Deployable rotor

Fluid reaction surfaces (i.e. – impellers) – Radially extensible or retractible rotor working member – Having pitch adjustment

Patent

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Details

416134A, 416142, B64C 2772

Patent

active

041116020

ABSTRACT:
A deployable stowed rotor having a rotor hub to which a pair of telescoping otor blades are connected is foldable into a package suitable for stowage prior to use. When the rotor is deployed, for example, as a lifting device for an ejection seat, positive preconing of the blades is provided by a spreading link arrangement connected to a drogue chute. Further coning during rotor spin-up is synchronized by intermeshed gears provided at respective one ends of the blades attached to the hub by teeter link hinges. Rotor speed is automatically regulated by a governing spring formed in conjunction with a helical spline arrangement between each of the blades and the hub and which varies the pitch of the spinning blades according to rotational velocity.

REFERENCES:
patent: 2282077 (1942-05-01), Moore
patent: 2415421 (1947-02-01), Filippis
patent: 2990149 (1961-06-01), Samms
patent: 3292711 (1966-12-01), Peterson
patent: 3297094 (1967-01-01), Kisovec
patent: 3700352 (1972-10-01), Gorndt

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