High "G" gyro with fluidic exhaust control for fluidic bearing
AssigneeThe United States of America as represented by the Secretary of the Army
InventorRayburn K. Widner
Life of this patent
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Abstract
A high "G" gyro that has a rotor mounted relative to a stator by a fluidic earing with fluidic exhaust control means for producing a lower pressure at the exhaust for the fluidic bearing to prevent the exhaust from the fluidic bearing from impinging on other portions of the rotor to cause error signals to be produced. By locating the exhaust for the fluidic bearing radially outwardly from the inlet ports to the fluidic bearing, and by producing a lower pressure at the exhaust, the exhaust fluids from the bearing are attracted to the exhaust and prevented from impinging and exerting undesirable forces on the rotor.
Claims4
A gyro comprising a stator housing, a rotor rotatably mounted in said stator housing by fluidic bearing means, said fluidic bearing means having a plurality of circumferentially arranged ports that have means for admitting fluid to said plurality of circumferentially arranged ports and said plurality of circumferentially arranged ports opening into a fluidic space defined between said rotor said rotor stator housing, exhaust means consisting of a circumferentially arranged exhaust from said fluidic bearing space and being located radially outwardly from said ports, and means for providing a reduced pressure at said circumferentially arranged exhaust to cause the fluid from the fluidic bearing space to be attracted to said exhaust and prevent the fluid from the bearing space from exerting undesirable forces on said rotor, said means for providing said reduced pressure at said circumferentially arranged exhaust consisting of a jet arrangement in said stator housing in which an outlet passage from said circumferential exhaust communicates at a 90.degree. angle with a jet outlet that receives fluid through a restricted orifice from an inlet passage to cause the fluid being jetted through said orifice and into said jet outlet to cause a low pressure to be produced in said outlet passage and said circumferential exhaust.
Dependencies are inferred from the claim text.