- Schenectady NY, US Nirm Velumylum Nirmalan - Liberty Township OH, US Mohamed Sakami - West Chester OH, US Thomas Charles Adcock - Glenville NY, US Jeffrey Jay Porubcan - Averill Park NY, US James William Sears - Niskayuna NY, US Naveenan Thiagarajan - Clifton Park NY, US Bernard Bewlay - Niskayuna NY, US Jason Edward Dees - Niskayuna NY, US James DeLancey - Corinth NY, US
International Classification:
G01K 13/02 G01F 15/04 G01K 1/12 G01K 1/14
Abstract:
An imaging system includes a sight tube extending along a longitudinal axis of the imaging system and configured to extend through an access port. The sight tube includes a wall extending about the longitudinal axis and defining a cavity. The imaging system also includes a plurality of cooling channels extending through the sight tube. The plurality of cooling channels are configured to direct cooling fluid through the sight tube for cooling the imaging system. The plurality of cooling channels are formed in the sight tube such that at least one cooling channel of the plurality of cooling channels extends in a direction oblique to the longitudinal axis.
System And Method For Disposable Infrared Imaging System
- Schenectady NY, US Naveenan Thiagarajan - Latham NY, US Todd Garrett Wetzel - Niskayuna NY, US Jason Edward Dees - Ballston Lake NY, US Bernard Patrick Bewlay - Niskayuna NY, US
International Classification:
G01J 1/02 G01N 21/35 F02C 7/12
Abstract:
An infrared imaging device includes a plurality of electronic components, a phase change material, and a heat transfer structure. The plurality of electronic components is configured to collect data and have a predetermined temperature parameter. The plurality of electronic components is disposed within the phase change material. The phase change material has a first material phase and a second material phase. The phase change material has a first material phase and a second material phase. The phase change material is configured to absorb heat through changing from the first material phase to the second material phase. The heat transfer structure is disposed within the phase change material. The heat transfer structure is configured to conduct heat within the phase change material. The phase change material and the heat transfer structure are further configured to regulate a temperature of the electronic components below the predetermined temperature parameter.
System And Method For Monitoring Of Gas Turbine Components With Infrared System
An infrared imaging device includes a case, a plurality of electronic components, and a heat transfer structure. The plurality of electronic components is configured to collect data and have a predetermined temperature parameter. The plurality of electronic components is disposed within the case. The heat transfer structure is disposed within the case. The heat transfer structure is configured to conduct heat away from the plurality of electronic components. The heat transfer structure is further configured to regulate a temperature of the electronic components below the predetermined temperature parameter.
- Schenectady NY, US Todd Garrett Wetzel - Rexford NY, US Jason Edward Dees - Ballston Lake NY, US
International Classification:
F02C 6/00 F01D 17/02
Abstract:
A turbine engine includes a compressor section, a combustor section fluidly coupled to the compressor section, a turbine section fluidly coupled to the combustor section, and a drive shaft coupled to the turbine section and the compressor section. The turbine engine also includes a plurality of internal components coupled to one of the compressor section, the combustor section, the turbine section, and the drive shaft. The turbine engine also includes at least one micro infrared sensor coupled to at least one of the plurality of internal components. The micro infrared sensor is configured to detect a surface temperature of the plurality of internal components.
Name / Title
Company / Classification
Phones & Addresses
Jason Dees Managing
REVEL & REVERE LLC
240 E Renfro St STE 205, Burleson, TX 76028 12301 Research Park Blvd, Austin, TX 78759
Ge Aviation
Sub Section Manager - Fleet Modeling
Ge Global Research Aug 2018 - Aug 2018
Aviation Product Cost Technology Leader
Ge Global Research Aug 2014 - Aug 2017
Manager - Turbine Gas Path Lab
Ge Global Research Aug 2010 - Aug 2014
Mechanical Engineer
Education:
The University of Texas at Austin 2019 - 2019
Master of Science, Doctorates, Masters, Doctor of Philosophy
The University of Texas at Austin 2004 - 2010
Master of Science, Doctorates, Masters, Doctor of Philosophy, Mechanical Engineering
Louisiana Tech University 1999 - 2003
Bachelors, Bachelor of Science, Mechanical Engineering
Skills:
Heat Transfer Fluid Mechanics Mechanical Engineering R&D Thermodynamics Matlab Gas Turbines Cfd Ansys Aerodynamics Fluid Dynamics Thermal Project Management Labview Experimental Design Turbomachinery Ir Thermography Research and Development Simulations Convective Heat Transfer Engineering Management Uncertainty