Attenuation of a closing flap for a secondary air intake opening

Fluid handling – Processes – Cleaning – repairing – or assembling

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Details

23926517, 244 53B, 16 84, B64D 3302

Patent

active

039917827

ABSTRACT:
The flap covering or opening a secondary air intake in an aircraft engine is linked to a shock attenuator so that movements of the flap near the closing position are strongly attenuated while movement about the fully open position is very little attenuated.

REFERENCES:
patent: 634596 (1899-10-01), Warner
patent: 1875593 (1932-09-01), Hall
patent: 3664612 (1972-05-01), Skidmore
patent: 3900177 (1975-08-01), Calder et al.

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