Welcome to Turbo Expo 2012! - Events

More documents

Recommendations

Info

FOR A COMPLETE LISTING OF JOINT SESSIONS, SEE PAGE 32 ASME TURBO EXPO 2012 FINAL PROGRAM 43 MONDAY, JUNE 11: 2:30 p.m. - 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Microturbines, Turbochargers, & Small Turbomachines • Paper Session Room BV1 • MB-20-2 ROTORdYNAMICS & BEARINGS Session Chair: dan lubell, Capstone Turbine, Chatsworth, CA, USA • Session Co-Chair: Keun Ryu, BorgWarner Turbo Systems, Arden, NC, USA Rotordynamics of a 105,000 rpm Oil-Free Compressor-Expander for Subsurface Natural Gas Compression and Reinjection GT2012-69119 Aaron M. Rimpel, Jeff Moore, Southwest Research Institute, San Antonio, TX, USA, Joseph S. Grieco, Perry C. Shy, Halliburton Energy Services, Carrollton, TX, USA, John M. Klein, Rotor-Therm, Anchorage, AK, USA, Jerry L. Brady, BP Exploration Alaska, Anchorage, AK, USA Non-deterministic Methodologies for Uncertainty quantification in Turbomachinery CFd Charles Hirsch, NUMECA International, Brussels Characterization of Stiffness and damping In Textured Sector-Pad Micro- Thrust Bearings Using Computational Fluid dynamics GT2012-69403 Christos I., Papadopoulos, Lambros Kaiktsis, National Technical University of Athens, Dept. of Naval Architecture & Marine Engineering, Athens, Greece, Pantelis Nikolakopoulos, University of Patras, Patras, Rio, Greece Management and Minimization of Errors and Uncertainties in Numerical Aerodynamics - The MUNA Project Bernhard Eisfeld, Deutsches Zentrum fuer Luft und Raumfahrt e.V., Braunschweig development and Experimental Performance verification of a Magneto-Aerostatic Bearing for Cartridge of dental Handpieces GT2012-68538 Guan-Chung Ting, Kuang-Yuh Huang, Keng-Ning Chang, National Taiwan University, Taipei City,Taiwan Quantification and management of uncertainty and variability in the industrial design context Marcus Meyer, Rolls-Royce Deutschland Ltd & Co KG, Blankenfelde-Mahlow OT Dahlewitz, Brandenburg, Germany Power loss in High-Speed Micro Turbomachinery - An Experimental Study GT2012-69558 James, F. Walton, Mohawk Innovative Technology, Inc., Albany, NY, USA, Hooshang Heshmat, Mohawk Innovative Technology, Inc., Albnay, NY, USA, Michael Tomaszewski, Mohawk Innovative Technology, Inc., Albany, NY, USA Reducing Uncertainty in Aeroelastic Models with Experimental data Richard Dwight, TU Delft, Delft, Netherlands A Tribological Study of Partialarc Bearings with Egg-shaped Surface Texture for Microturbine Applications GT2012-69383 Dimitrios Bompos, Pantelis Nikolakopoulos, University of Patras, Patras, Rio,Greece, Christos I., Papadopoulos, Lambros Kaiktsis, National Technical University of Athens, Dept. of Naval Architecture & Marine Engineering, Athens,Greece COMMITTEE: Structures & dynamics: Probabilistic Methods • Panel Session Room B5-M4 • MB-26-3 PROBABIlISTIC METHOdS FOR CFd APPlICATIONS Session Chair: Alexander lange, TU Dresden, Dresden, Germany • Session Co-Chair: Philipp Hecker, Alstom Switzerland, Baden, Switzerland Experiments on vibrating Contact Friction and Model validation Muzio Gola, Politecnico di Torino, Torino, Italy Practical Applications of Friction damping in Gas Turbines Robert Elliott, Rolls-Royce plc, Derby, UK Experimental Studies Of damping Phenomena For Turbine Blades: Friction Dr. Lars Panning-von Scheidt, Leibniz Universität Hannover, Hannover, Germany Alstom GT Experiences with Friction damping Technology Jaroslaw Szwedowicz, ALSTOM Power / Thermal Services, Baden, AG, Switzerland Efficient robustness estimation and reliability analysis using surrogate models Dirk Roos, Niederrhein University of Applied Sciences, Krefeld, Germany COMMITTEE: Structures & dynamics: damping Technologies • Panel Session Room B5-M2 • MB-30-1 FRICTION dAMPING TECHNOlOGY: PRESENT ANd FUTURE Session Chair: dr Evgeny Petrov, The University of Sussex, Brighton, UK GE Successes and Challenges with Friction devices Sergio Filippi, GE Aviation, Cincinnati, OH, USA Friction/Flutter Interaction of Shrouded Blades Jerry H. Griffin, Blade Diagnostics Corporation, Pittsburgh, PA, USA
Look for this Symbol R for Gas Turbine User Related Sessions ASME TURBO EXPO 2012 FINAL PROGRAM 44 MONDAY, JUNE 11: 2:30 p.m. - 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Supercritical CO2 Power Cycles • Paper Session Room B3-M4 • MB-32-1 SUPERCRITICAl CO2 POwER CYClES I Session Chair: Klaus Brun, SWRI, San Antonio, USA • Session Co-Chair: Kenneth Kimball, Knolls Atomic Power Laboratory, Schenectady, NY, USA Supercritical Carbon dioxide Brayton Power Cycle development Overview GT2012-68204 Kenneth Kimball, Knolls Atomic Power Laboratory, Schenectady, NY, USA, Eric Clementoni, Bettis Atomic Power Laboratory, West Mifflin, PA, USA Robust design Strategies for Heavy duty Axial Compressor Inlet Strut GT2012-69015 Marco Cioffi, Ansaldo Energia, Genova, Italy, Enrico Puppo, andrea silingardi, Mauro Macciò, Ansaldo Energia, GENOA, Italy Performance Characteristics of an Operating Supercritical CO2 Brayton Cycle GT2012-68415 Thomas Conboy, Jim Pasch, Darryn Fleming, Gary Rochau, Sandia National Labs, Albuquerque, NM, USA, Steven Wright, Critical Energy LLC (Sandia Labs, Retired), Albuquerque, NM, USA, Robert Fuller, Barber- Nichols Inc, Arvada, CO, USA Numerical and Experimental Investigations of Steady and Unsteady Characteristics of a Counter Rotating Fan Model with Thickened Blades of working wheel GT2012-69734 Victor Mileshin, Igor Brailko, Alexandr Stepanov, Vladimir Korzhnev, Central Institute of Aviation Motors, Moscow, Russia Supercritical Carbon dioxide Power Cycle Configuration for Use in Concentrating Solar Power Systems GT2012-68932 Criag turchi, NREL, Golden, USA, Zhiwen Ma, National Renewable Energy Laboratory, Golden, CO, USA, John Dyreby, University of Wisconsin, Madison, WI, USA Effect of Speed Ratio and Axial Spacing variations on the Performance of a High Aspect ratio, low Speed Contra-rotating Fan GT2012-68383 Chetan Mistry, Indian Institute of Technology Bombay, Mumbai, Maharashtra, India, Pradeep AM, Indian Institute of Technology, Bombay, Mumbai, Maharashtra, India The Texas Cryogenic Oxy-Fuel Cycle (TCO): A Novel Approach to Power Generation with CO2 Options GT2012-69930 Jason Gatewood, Jeff Moore, Klaus Brun, Vishwas Iyengar, Southwest Research Institute, San Antonio, TX, USA, Marybeth Nored, Apache Corporation, Houston, TX, USA COMMITTEE: Turbomachinery: Axial Flow Fan & Compressor Aerodynamics • Paper Session Room B3-M6 • MB-33-2 dESIGN, ANAlYSIS, ANd TEST II Session Chair: Alessandro Corsini, Sapienza University of Rome, Rome, Italy Effects of low Reynolds Number on Flow Characteristics of a Transonic Compressor GT2012-68273 Hui Du, AVIC Commercial Aircraft Engine CO., LTD., Shanghai, Shanghai, China, Shengfeng Zhao, Jianbo Gong, Xingen Lu, Junqiang Zhu, Chinese Academy of Sciences, Beijing, Beijing, China The Effect of Reynolds Number on A Transonic Swept Fan OGv in a Small Turbofan Engine GT2012-69956 Toyotaka Sonoda, Toshiyuki Arima, Honda R&D Co., Ltd, Fundamental Technology Research Center, wakoshi, Japan, Giles Endicott, Markus Olhofer, Bernhard Sendhoff, Honda Reseach Institute, Offenbach, Germany An Experimental Study of loss Sources in a Fan Operating with Continuous Inlet Stagnation Pressure distortion GT2012-68888 Cesare Hall, Ewan J. Gunn, University of Cambridge, Cambridge, UK, Sarah E. Tooze, Rolls-Royce plc., Derby, UK, Yann Colin, Airbus S.A.S., Toulouse, France Angle-of-Attack Effects on Counter-Rotating Propellers at Take-Off GT2012-69901 Tobias brandvik, Cesare Hall, University of Cambridge, Cambridge, UK, Anthony Parry, Rolls-Royce, Derby, UK Experimental Investigation on the Performance of a Compressor Airfoil in droplet laden Flow GT2012-69464 Birger Ober, Helmut-Schmidt- University, Hamburg, Hamburg, Germany, Franz Joos, Helmut- Schmidt-University/ University of the Federal Armed Forces Hamburg, Hamburg, Germany The Effect of Tip Clearance on the Performance of Contra-Rotating Compressor GT2012-68801 Limin Gao, xiaojun li, Xudong Feng, Bo Liu, Northwestern Polytechnical University, XI’AN, Shaanxi, China Reverse Flow Turbine-like Operation of an Axial Flow Compressor GT2012-68783 Andrew Gill, T.W Von Backström, T.M. Harms, Department of Mechanical and Mechatronic engineering, University of Stellenbosch, Stellenbosch, Western cape, South Africa The Effect of Speed Ratio on the First Rotating Stall Stage in Contra-Rotating Compressor GT2012-68802 Limin Gao, xiaojun li, Jian Xie, Bo Liu, Northwestern Polytechnical University, XI’AN, Shaanxi, China COMMITTEE: Turbomachinery: Axial Flow Fan & Compressor Aerodynamics • Paper Session Room B3-M8 • MB-33-11 COMPRESSOR OPERATION Session Chair: Aspi wadia • Session Co-Chair: Rudi Selmeier, GE Global Research, Garching near Munich, Germany
Page 3: Dear Turbo Expo 2012 Participants:
Page 6 and 7: 4 grand Opening Featuring Keynote S
Page 8 and 9: 6 Networking Events grand Opening M
Page 10 and 11: 8 Participating Organizations Turbo
Page 12 and 13: 10 guest Tours guest Hospitality Su
Page 14 and 15: 12 Facility Tours Take advantage of
Page 16 and 17: 14 Session Participant Information
Page 18 and 19: 16 Exhibit Hall Floor Plan Subject
Page 20 and 21: PLEASE REFER TO ONLINE EXHIBITOR DI
Page 23 and 24: your career... your thirst for know
Page 25 and 26: 30 Technical Conference The Technic
Page 27 and 28: 32 Joint Sessions Coal, Biomass & A
Page 29 and 30: Look for this Symbol R for Gas Turb
Page 37: Look for this Symbol R for Gas Turb
Page 89 and 90:
Look for this Symbol R for Gas Turb
Page 91 and 92:
Page 93 and 94:
Page 95 and 96:
Page 97 and 98:
Page 99 and 100:
Page 101 and 102:
Page 103 and 104:
Page 105 and 106:
Page 107 and 108:
Page 109 and 110:
Page 111 and 112:
Page 113 and 114:
Page 115 and 116:
Page 117 and 118:
Page 119 and 120:
Page 121 and 122:
Page 123 and 124:
128 Gas Turbine User Session Listin
Page 125 and 126:
130 Exhibit Advisory Committee MISS
Page 127 and 128:
132 Technical Committee Officers AI
Page 129 and 130:
134 IGTI Board ASME Vice President,
Page 131 and 132:
A. Gomes, R. ......................
Page 133 and 134:
Hartey, M. ........................
Page 135 and 136:
Peschiulli, A. ....................
Page 137 and 138:
142 Technical Committee Meeting Sch
Page 139:
Saturday, June 9 144 Turbo Expo 201
show all

Welcome to Turbo Expo 2012! - Events

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?