Soft in-plane tiltrotor hub

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Nonmetallic resilient mounting

Reexamination Certificate

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Details

C416S107000, C416S140000, C416S141000, C416S148000, C188S282100, C188S283000, C188S266300, C188S299100, C188S319200, C188S322150

Reexamination Certificate

active

07828525

ABSTRACT:
A rotor hub assembly for a rotary-wing aircraft has a central member and a plurality of blade grips adapted for attaching rotor blades to the central member. The blade grips are pivotally attached to the central member and are capable of pivoting about a pivot axis generally normal to a plane of rotation of the blades. The pivoting allows for in-plane motion of the blades relative to the central member. A damper is operably connected to each blade grip for damping the in-plane motion of the associated blade, each damper being selectively switchable between at least two spring rates.

REFERENCES:
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patent: 2774553 (1956-12-01), Jensen
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patent: 1500007 (1978-02-01), None
patent: 1514347 (1978-06-01), None

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