Landing gear noise reduction

Aeronautics and astronautics – Landing gear

Reexamination Certificate

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Details

C244S11000H

Reexamination Certificate

active

07484688

ABSTRACT:
An aircraft landing gear (1) is described including a noise-reducing element that includes an air-deflecting surface, in the form of a fairing (4), and a perforated airflow-reducing region (8). In use, some air passes through the perforations, whilst other air is deflected by the fairing away from a noise-generating region of the landing gear. Noise caused by the passing of the landing gear through the air is therefore reduced.

REFERENCES:
patent: 2176461 (1939-10-01), Larsen
patent: 2180462 (1939-11-01), De Seversky
patent: 2941756 (1960-06-01), Roberts
patent: 3934923 (1976-01-01), Lissaman et al.
patent: 4537373 (1985-08-01), Butts
patent: 6786451 (2004-09-01), Courtois et al.
patent: 1 067 045 (2001-01-01), None
patent: 1 340 676 (2003-09-01), None
patent: 579657 (1944-08-01), None
patent: 568331 (1945-03-01), None
patent: 608883 (1948-09-01), None
patent: 958427 (1964-05-01), None
patent: 603804 (1984-06-01), None
patent: WO 01/04003 (2001-01-01), None

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