GoDaddy.com - Gilbert, AZ since Jun 2010
Senior Lead Developer
VickersWeb Jul 2009 - Jun 2010
Sole Proprietor
CrossFit Persevere Feb 2009 - Jun 2010
Trainer
Exploria SPS Jun 2008 - Jul 2009
Software Developer
Exploria Aug 2003 - Jun 2008
Director of Programming
Education:
The University of Connecticut 1995 - 1999
BS, Computer Science and Engineering
Skills:
Php Javascript C# Html Python Software Development Web Services Ios Development Mobile Applications Agile Methodologies Mysql Sql Visual Studio Xml Game Development Objective C Ajax Programming
Thomas E. Vickers - Mesa AZ James A. Sanger - Prescott AZ
Assignee:
Allied-Signal Inc. - Morris Township, Morris County NJ
International Classification:
B23B 100
US Classification:
2988921
Abstract:
A turbine or compressor blade holding fixture and machining method contemplates the subassembly of all the blades upon the rotor of the compressor or turbine. Fixture rings along with radial biasing members in the form of annular o-rings are intersecured to opposite sides of the blades so as to radially position the latter in their normal "running position" while so mounted on the rotor of the wheel. In such condition all of the blades may be simultaneously machined such that the outer tips thereof lie on a true uniform, desired outer diameter to provide subsequently uniform tip clearance to the surrounding shroud when mounted in a gas turbine engine for operation.
Apparatus To Hold Compressor Or Turbine Blade During Manufacture
Thomas E. Vickers - Mesa AZ James A. Sanger - Prescott AZ
Assignee:
AlliedSignal Inc. - Morris Township NJ
International Classification:
B23P 100
US Classification:
269 47
Abstract:
A turbine or compressor blade holding fixture and machining method contemplates the subassembly of all the blades upon the rotor of the compressor or turbine. Fixture rings along with radial biasing members in the form of annular o-rings are intersecured to opposite sides of the blades so as to radially position the latter in their normal "running position" while so mounted on the rotor of the wheel. In such condition all of the blades may be simultaneously machined such that the outer tips thereof lie on a true uniform, desired outer diameter to provide subsequently uniform tip clearance to the surrounding shroud when mounted in a gas turbine engine for operation.