Aircraft engine flexible fluid damped coupling

Details Aircraft engine flexible fluid damped coupling Aircraft engine flexible fluid damped coupling

1975-01-22

1976-05-04

Scott, Samuel

64 6, 64 15C, 64 26, F16D 314

Patent

active

039539873

ABSTRACT:
The flexible mechanical coupling herein shown comprises a drive member, flange and internally notched barrel in rigid relationship. The flange is a part of a helically formed coil-like torsion spring. An externally toothed sleeve is in concentric relationship to the barrel with its teeth in loose engagement with the notches. The driven element and the sleeve and the end of the torsion spring remote from the flanged end are secured in rigid relationship. The reservoir within the barrel is filled with viscous damping fluid.

REFERENCES:
patent: 1464220 (1923-08-01), Sachs et al.
patent: 2006578 (1935-07-01), Tate
patent: 2394405 (1946-02-01), Schjolin
patent: 2397700 (1946-04-01), Sloan
patent: 3122902 (1964-03-01), Blair et al.

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