BRIAN A OWEN
Medical Practice in Orlando, FL
License number
Florida 22453
Issued Date
May 24, 1983
Effective Date
Oct 4, 1996
Expiration Date
Jun 30, 1988
Category
Health Care
Type
Clinical Laboratory Personnel
Address
Address
Derek And Assoc , Path Labs, Orlando, FL 32809
Professional information
Prog/Analysis Associate At Convergys
Position:
Prog/Analysis Associate at Convergys
Location:
Orlando, Florida Area
Industry:
Information Technology and Services
Work:
Convergys
since May 2009
-
Prog/Analysis Associate
Convergys
Oct 2007 - May 2009
-
Answer Station Admin
Convergys
Sep 2006 - Oct 2007
-
ID Administrator
Convergys
Aug 2003 - Sep 2006
-
Team Leader
Convergys
Nov 1997 - Aug 2003
-
Customer Service Representative
Cooling Scheme For Turbine Hot Parts
US Patent:
6105363, Aug 22, 2000
Filed:
Apr 27, 1998
Appl. No.:
9/067593
Inventors:
Kent Goran Hultgren - Winter Park FL
Brian Charles Owen - Orlando FL
Steven Wayne Dowman - Orlando FL
Raymond Scott Nordlund - Orlando FL
Ricky Lee Smith - Oviedo FL
Brian Charles Owen - Orlando FL
Steven Wayne Dowman - Orlando FL
Raymond Scott Nordlund - Orlando FL
Ricky Lee Smith - Oviedo FL
Assignee:
Siemens Westinghouse Power Corporation - Orlando FL
International Classification:
F02C 300
US Classification:
60 3975
Abstract:
A closed-loop cooling scheme for cooling stationary combustion turbine components, such as vanes, ring segments and transitions, is provided. The cooling scheme comprises: (1) an annular coolant inlet chamber, situated between the cylinder and blade ring of a turbine, for housing coolant before being distributed to the turbine components; (2) an annular coolant exhaust chamber, situated between the cylinder and the blade ring and proximate the annular coolant inlet chamber, for collecting coolant exhaust from the turbine components; (3) a coolant inlet conduit for supplying the coolant to said coolant inlet chamber; (4) a coolant exhaust conduit for directing coolant from said coolant exhaust chamber; and (5) a piping arrangement for distributing the coolant to and directing coolant exhaust from the turbine components. In preferred embodiments of the invention, the cooling scheme further comprises static seals for sealing the blade ring to the cylinder and flexible joints for attaching the blade ring to the turbine components.