Compact thrust reverser

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60230, 23926529, F02K 172

Patent

active

055751474

ABSTRACT:
A thrust reverser (30) of a gas turbine engine (10) includes a blocker door (36) and a plurality of cascades (38). The thrust reverser (30) and the blocker door (36) have a stowed position and a deployed position. In the deployed position the blocker door (36) "leaks" airflow therethrough without generating substantial forward thrust. The leaked airflow reduces the amount of total airflow that must be accommodated by the cascades (38) of the thrust reverser (30), thereby decreasing the overall size of the cascades (38) and of the associated thrust reverser hardware and subsequently reducing the overall weight thereof.

REFERENCES:
patent: 3500644 (1970-03-01), Hom et al.
patent: 3568930 (1971-03-01), Huchar
patent: 4356973 (1982-11-01), Lawson

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