TODD STANLEY NEMEC
Pilots at Meadowbrook, Guilderland, NY

License number
New York A2681740
Issued Date
Oct 2016
Expiration Date
Oct 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
23 Meadowbrook Ct APT D, Guilderland, NY 12084

Professional information

Todd Nemec Photo 1

Methods And Systems For Performing Integrated Analyses, Such As Integrated Analyses For Gas Turbine Power Plants

US Patent:
2003008, May 1, 2003
Filed:
Oct 30, 2001
Appl. No.:
10/020588
Inventors:
Cedric Chow - Rego Park NY, US
Kelly Crotty - Greenville SC, US
John Drohan - Greer SC, US
James Fehlberg - Simpsonville SC, US
Arlie Martin - Simpsonville SC, US
Thad Morton - Greenville SC, US
Todd Nemec - Guilderland NY, US
David Pesetsky - Greenville SC, US
Robert Priestley - Ballston Lake NY, US
Ming Zhou - Reading MA, US
International Classification:
G01B003/44, G01B003/52, G06F019/00
US Classification:
702/034000
Abstract:
Automated systems for performing integrated analyses. In one embodiment, an integrated analysis system can be used to comprehensively evaluate the effects of changes in hardware configuration or operating conditions on gas turbine power plant performance and economics. The system evaluates these changes by concurrently analyzing a number of different aspects of the power plant while ensuring that the data used in each of the different analyses is consistent. These analyses can include turbine and compressor aerodynamic analysis, cooling and leakage flow analysis, heat transfer analysis, part life analysis, heat balance analysis, cost analysis and overall power plant performance and economic analysis.


Todd Nemec Photo 2

Method And System To Facilitate Combined Cycle Working Fluid Modification And Combustion Thereof

US Patent:
2009019, Aug 6, 2009
Filed:
Feb 4, 2008
Appl. No.:
12/025437
Inventors:
Mark Stewart Schroder - Greenville SC, US
Mark Allan Hadley - Greenville SC, US
Richard Anthony DePuy - Burnt Hills NY, US
Todd Stanley Nemec - Guilderland NY, US
International Classification:
F02C 3/22, B23P 11/00, F02C 6/00
US Classification:
60726, 29700, 60 3948, 60 39182
Abstract:
A method of assembling a combustion system includes providing a gas turbine engine that includes a gas turbine section coupled downstream from a combustion chamber and coupling a source of oxygen to the gas turbine engine such that a stream of oxygen discharged from the source facilitates displacing nitrogen in the working fluid of the gas turbine engine and facilitates decreasing emissions generated within the gas turbine engine.