Resumes
Resumes
Mihir Lal Phones & Addresses
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Greer, SC
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5705 Mimosa Ct, Albuquerque, NM 87111 (505) 332-3087
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150 Oak Ridge Pl, Greenville, SC 29615
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39 Stone Valley Dr, Lilburn, GA 30047 (770) 923-3020
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Norcross, GA
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Doraville, GA
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Nyc, NY
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39 Stone Valley Dr SW, Lilburn, GA 30047 (404) 909-4236
Work
Position:
Production Occupations
Education
Degree:
Associate degree or higher
Publications
Us Patents
Systems And Methods For Modified Wobbe Index Control With Constant Fuel Temperature
View pageUS Patent:
20130008172, Jan 10, 2013
Filed:
Jul 5, 2011
Appl. No.:
13/176017
Inventors:
Dean Matthew Erickson - Greenville SC, US
Brian Gallagher - Greenville SC, US
Mihir Lal - Greenville SC, US
Scott Day - Greenville SC, US
Brian Gallagher - Greenville SC, US
Mihir Lal - Greenville SC, US
Scott Day - Greenville SC, US
Assignee:
GENERAL ELECTRIC COMPANY - Schnectady NY
International Classification:
F02C 7/22
F02C 7/224
F02C 7/224
US Classification:
60776, 60736
Abstract:
The present application provides a gas turbine engine system for combusting a flow of fuel. The gas turbine engine system may include a combustor and a fuel system for providing the flow of fuel to the combustor. The fuel system may include a fuel heat exchanger so as to provide the flow of fuel to the combustor at a substantially constant temperature.
Gas Turbine Components And Methods Of Assembling The Same
View pageUS Patent:
20200165923, May 28, 2020
Filed:
Apr 25, 2017
Appl. No.:
16/608214
Inventors:
- Schenecatdy NY, US
Chuan LIN - Shanghai, CN
Shizhong WANG - Shanghai, CN
Mihir Kumar LAL - Greenville SC, US
Richard Todd EVERHART - Greenville SC, US
Chuan LIN - Shanghai, CN
Shizhong WANG - Shanghai, CN
Mihir Kumar LAL - Greenville SC, US
Richard Todd EVERHART - Greenville SC, US
International Classification:
F01D 5/28
C04B 41/50
C01B 33/20
C09D 5/00
C09D 1/00
C04B 41/52
F01D 25/08
C09D 5/08
C04B 41/87
C04B 41/89
C01G 25/00
C23C 4/11
C23C 4/134
C04B 41/50
C01B 33/20
C09D 5/00
C09D 1/00
C04B 41/52
F01D 25/08
C09D 5/08
C04B 41/87
C04B 41/89
C01G 25/00
C23C 4/11
C23C 4/134
Abstract:
A gas turbine component includes a substrate and a corrosion resistant layer coupled to the substrate. The corrosion resistant layer includes zirconium silicate and is configured to protect the substrate from exposure to a vanadium corrodent.
Model-Less Combustion Dynamics Autotune
View pageUS Patent:
20180149363, May 31, 2018
Filed:
Dec 27, 2016
Appl. No.:
15/391450
Inventors:
- Schenectady NY, US
Mihir Lal - Greenville SC, US
James Harper - Greenville SC, US
Douglas Edward Dean - Greenville SC, US
Abhijit Prabhakar Kulkarni - HITEC City, IN
Mihir Lal - Greenville SC, US
James Harper - Greenville SC, US
Douglas Edward Dean - Greenville SC, US
Abhijit Prabhakar Kulkarni - HITEC City, IN
International Classification:
F23R 3/34
F02C 9/26
F02C 9/28
F02C 9/26
F02C 9/28
Abstract:
This disclosure relates to systems and methods for tuning combustion dynamics in a combustor. In one embodiment of the disclosure, a method includes providing, via at least one sensor, combustion dynamics amplitude data associated with a combustor. Method may allow monitoring, by an equipment controller communicatively coupled to the at least one sensor, the combustion dynamics amplitude data. The method may allow detecting at least one change in acoustic pressure amplitude associated with combustion in the combustor. In response to detecting the change in the acoustic pressure amplitude, the method proceeds with determining a fuel split change to at least two fuel circuits configured to supply fuel to the combustor, and applying the fuel split change to the combustor.