Thrust reversing arrangement for a long duct mixed flow exhaust

Power plants – Reaction motor – Interrelated reaction motors

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Details

60230, 244110B, 23926529, F02K 302

Patent

active

053137884

ABSTRACT:
A thrust reverser for a long duct mixed flow fan jet engine having a nacelle formed by a fixed forward structure surrounding the fan, a rear fixed structure and a translatable inner and outer cowl therebetween, the nacelle surrounds the engine and forms a long by-pass duct therewith, a common actuator fixed to the translatable cowls to simultaneously displace them over the rear structure, blocker doors coupled to the inner translating cowls for deployment during thrust reversal into the by-pass duct into a blocking position to divert the airflow through the cascades placed into an opening uncovered when the translatable cowls are axially displaced.

REFERENCES:
patent: 3262271 (1966-07-01), Beavers
patent: 3500645 (1970-03-01), Hom
patent: 3541794 (1970-11-01), Johnston et al.
patent: 3599432 (1971-08-01), Ellis
patent: 3603090 (1971-09-01), MacNamara et al.
patent: 3988889 (1976-11-01), Chamay et al.
patent: 4278220 (1981-07-01), Johnston et al.
patent: 4564160 (1986-01-01), Vermilye
patent: 4716724 (1988-01-01), Newton

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