Electrical grounding connector for a helicoptor rotor

Details Electrical grounding connector for a helicoptor rotor Electrical grounding connector for a helicoptor rotor

1987-09-17

1989-02-28

Weidenfeld, Gil

Fluid reaction surfaces (i.e., impellers)

With illumination means

174 6, 439 98, H01R 466

Patent

active

048080721

ABSTRACT:
An electrical grounding connector for a helicopter rotor hub (15) comprises a bushing (25) which receives a hollow spindle (30) therewithin. Spindle (30) accommodates a cable or wire harness (35) therewithin and is rotatable within the bushing to accommodate twisting of the harness due to displacement of the helicopter blades. An electrical connection to hub (15) is made via flexible conductor (75), the spindle, and flexible conductor (60).

REFERENCES:
patent: 4320252 (1982-03-01), Holman et al.
patent: 4424947 (1984-01-01), Adams et al.

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