Grip-yoke assembly with a redundant centrifugal load support

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Plural articulation

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416135, B64C 2748

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active

039429105

ABSTRACT:
A grip-yoke assembly for attaching a helicopter blade to the mast of the helicopter rotor having a conventional primary coupling to carry the centrifugal loads and a redundant path operative should the primary coupling fail to insure continued operability of the blade. In one embodiment, the redundant load path has a bearing surface formed on the inboard end of the grip and a corresponding thrust bearing mounted on an inboard yoke fitting for engagement with the bearing surface upon failure of the coupling. In an alternative embodiment, a bearing surface is formed on an outboard grip fitting and a corresponding thrust bearing is supported on the yoke outboard of the grip fitting.

REFERENCES:
patent: 3111172 (1963-11-01), Gorndt et al.
patent: 3280918 (1966-10-01), Drees et al.
patent: 3292712 (1966-12-01), Schmidt
patent: 3556673 (1971-01-01), Killian
patent: 3695779 (1972-10-01), Kastan et al.
patent: 3700352 (1972-10-01), Gorndt
patent: 3761199 (1973-09-01), Ferris et al.
patent: 3790302 (1974-02-01), Pascher
patent: 3807896 (1974-04-01), Johnson

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