Huntsville Stars Huntsville, AL Jan 2014 to Sep 2014 Stadium Operations AssistantBaker Hill Golf Club Newbury, NH May 2013 to Nov 2013 GroundskeeperEastern Connecticut State University Athletics Willimantic, CT 2012 to 2013 Assistant to Equipment ManagerEastern Connecticut State University Athletics Willimantic, CT 2011 to 2013 Director of Baseball Operations
Education:
Eastern Connecticut State University May 2013 Bachelors in Business Administration
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.