Purdue University 2013 - 2017
Doctorates, Doctor of Philosophy, Geotechnical Engineering, Philosophy
Purdue University 2011 - 2013
Masters, Geotechnical Engineering
Huazhong University of Science and Technology 2007 - 2011
Bachelors, Bachelor of Science, Civil Engineering
Skills:
Finite Element Analysis Matlab Structural Analysis Abaqus Autocad Microsoft Office Numerical Analysis Foundation Design Visual C# Plasticity C
Robert Naumiec - Clifton Park NY Walter Smith - Ballston Spa NY Fei Han - Schenectady NY Eamon Gleeson - Atlanta GA Robert A. Hedeen - Clifton Park NY
Assignee:
General Electric Company - Schenectady NY
International Classification:
G01L 2700
US Classification:
73 166
Abstract:
In one embodiment, the invention is a pressure sensor calibration system comprising a pressure chamber in fluid communication with a pressure sensor to be calibrated, the chamber is pressurized to a static pressure level. An oscillating surface on a wall of the chamber imparts a rapid pressure fluctuation in the static pressure level of the chamber. These rapid pressure fluctuations in a high-static pressure level chamber are used to calibrate the pressure sensor.
Fei Han - Schenectady NY, US Osman Saim Dinc - Troy NY, US Sung Jin Kim - Guilderland NY, US
Assignee:
General Electric Company - Niskayuna NY
International Classification:
F02C 314 F02C 724
US Classification:
60772, 60 3937, 60725
Abstract:
Respective combustion gas streams are generated in a can combustor. The streams are channeled downstream into an annular turbine nozzle. And, dynamic interaction of circumferentially adjacent combustion gas streams is suppressed axially between the cans and the nozzle.
Combustion Chamber Dynamic Pressure Transducer Tee Probe Holder And Related Method
Eamon P. Gleeson - Atlanta GA, US Fei Han - Schenectady NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
G01L 700
US Classification:
73756
Abstract:
A dynamic pressure probe includes a holder body having a first passage therein adapted to receive a pressure signal, a pressure sensor including at least a pressure sensing portion located within a sleeve seated within a pressure sensor housing portion, the sleeve engaged with a wall of the housing portion; the pressure sensor including a diaphragm having one face exposed to a pressure chamber within the sleeve between the pressure sensor and the wall; wherein an aperture in the wall of the housing connects the pressure chamber to the first passage; and wherein the first passage continues axially beyond the aperture in a flow direction an acoustic damping coil wound about a vertical axis.
Combustion Chamber Dynamic Pressure Transducer Tee Probe Holder And Related Method
Eamon P. Gleeson - Atlanta GA, US Fei Han - Schenectady NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
G01L007/00
US Classification:
73756
Abstract:
A dynamic pressure probe for a combustor comprising a holder body having a pressure sensing passage; a pressure sensor and a pressure chamber located in a housing portion arranged substantially perpendicularly to the pressure sensing passage; and wherein the pressure chamber communicates with the pressure sensing passage via a relatively small aperture in a wall separating the pressure chamber from the pressure sensing passage.
Dynamic Pressure Probe Holder And Method Of Obtaining A Dynamic Pressure Signal
Eamon P. Gleeson - Atlanta GA, US Walter John Smith - Baliston Spa NY, US Robert John Naumiec - Clifton Park NY, US Fei Han - Clifton Park NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
G01L007/00
US Classification:
73756, 73 171
Abstract:
A component adapted to transmit a dynamic pressure signal from a high temperature environment to a location where it can be measured without causing significant attenuation of the signal. In particular, the component provides for a dynamic pressure signal transmission in the manner that will not result in the formation of condensation in the measurement system and thus eliminates the need to periodically purge condensate from the system.
Estimating Combustor Flame Temperature Based On Frequency Of Combustor Dynamics Transverse Mode
Warren James Mick - Altamont NY, US Eamon P. Gleeson - Atlanta GA, US Willy Steve Ziminsky - Simpsonville SC, US Aparna Basker - Alpharetta GA, US Fei Han - Clifton Park NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
G01K011/026
US Classification:
374117, 73579, 60803, 60 3924
Abstract:
A method of determining the temperature inside a combustion liner without making a direct measurement of the actual temperature. The technique is based on a measurement of the frequency of one of the transverse acoustic modes occurring inside the combustion chamber. The frequency is determined from the transverse geometric dimensions of the combustion chamber and the speed of sound in the gas inside the combustion chamber. The speed of sound in the gas is known from thermodynamics to be a function of gas temperature and gas properties. Thus, from a measurement of the resonant frequency and knowing the combustor dimensions and gas properties, the temperature can be determined with accuracy.
Method And Apparatus To Detect Onset Of Combustor Hardware Damage
Eamon Patrick Gleeson - Atlanta GA, US Warren James Mick - Altamont NY, US George Edward Williams - Niskayuna NY, US Fei Han - Clifton Park NY, US Shivakumar Srinivasan - Greer SC, US Scott Alan Kopcho - Atlanta GA, US Ilan Leibu - Marietta GA, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02M 35/00
US Classification:
60779, 60 39091
Abstract:
A method for determining when a combustor is experiencing hardware damage includes sensing acoustic vibrations of a plurality of combustor cans, determining a center frequency for each acoustic tone of the sensed acoustic vibrations within a predetermined frequency range, and indicating an alarm when a center frequency of one or more of the combustor cans changes in a different manner compared to a representative center frequency of the plurality of combustor cans.
Method And System For Determining Lean Blow Out Condition For Gas Turbine Combustion Cans
Warren James Mick - Altamont NY, US George Edward Williams - Niskayuna NY, US Fei Han - Clifton Park NY, US Eamon Patrick Gleeson - Atlanta GA, US Shiva Srinivasan - Greer SC, US Scott Alan Kopcho - Atlanta GA, US Ilan Leibu - Marietta GA, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 7/00
US Classification:
60779
Abstract:
A method for determining a lean blow out condition for a combustor. In an exemplary embodiment, the method includes determining acoustical frequency data for the combustor, determining a combustor flame temperature based on the acoustical frequency data, determining an existing fuel/air ratio in the combustor based on the combustor flame temperature, and comparing the existing fuel/ratio to a lean blow out fuel/air ratio. A lean blow out condition for the combustor is indicated when the existing fuel/air ratio is about equal to the lean blow out fuel/air ratio.
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