Baker Hughes
Product Design Engineer - Pdc Drill Bits
Baker Hughes Sep 2012 - Nov 2013
Rdd Engineer Iii - Drilling Service Navi Drill Motor
Baker Hughes May 2011 - Oct 2012
Product Design Engineer- Rwd Technology
Spirit Aerosystems May 2006 - May 2011
Design Enginner
Triumph Aerostructures - Vought Aircraft Division Feb 2005 - Jun 2006
Quality Engineer
Education:
University of Houston 2014 - 2016
Master of Science, Masters, Engineering
The University of Texas at Arlington 2001 - 2004
Bachelors, Bachelor of Science, Mechanical Engineering
Florida A&M University
Skills:
Solidworks Nx Unigraphics Product Design Catia Engineering Manufacturing Oil and Gas Microsoft Office Process Engineering Mechanical Engineering Six Sigma Autocad Cad/Cam Enovia Lca Teamcenter Lean Manufacturing
Interests:
Children Economic Empowerment Education Science and Technology Arts and Culture
Prime Time Construction, LLC Hattiesburg, MS Aug 2009 to Dec 2012 Construction LaborerKohler Engines Hattiesburg, MS Oct 2008 to Aug 2009 Maintenance TechnicianFoot Locker, Inc Hattiesburg, MS Jun 2007 to Sep 2008 Sales Associate
Us Patents
Reamers For Earth-Boring Applications Having Increased Stability And Related Methods
- Houston TX, US Mitchell A. Rothe - Montgomery TX, US Kendrick D. McGee - Spring TX, US Mitchell F. Marks - Youngsville LA, US
International Classification:
E21B 10/32 E21B 7/28 E21B 12/00
Abstract:
Reamer for earth-boring applications may include a body having a longitudinal axis and a blade carried by the body. The blade may include at least one cutting element located at a first radial distance from the longitudinal axis and a gage pad located at a second, smaller radial distance from the longitudinal axis. Methods of enlarging pilot holes in earth formations utilizing reamers may involve removing earth material from a sidewall of the pilot hole utilizing at least one cutting element located at a first radial distance from a longitudinal axis of a body of the reamer on a blade of a reamer. The reamer may be stabilized by placing a gage pad located on the blade in sliding contact with a portion of the sidewall of the pilot hole, the gage pad located at a second, smaller radial distance from the longitudinal axis