Resumes
Resumes
Peter Sobieski Phones & Addresses
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Baytown, TX
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Leakey, TX
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Damon, TX
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Needville, TX
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330 Bayou View Dr, Seabrook, TX 77586 (281) 326-1037
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El Lago, TX
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Pasadena, TX
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Allen Park, MI
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Houghton, MI
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Richmond, TX
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330 Bayou View Dr, El Lago, TX 77586
Business Records
Name / Title
Company / Classification
Phones & Addresses
TRS SERVICES, LLC
Repair Services · Repair Services, NEC
Repair Services · Repair Services, NEC
2105 Skinner Rd, Houston, TX 77093
2100 Skinner Rd, Houston, TX 77093
(713) 692-2930
2100 Skinner Rd, Houston, TX 77093
(713) 692-2930
TSOLV, LLC
Business Consulting Services
Business Consulting Services
3909 Travis Lk Ct, Pearland, TX 77581
Publications
Us Patents
Gas Turbine Fuel Pilot Nozzle
View pageUS Patent:
20050039460, Feb 24, 2005
Filed:
Aug 20, 2003
Appl. No.:
10/644385
Inventors:
Peter Sobieski - El Lago TX, US
Kelly Smith - Kingwood TX, US
Alan Lovelace - Kingwood TX, US
Hany Rizkalla - Stuart FL, US
Kelly Smith - Kingwood TX, US
Alan Lovelace - Kingwood TX, US
Hany Rizkalla - Stuart FL, US
International Classification:
F02C007/22
US Classification:
060772000, 060740000
Abstract:
A pilot fuel nozzle configuration for use in a combustor is disclosed having a natural frequency outside the range of the operating frequencies of a gas turbine engine. Multiple embodiments are disclosed for the improved pilot fuel nozzle including configurations for newly manufactured nozzles, repair to existing pilot nozzles, as well as multiple natural frequency levels for the improved pilot fuel nozzle. The pilot fuel nozzle comprises an elongated housing, first and second flanges, and a nozzle tip, with the first flange fixed to the elongated housing at a first end and the nozzle tip fixed to the second end, opposite of the first end. The second flange is fixed along the elongated housing and is used for attaching the pilot fuel nozzle to a combustor. The present invention incorporates an increased wall thickness along at least a mid-span portion of the pilot nozzle to increase the stiffness and change the natural frequency.
Gas Turbine Efficiency And Regulation Speed Improvements Using Supplementary Air System Continuous And Storage Systems And Methods Of Using The Same
View pageUS Patent:
20180058326, Mar 1, 2018
Filed:
Oct 26, 2017
Appl. No.:
15/794973
Inventors:
- Jupiter FL, US
Scott Auerbach - Jupiter FL, US
Peter A. Sobieski - Seabrook TX, US
Scott Auerbach - Jupiter FL, US
Peter A. Sobieski - Seabrook TX, US
International Classification:
F02C 7/10
F02C 6/16
F02C 9/16
F02C 7/224
F02C 6/16
F02C 9/16
F02C 7/224
Abstract:
A method of cooling a gas fueled engine driven intercooled air compressor comprises providing the intercooled air compressor, a gearbox, and the gas fueled engine. The method includes flowing a liquid coolant from a liquid coolant supply to each of the gearbox and an intercooler of the intercooled air compressor. The method comprises recombining the liquid coolant after the gearbox and the intercooler. The method includes directing the recombined liquid coolant via multiple paths to cool the gas fueled engine. The method comprises recombining the liquid coolant after the liquid coolant has passed through the multiple paths.
Turbocooled Vane Of A Gas Turbine Engine
View pageUS Patent:
20160230665, Aug 11, 2016
Filed:
Dec 17, 2015
Appl. No.:
14/972403
Inventors:
- Jupiter FL, US
Scott AUERBACH - Jupiter FL, US
Peter A. SOBIESKI - Seabrook TX, US
Scott AUERBACH - Jupiter FL, US
Peter A. SOBIESKI - Seabrook TX, US
International Classification:
F02C 7/18
F01D 25/12
F01D 25/12
Abstract:
The present invention discloses a novel apparatus and methods for augmenting the power of a gas turbine engine, improving gas turbine engine operational flexibility and efficiency, and reducing the response time necessary to meet changing demands of an electrical grid. Improvements in power augmentation and engine operation include systems and methods for providing rapid response given a change in electrical grid.
Gas Turbine Efficiency And Regulation Speed Improvements Using Supplementary Air System Continuous And Storage Systems And Methods Of Using The Same
View pageUS Patent:
20140366547, Dec 18, 2014
Filed:
Jul 11, 2014
Appl. No.:
14/329340
Inventors:
- Jupiter FL, US
Scott Auerbach - Jupiter FL, US
Peter A. Sobieski - Seabrook TX, US
Scott Auerbach - Jupiter FL, US
Peter A. Sobieski - Seabrook TX, US
International Classification:
F02C 7/10
F02C 9/16
F02C 6/16
F02C 9/16
F02C 6/16
US Classification:
60772, 60 39511, 60793
Abstract:
The present invention discloses a novel apparatus and methods for augmenting the power of a gas turbine engine, improving gas turbine engine operation, and reducing the response time necessary to meet changing demands of a power plant. Improvements in power augmentation and engine operation include additional heated compressed air injection, steam injection, water recovery, exhaust tempering, fuel heating, and stored heated air injection.