Mark S Stablein, 70Erie, PA
Mark Stablein Phones & Addresses
Erie, PA
Lawrence Park, PA
North East, PA
Waterford, PA
Mentions for Mark S Stablein
Publications & IP owners
Us Patents
Method And System For Controlling Engine Performance
US Patent:
2011030, Dec 15, 2011
Filed:
Jun 15, 2010
Appl. No.:
12/816063
Inventors:
Kendall Roger Swenson - Erie PA, US
Roy Primus - Niskayuna NY, US
Lukas Johnson - Erie PA, US
Mark Stablein - Erie PA, US
Kevin Paul Bailey - Grove City PA, US
John Dowell - Grove City PA, US
Frederick Thwaites - Erie PA, US
Jonathan Nagurney - Erie PA, US
Roy Primus - Niskayuna NY, US
Lukas Johnson - Erie PA, US
Mark Stablein - Erie PA, US
Kevin Paul Bailey - Grove City PA, US
John Dowell - Grove City PA, US
Frederick Thwaites - Erie PA, US
Jonathan Nagurney - Erie PA, US
International Classification:
F02D 41/00
F02B 47/08
F02M 25/07
G06F 7/00
F02B 33/40
F02D 23/00
F02B 47/08
F02M 25/07
G06F 7/00
F02B 33/40
F02D 23/00
US Classification:
701 21, 606051, 60611, 606052, 701102
Abstract:
Methods and systems are provided for operating a vehicle including an engine comprising a turbocharger including a compressor and a turbine. The engine further includes a bypass path configured to selectively route gas from downstream of the compressor to upstream of the turbine. In one embodiment, the method comprises selectively increasing gas flow to the engine by adjusting gas flow through the bypass path from downstream of the compressor to upstream of the turbine. In this manner, the performance of the engine may be adjusted for various operating conditions.
Fragment Containment Assembly And Method For Adding A Fragment Containment Assembly To A Turbine
US Patent:
2012003, Feb 16, 2012
Filed:
Aug 12, 2010
Appl. No.:
12/855317
Inventors:
Kendall SWENSON - Erie PA, US
Mark Stablein - Lawrence Park PA, US
Lukas Johnson - Erie PA, US
Mark Stablein - Lawrence Park PA, US
Lukas Johnson - Erie PA, US
International Classification:
F01D 21/00
B23P 19/00
B23P 19/00
US Classification:
415 9, 29700
Abstract:
A fragment containment assembly for a turbine is provided. The fragment containment assembly includes a plurality of bands disposed around a shroud of the turbine and positioned such that the shroud is disposed between blades of the turbine and the bands along radial directions outwardly extending from a shaft of the turbine. The bands include a material having a first modulus of toughness parameter that is greater than a second modulus of toughness parameter of the shroud at temperatures of at least 260 degrees Celsius. The bands are disposed around the shroud to prevent debris of the turbine from being released outside of the bands along the radial directions caused by failure of the turbine.
Method And System For Improving Efficiency Of Multistage Turbocharger
US Patent:
2012022, Sep 13, 2012
Filed:
Mar 9, 2011
Appl. No.:
13/043826
Inventors:
Rodrigo Rodriguez Erdmenger - Munich, DE
Alberto Scotti Del Greco - Figline Valdarno, IT
Vittorio Michelassi - Munich, DE
Kendall Roger Swenson - Erie PA, US
Daniel Edward Loringer - Erie PA, US
Mark Thomas Stablein - Erie PA, US
Lukas William Johnson - Erie PA, US
Alberto Scotti Del Greco - Figline Valdarno, IT
Vittorio Michelassi - Munich, DE
Kendall Roger Swenson - Erie PA, US
Daniel Edward Loringer - Erie PA, US
Mark Thomas Stablein - Erie PA, US
Lukas William Johnson - Erie PA, US
Assignee:
GENERAL ELECTRIC COMPANY - SCHENECTADY NY
International Classification:
F02C 6/12
US Classification:
60612
Abstract:
A turbine system for a multistage turbocharger and a method for utilizing the same are disclosed. The turbine system includes a high pressure turbine having an inlet for receiving a flow of fluid, and an outlet for passing the flow on extraction of work from the high pressure turbine. The system further includes a low pressure turbine, having an inlet for receiving a flow of fluid from the high pressure turbine. A diffuser connects the outlet of the high pressure turbine and the inlet of the low pressure turbine. The system also includes a bypass channel for bypassing a portion of the flow around the high pressure turbine, from upstream of the high pressure turbine to downstream of the high pressure turbine. The system includes an injector to input the bypass flow in the diffuser in a manner to reduce flow separation in the diffuser.
Systems And Methods For An Engine With A Two-Stage Turbocharger
US Patent:
2013003, Feb 7, 2013
Filed:
Aug 3, 2011
Appl. No.:
13/197108
Inventors:
Rodrigo Rodriguez Erdmenger - Garching, DE
Douglas C. Hofer - Niskayuna NY, US
Jassin Fritz - Garching, DE
Alberto Scotti Del Greco - Florence, IT
Georgios Bikas - Garching, DE
Mark Stablein - Lawrence Park PA, US
Sebastian Walter Freund - Garching, DE
Vittorio Michelassi - Florence, IT
Douglas C. Hofer - Niskayuna NY, US
Jassin Fritz - Garching, DE
Alberto Scotti Del Greco - Florence, IT
Georgios Bikas - Garching, DE
Mark Stablein - Lawrence Park PA, US
Sebastian Walter Freund - Garching, DE
Vittorio Michelassi - Florence, IT
International Classification:
F02C 6/12
US Classification:
606051
Abstract:
Various methods and systems are provided for an engine. In one example, the system includes a two-stage turbocharger which has first turbocharger with a first turbine and a first compressor and a second turbocharger with a second turbine and a second compressor, where the first turbine and the second turbine are arranged in parallel and the first compressor and the second compressor are arranged in series. The system may include a duct coupling turbine inlets of the first and second turbine, and a valve coupled between the duct and the inlet of the first turbine to throttle flow to first turbine.
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