Thrust reverser for a fluid flow propulsion engine

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

23926531, F02K 120

Patent

active

041776399

ABSTRACT:
In a gas turbine ducted fan engine, the inner wall portion which during cruise blocks the inner end of the reverser outlet, and the blocker flaps are separate entities which are aligned with each other in an upstream, downstream direction. This enables inter alia, the inner wall portion to be of much stiffer construction than hitherto, per unit volume of material used and thus improves sealing of the fan duct.

REFERENCES:
patent: 3568931 (1971-03-01), Mortlock
patent: 3620022 (1971-11-01), Beale
patent: 4047682 (1977-09-01), Brownhill

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