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:
Jun. 30, 2020

Filed:

Oct. 28, 2015
Applicant:

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

Inventors:

Larry DeLynn Chambers, Kingwood, TX (US);

Joe Marzouk, Conroe, TX (US);

Olumide O. Odegbami, Houston, TX (US);

Mukul M. Agnihotri, Spring, TX (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
E21B 4/02 (2006.01); H02K 7/18 (2006.01); F03B 13/02 (2006.01); F01D 11/20 (2006.01); E21B 41/00 (2006.01); F04D 29/62 (2006.01); F01D 11/22 (2006.01); F01D 11/24 (2006.01);
U.S. Cl.
CPC ...
E21B 4/02 (2013.01); F03B 13/02 (2013.01); H02K 7/1823 (2013.01); E21B 41/0085 (2013.01); F01D 11/20 (2013.01); F01D 11/22 (2013.01); F01D 11/24 (2013.01); F04D 29/622 (2013.01); F05B 2250/02 (2013.01); F05B 2270/1033 (2013.01); F05D 2240/11 (2013.01);
Abstract

A method and apparatus according to which an output of a power generation system is controlled. In one embodiment, the power generation system includes a turbine and a feedback control system. The turbine includes a rotor to which a first portion of a power fluid is communicated, the first portion imparting torque to the rotor; a shaft to which the rotor is connected; a shroud extending circumferentially about the rotor and the shaft; and a bypass gap between the rotor and the shroud, through which a second portion of the power fluid is communicated. The feedback control system axially displaces the shroud relative to the rotor, thereby adjusting the size of the bypass gap and, consequently, the ratio of the first portion relative to the second portion.


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