US 4,069,990 AGranted

Ring-wing canard spin-up control mechanism

AssigneeThe United States of America as represented by the Secretary of the Army

InventorsAubrey Rodgers, Rayburn K. Widner

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Abstract

Apparatus of the present invention requires a very short spin-up wheel mot arm compared to a large wheel diameter. Such a requirement demands good wheel control during low rpm and excellent stability for high rpm in order to avoid uncontrollable wheel oscillations. Uncontrollable oscillations will prevent the wheel from either completing the spin-up cycle or it will destroy the gas bearing. Apparatus of the present invention uses a combination of a gas film bearing to control the alignment of the wheel during low rpm and a point contact configuration that uses the gyroscopic law of angular momentum to achieve wheel stability for the high rpm. The gyro law states that the angular momentum vector will precess into the torque vector. The spin-up control mechanism can be used to control and maintain stability of any wheel that has a large OD to small spin-up moment arm ratio requirement. An advantage of the structure of the present invention is that it utilizes the available angular momentum energy to capture and maintain wheel stability during the spin-up cycle. The higher the wheel rpm is, the better the control.

Claims5

Dependent claims

Apparatus for imparting spin to a member comprising:

a. a housing having a stator secured thereto, said stator having a chamber therein, an axial inlet for directing air to said chamber, an axial outlet for directing air axially out of said chamber, and, radially extending passages for directing air to the outer surface of said stator;
b. a rotor disposed for rotation about said stator, said rotor having an inner surface adjacent said outer surface of said stator for providing an air bearing between said rotor and said stator in response to air flow from said chamber through said radially extending passages,
c. a rotatable assembly secured to said rotor for rotation therewith, said assembly including a forward spherical portion and a rear cylindrical portion having passages therein in communication with the air between said stator and rotor and the distal edge of said cylindrical portion;
d. spin-up nozzle means communicating with a second air source and with said rotor for impingment of air thereon for rotation thereof;
e. point contact means disposed for actuation by said air exhausting from said axial outlet to align said rotating assembly in a plane with said spin-up nozzles;
and,
f. caging means for caging and uncaging said rotating assembly responsive to rotation thereof.

4 more elements

Dependencies are inferred from the claim text.