Centrifugal pump apparatus and method for using a single impeller with multiple passes

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United States of America Patent

PATENT NO 6447244
SERIAL NO

09567883

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Abstract

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A method of increasing the pressure of a fluid in an aircraft centrifugal pump by forcing the fluid to make multiple passes through one impeller of the aircraft centrifugal pump is provided. It includes providing fluid through a pump inlet to an aircraft impeller inlet. The fluid then exits the impeller through a first set of discharge ports and the exiting fluid is directed to a second inlet on the same impeller. The fluid then exits the impeller through a second set of discharge ports to a pump outlet. Each pass through the impeller by the fluid increases the pressure thereof.

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Patent Owner(s)

Patent OwnerAddress
ARGO-TECH CORPORATION23555 EUCLID AVENUE CLEVELAND OH 44117

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Clements, Martin A North Royalton, OH 33 202

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