Mast torque metering system

Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes

Patent

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Details

73136A, 416 38, 416 61, B64C 2700

Patent

active

040835189

ABSTRACT:
In a helicopter, torque display for a main rotor mast is mounted and connected to be driven from a power source at its base and connected to a main rotor at its tip. A reference member secured inside the main mast at the tip thereof depends freely and extends coaxially the length of the mast to a point adjacent the base thereof. A separate index is carried by the reference member adjacent to the base and by the main rotor mast adjacent to its base. A pick-off senses rotational movement of one index relative to the other and provides for actuation of a torque indicator for the pilot of the helicopter.

REFERENCES:
patent: 2397935 (1946-04-01), Gardiner et al.
patent: 2699833 (1955-01-01), Jensen
patent: 3174551 (1965-03-01), McCarthy
patent: 3538762 (1970-11-01), Parkinson et al.
patent: 3625055 (1971-12-01), Lafourcade
patent: 3672213 (1972-06-01), Watson

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