Search Results | ASME Digital Collection

Proc. ASME. GT2013, Volume 5A: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Microturbines, Turbochargers, and Small Turbomachines, V05AT20A006, June 3–7, 2013

Paper No: GT2013-95402

DOI: https://doi.org/10.1115/GT2013-95402

View Paper

Topics: Compressors, Flow (Dynamics), Design, Water, Turbines, Cooling, Drops, Evaporation, Gas turbines, Industrial gases

Journal Articles

Effect of Impeller Blade Loading on Compressor Stage Performance in a High Specific Speed Range

Takanori Shibata, Manabu Yagi, Hideo Nishida, Hiromi Kobayashi, Masanori Tanaka

J. Turbomach. July 2012, 134(4): 041012.

DOI: https://doi.org/10.1115/1.4003659

Published Online: July 21, 2011

View Article

Topics: Blades, Compressors, Design, Flow (Dynamics), Impellers, Surges

Proceedings Papers

Optimizing a Suction Channel to Improve Performance of a Centrifugal Compressor Stage

Manabu Yagi, Takanori Shibata, Hideo Nishida, Hiromi Kobayashi, Masanori Tanaka, Kazuyuki Sugimura

Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 2007-2017, June 14–18, 2010

Paper No: GT2010-23019

DOI: https://doi.org/10.1115/GT2010-23019

View Paper

Topics: Compressors, Suction, Design, Flow (Dynamics), Pressure, Computational fluid dynamics, Dimensions, Experimental design, Impellers, Mach number

Proceedings Papers

Effect of Impeller Blade Loading on Compressor Stage Performance in a High Specific Speed Range

Takanori Shibata, Manabu Yagi, Hideo Nishida, Hiromi Kobayashi, Masanori Tanaka

Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 1757-1768, June 14–18, 2010

Paper No: GT2010-22281

DOI: https://doi.org/10.1115/GT2010-22281

View Paper

Topics: Blades, Compressors, Impellers, Surges, Design, Diffusion (Physics), Flow (Dynamics), Mach number, Machinery, Pressure

Journal Articles

Performance Improvement of a Centrifugal Compressor Stage by Increasing Degree of Reaction and Optimizing Blade Loading of a 3D Impeller

Takanori Shibata, Manabu Yagi, Hideo Nishida, Hiromi Kobayashi, Masanori Tanaka

J. Turbomach. April 2011, 133(2): 021004.

DOI: https://doi.org/10.1115/1.4000565

Published Online: October 19, 2010

View Article

Topics: Blades, Compressors, Design, Impellers, Flow (Dynamics)

Proceedings Papers

Performance Improvement of a Centrifugal Compressor Stage by Increasing Degree of Reaction and Optimizing Blade Loading of a 3D-Impeller

Takanori Shibata, Manabu Yagi, Hideo Nishida, Hiromi Kobayashi, Masanori Tanaka

Proc. ASME. GT2009, Volume 7: Turbomachinery, Parts A and B, 1305-1315, June 8–12, 2009

Paper No: GT2009-59588

DOI: https://doi.org/10.1115/GT2009-59588

View Paper

Topics: Blades, Compressors, Impellers, Diffusion (Physics), Computational fluid dynamics, Design, Pressure, Surges, Flow (Dynamics), Mach number

Proceedings Papers

Test Results From the Advanced Humid Air Turbine System Pilot Plant: Part 1—Overall Performance

Shinichi Higuchi, Tomomi Koganezawa, Yasuhiro Horiuchi, Hidefumi Araki, Takanori Shibata, Shinya Marushima

Proc. ASME. GT2008, Volume 2: Controls, Diagnostics and Instrumentation; Cycle Innovations; Electric Power, 691-700, June 9–13, 2008

Paper No: GT2008-51072

DOI: https://doi.org/10.1115/GT2008-51072

View Paper

Topics: Gas turbines, Turbines, Water reuse, Thermal efficiency, Axial flow, Combustion chambers, Compressors, Cycles, Flow (Dynamics), Pressure

Proceedings Papers

Inlet Air Cooling With Overspray Applied to a Two-Stage Centrifugal Compressor

Takanori Shibata, Yasuo Takahashi, Shigeo Hatamiya

Proc. ASME. GT2008, Volume 7: Education; Industrial and Cogeneration; Marine; Oil and Gas Applications, 207-217, June 9–13, 2008

Paper No: GT2008-50893

DOI: https://doi.org/10.1115/GT2008-50893

View Paper

Topics: Compressors, Cooling, Gas turbines

Proceedings Papers

Performance Improvement of Centrifugal Compressor Impellers by Optimizing Blade-Loading Distribution

Manabu Yagi, Tadaharu Kishibe, Takanori Shibata, Hideo Nishida, Hiromi Kobayashi

Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 1639-1648, June 9–13, 2008

Paper No: GT2008-51025

DOI: https://doi.org/10.1115/GT2008-51025

View Paper

Topics: Blades, Compressor impellers, Impellers, Design, Computational fluid dynamics, Flow (Dynamics), Performance characterization, Suction, Testing performance

Proceedings Papers

Development of Elemental Technologies for Advanced Humid Air Turbine System

Hidetoshi Kuroki, Takanori Shibata, Tomomi Koganezawa, Nobuaki Kizuka, Shigeo Hatamiya, Shinya Marushima

Proc. ASME. GT2006, Volume 4: Cycle Innovations; Electric Power; Industrial and Cogeneration; Manufacturing Materials and Metallurgy, 183-189, May 8–11, 2006

Paper No: GT2006-90639

DOI: https://doi.org/10.1115/GT2006-90639

View Paper

Topics: Turbines, Gas turbines, Combustion chambers, Compressors, Cooling, Emissions, Nitrogen oxides, Pressure, Thermal efficiency, Compression

Journal Articles

Development of Elemental Technologies for Advanced Humid Air Turbine System

Hidetoshi Kuroki, Shigeo Hatamiya, Takanori Shibata, Tomomi Koganezawa, Nobuaki Kizuka, Shinya Marushima

J. Eng. Gas Turbines Power. May 2008, 130(3): 031701.

DOI: https://doi.org/10.1115/1.2833490

Published Online: March 26, 2008

View Article

Topics: Compressors, Gas turbines, Turbines, Temperature, Combustion chambers, Cooling

Journal citation

NARROW

Manuscript

Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor

Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor

Improvement of Steam Turbine Stage Efficiency by Controlling Rotor Shroud Leakage Flows—Part II: Effect of Axial Distance Between a Swirl Breaker and a Rotor Shroud on Efficiency Improvement

Improvement of Steam Turbine Stage Efficiency by Controlling Rotor Shroud Leakage Flows—Part I: Design Concept and Typical Performance of a Swirl Breaker

Improvement of Steam Turbine Stage Efficiency by Controlling Rotor Shroud Leakage Flows: Part I — Design Concept and Typical Performance of a Swirl Breaker

Improvement of Steam Turbine Stage Efficiency by Controlling Rotor Shroud Leakage Flows: Part II — Effect of Axial Distance Between a Swirl Breaker and Rotor Shroud on Efficiency Improvement

Starting Characteristic Analysis of a Radial Inflow Turbine for the Regenerative Brayton Cycle

Suppression of Secondary Flows in an Axial Flow Turbine Rotor With a Novel Blade Design Concept

Evaluation of Axial Compressor Characteristics Under Overspray Condition

Effect of Impeller Blade Loading on Compressor Stage Performance in a High Specific Speed Range

Optimizing a Suction Channel to Improve Performance of a Centrifugal Compressor Stage

Effect of Impeller Blade Loading on Compressor Stage Performance in a High Specific Speed Range

Performance Improvement of a Centrifugal Compressor Stage by Increasing Degree of Reaction and Optimizing Blade Loading of a 3D Impeller

Performance Improvement of a Centrifugal Compressor Stage by Increasing Degree of Reaction and Optimizing Blade Loading of a 3D-Impeller

Test Results From the Advanced Humid Air Turbine System Pilot Plant: Part 1—Overall Performance

Inlet Air Cooling With Overspray Applied to a Two-Stage Centrifugal Compressor

Performance Improvement of Centrifugal Compressor Impellers by Optimizing Blade-Loading Distribution

Development of Elemental Technologies for Advanced Humid Air Turbine System

Development of Elemental Technologies for Advanced Humid Air Turbine System

Journals

Conference Proceedings

eBooks

Resources

Opportunities

Journals

Conference Proceedings

eBooks

Resources

Opportunities

This Feature Is Available To Subscribers Only