Jayson Lee Houston

age ~49

from San Antonio, TX

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Also known as:

Jayson L Houston
Jeffrey J Houston
Jason L Houston

Phone and address:: 11511 Buckrail St, San Antonio, TX 78232
2107053740

Connected to:

Jayson Houston Phones & Addresses

11511 Buckrail St, San Antonio, TX 78232 • 2107053740
Blanket, TX
Henrietta, TX
Dallas, TX
Irving, TX
Arlington, TX
Waco, TX
Pecos, NM
Bruni, TX
11511 Buckrail St, San Antonio, TX 78232

Work

Company:

Pratt whitney power systems san antonio
Jan 2002 to Jan 2013
Position:

Senior welder and team leader

Education

School / High School:

Texas State Technical College Waco
1999 to 2001
Specialities:

Applied Science, Welding

Skills

Energy • Power Generation • Power Plants • Gas Turbines • Matlab • Inspection • Engineering • Project Engineering • Welding • Turbines • Aerospace • Mechanical Engineering • Continuous Improvement • Lean Manufacturing • Maintenance

Industries

Oil & Energy

Resumes

Senior Welder And Team Lead

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Location:

San Antonio, TX

Industry:

Oil & Energy

Work:

Pratt Whitney Power Systems San Antonio Jan 2002 - Jan 2013
Senior Welder and Team Leader
Pwps Mitsubishi Heavy Industries Jan 2002 - Jan 2013
Senior Welder and Team Lead
Pratt Daro Jan 2001 - Jan 2002
Special Process Vacuum Furnace Brazing and Welding
Wood Group Hit Jan 2000 - Jan 2001
Senior Welder
Us Navy Jan 1995 - Jan 1999
Hull Maintenance Technician

Education:

Texas State Technical College Waco 1999 - 2001

Skills:

Energy
Power Generation
Power Plants
Gas Turbines
Matlab
Inspection
Engineering
Project Engineering
Welding
Turbines
Aerospace
Mechanical Engineering
Continuous Improvement
Lean Manufacturing
Maintenance

Us Patents

Repair Or Remanufacture Of Blade Platform For A Gas Turbine Engine
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US Patent:

20160067836, Mar 10, 2016
Filed:

Sep 10, 2014
Appl. No.:

14/482273
Inventors:

- Glastonbury CT, US
Jayson Houston - San Antonio TX, US
Mark Towner - Kenedy TX, US
International Classification:

B23P 6/00
F01D 5/14
B23H 1/00
Abstract:

A method of remanufacturing a turbine component includes electrical discharge machining a puck via the turbine component to form an electrical discharged machined puck; and brazing the electrical discharged machined puck to the turbine component.

Repaired Or Remanufactured Blade Platform For A Gas Turbine Engine
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US Patent:

20160069196, Mar 10, 2016
Filed:

Sep 10, 2014
Appl. No.:

14/482303
Inventors:

- Glastonbury CT, US
Jayson Houston - San Antonio TX, US
Mark Towner - Kenedy TX, US
International Classification:

F01D 5/30
Abstract:

A article of manufacture, the article having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE 1, and wherein X and Y are distances in inches which, when connected, define profile sections at each distance Z in inches to form a portion of a rotor blade.