Mechanism for testing helicopter rotor blade fatigue properties

Details Mechanism for testing helicopter rotor blade fatigue properties Mechanism for testing helicopter rotor blade fatigue properties

1988-04-22

1989-09-12

Myracle, Jerry W.

Measuring and testing

Specimen stress or strain, or testing by stress or strain...

By loading of specimen

73812, G01N 334

Patent

active

048648639

ABSTRACT:
Mechanism for determining the fatigue properties of helicopter rotor blade flexbeam sections using one motor driven eccentric for imparting combined bending, twisting and deflection loads to a flexbeam.

REFERENCES:
patent: 3170321 (1965-02-01), Sullivan et al.
patent: 4089211 (1978-05-01), Vercellone et al.

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