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:
Sep. 28, 2021

Filed:

Mar. 13, 2018
Applicant:

Halliburton Energy Services, Inc., Houston, TX (US);

Inventors:

Donn J. Brown, Broken Arrow, OK (US);

Randy S. Roberts, Tulsa, OK (US);

Thomas John Gottschalk, Houston, TX (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
E21B 43/38 (2006.01); E21B 43/12 (2006.01); F04D 13/10 (2006.01); F04D 9/00 (2006.01); F04D 7/04 (2006.01); F04D 13/08 (2006.01);
U.S. Cl.
CPC ...
E21B 43/38 (2013.01); E21B 43/128 (2013.01); F04D 7/04 (2013.01); F04D 9/003 (2013.01); F04D 13/08 (2013.01); F04D 13/10 (2013.01);
Abstract

An electric submersible pump (ESP) gas separator is described. An ESP gas separator includes a propeller upstream of a fluid entrance to a crossover, the crossover including a production pathway and a vent pathway, and the propeller including a plurality of blades comprising washout twist, wherein gas rich fluid of multi-phase fluid traveling through the gas separator flows through the propeller and into the vent pathway, and gas poor fluid of the multi-phase fluid flows around the propeller and then through the production pathway. An ESP assembly includes a gas separator between a centrifugal pump and an induction motor, the gas separator serving as an intake for fluid into the centrifugal pump and including a propeller in a separation chamber, the propeller comprising a plurality of blades, each blade having a pitch that increases in coarseness from a hub towards a shroud of the propeller.


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