Debris deflecting device, system, and method

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Reexamination Certificate

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Details

C244S10000R

Reexamination Certificate

active

07946531

ABSTRACT:
A debris deflector includes a bracket and a horizontal blade assembly. The bracket is to secure the debris deflector to an aft side of a landing gear assembly. The horizontal blade assembly is secured to the bracket. The horizontal blade assembly includes a blade and flap. The blade has a forward blade edge, blade body, and trailing blade edge. The forward blade edge is configured for placement aft of a tire for the landing gear assembly. The blade body extends outward from the forward blade edge substantially parallel to a road surface. The flap is secured to the trailing blade edge and extends from the trailing blade edge generally rearward and downward from the trailing edge.

REFERENCES:
patent: 3088751 (1963-05-01), Barry et al.
patent: 3670996 (1972-06-01), Jenny
patent: 4389029 (1983-06-01), Glasenapp et al.
patent: 4681285 (1987-07-01), Bowdy et al.
patent: 5058827 (1991-10-01), Dansereau et al.
patent: 6845943 (2005-01-01), Chambers et al.

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