Installation for affording electrical continuity for rotorcraft

Details Installation for affording electrical continuity for rotorcraft Installation for affording electrical continuity for rotorcraft

1996-07-12

1998-02-10

Verdier, Christopher

Fluid reaction surfaces (i.e., impellers)

Articulated, resiliently mounted or self-shifting impeller...

Nonmetallic resilient mounting

416 39, 416140, 416141, 416143, 416146R, 416500, 244 1A, 361218, B64C 2739, B64C 2750

Patent

active

057161933

ABSTRACT:
The installation for removing electrostatic charge and passing lightning current between a conductor of each blade of the rotor and a metallic part of the hub comprises at least one conductive member integral with the member for linking the blade to the hub in its angular deflections, and in electrical continuity with the conductor of the blade and held elastically in permanent contact with a conductive terminal integral with the hub and in electrical continuity therewith.

REFERENCES:
patent: 3804552 (1974-04-01), Covington
patent: 4268222 (1981-05-01), Bernard
patent: 4304525 (1981-12-01), Mouille
patent: 4574325 (1986-03-01), Holton
patent: 5267833 (1993-12-01), Mouille

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