestion problems. There is described herein an apparatus which either maintains the upstream portion of reversed flow in a given position with respect to the plane of the air intake or alternatively destroys the reversed flow entirely.

REFERENCES:
patent: 3605411 (1971-09-01), Maison
patent: 3660981 (1972-05-01), Stevens
patent: 3729934 (1973-05-01), Denning
patent: 3736750 (1973-06-01), Britt

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