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:
Jan. 09, 2018

Filed:

Dec. 05, 2014
Applicant:

Schlumberger Technology Corporation, Sugar Land, TX (US);

Inventors:

Gary L. Rytlewski, League City, TX (US);

Laure Mandrou, Bellaire, TX (US);

David Allensworth, Pearland, TX (US);

Quangen Du, Fresno, TX (US);

Deepak Dcosta, Houston, TX (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
E21B 33/035 (2006.01); E21B 23/04 (2006.01); E21B 34/16 (2006.01); E21B 41/00 (2006.01); E21B 33/06 (2006.01); E21B 33/064 (2006.01); E21B 34/04 (2006.01); F42D 1/04 (2006.01); E21B 34/00 (2006.01);
U.S. Cl.
CPC ...
E21B 33/0355 (2013.01); E21B 23/04 (2013.01); E21B 33/063 (2013.01); E21B 33/064 (2013.01); E21B 34/04 (2013.01); E21B 34/16 (2013.01); E21B 41/0007 (2013.01); F42D 1/04 (2013.01); E21B 2034/002 (2013.01); E21B 2034/005 (2013.01);
Abstract

Systems and methods for using propellant as a force generator in component actuation are disclosed. One embodiment may take the form of a method including deploying at least one component to a subsea location, controlling operation of the at least one component using a control system, and igniting a propellant. The ignition of the propellant actuates the at least one component. Another embodiment may take the form of a subsea system including a control system, a propellant system in communication with the control system, and a component in communication with the propellant system. The propellant system is ignitable by the control system upon receipt of a ignite signal and upon losing communication with the control system after being placed in an armed state by the control system. The component is actuatable by the propellant system after ignition of the propellant system.


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