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Title: Fluidic direct-impact modulator accelerometer

Abstract: A fluidic accelerometer employing a direct-impact modulator for measuring celeration or velocity of a body along a specified axis of the accelerometer. This device uses two similar collinear power-input tubes directed toward each other. The axially opposing power jets from the tubes impact where the flow meets an air-bearing supported proofmass containing annular rings and produce symmetrical radial flow cones at the balance point. A change in the position of the proofmass causes the balance point to move which causes the radial flow cones to become asymmetrical and a net pressure difference is developed in the output receivers.


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Inventors: Hunter, Joe S. (Huntsville, AL, US)
Bailey, Escar L. (Athens, AL, US)
Little, Little J. (Huntsville, AL, US)

Application Number: 635824
Filing Date: 1975-11-28
Publication_date: 1976-08-10
Assignee: The United States of America as represented by the Secretary of the Army (Washington, DC)
Primary Class(es): 73/514.07 73/514.11, 137/824
Other Classes:
US Patent Ref:
3513710May, 1970Bates et al.73/515.
3572132Mar, 1971Trugman73/515.

Other Refs:
Primary Examiner: Gill, James J.
Assistant Examiner:
Attorney: Edelberg; Nathan, Gibson; Robert P., Carter; Charles R.