Kenneth Winston Beebe - Galway NY Leslie Boyd Keeling - Niskayuna NY
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 726
US Classification:
60777, 60723, 60751
Abstract:
A device for conditioning the flow of hot gas in a catalytic combustor in preparation for entry into a catalytic reactor. The device is composed of at least one and most preferably two or more disks that are secured to a shroud so as to be disposed in a plane generally perpendicular to the hot gas flow direction. Each disk is composed of a plurality of small cells oriented so that flow channels therethrough are axially disposed. The cells linearize the gas flow and exert drag on the gas flow therethrough. This generates a static pressure gradient in the flow fields upstream and downstream of the honeycomb disk, which in turn causes flow adjustments so as to produce a more uniform axial flow field. This results in a more uniform fuel/air concentration distribution and velocity distribution at the catalytic reactor inlet.
Resumes
Turbofan Turbojet Fan And Compressor Module Leader
GE Aviation - Lynn Ma since Jan 2012
Egineering Technology Team Leader
The Timken Company May 2007 - Jan 2012
Group Leader Product Design Engineering
General Electric Mar 2004 - Apr 2007
Lead Mechanical Design Engineer - Steam Turbine
GE Energy 2001 - 2004
Lead mechanical design engineer - Generator Rotor Design
General Electric 1992 - 2001
Mechanical Design Engineer - Gas Turbine Combustion
Education:
Union College 1995 - 1999
BSE, Civil /Mechanical Engineering
Northeastern University 2010
MS, Project Mnagement