The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 07, 2019

Filed:

Dec. 18, 2013
Applicant:

GE Oil & Gas Esp, Inc., Oklahoma City, OK (US);

Inventors:

Vishal Gahlot, Moore, OK (US);

Colby Lane Loveless, Oklahoma City, OK (US);

Mark James, Oklahoma City, OK (US);

Assignee:

GE OIL & GAS ESP, INC., Oklahoma City, OK (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/041 (2006.01); F04D 29/06 (2006.01); F04D 1/06 (2006.01); F04D 13/10 (2006.01); F04D 29/047 (2006.01); E21B 43/12 (2006.01); F04B 47/06 (2006.01); F04D 29/44 (2006.01);
U.S. Cl.
CPC ...
F04D 29/041 (2013.01); E21B 43/128 (2013.01); F04B 47/06 (2013.01); F04D 1/06 (2013.01); F04D 13/10 (2013.01); F04D 29/0413 (2013.01); F04D 29/0473 (2013.01); F04D 29/061 (2013.01); F04D 29/445 (2013.01);
Abstract

A multistage centrifugal pump includes a housing, a rotatable shaft and first and second turbomachinery stages. The first turbomachinery stage includes a first diffuser connected to the housing, a first impeller connected to the rotatable shaft. The second turbomachinery stage includes a second diffuser connected to the housing and a second impeller connected to the rotatable shaft. The multistage centrifugal pump further includes an integral axial load and bearing system that includes at least one diffuser bushing and at least one impeller bearing. The integral axial load and bearing system permits the independent axial movement of the first and second impellers. The integral axial load and bearing system also provides an opposite force to up-thrust and down-thrust produced by the first and second turbomachinery stages.


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