Microturbines have been developed as compact gas turbines to be applied in the regenerative Brayton cycle. A typical microturbine is composed of a centrifugal compressor and a radial inflow turbine. As such, the microturbine has a starting characteristic peculiar to radial inflow turbines. An idling state known as the windage point for mass flow rate can be formed because of improper inlet flow conditions for turbine expansion flow. The present study looked at the relationships between the radius ratio of the radial inflow turbine to the centrifugal compressor and the starting characteristic and at the effects of turbine inlet flow conditions on the starting characteristic. Fundamental equations for the relationships between the radius ratio and the starting characteristic were obtained. Effectiveness of the equations was compared with experiment results obtained with a 150 kW class prototype microturbine.
Skip Nav Destination
Article navigation
June 2015
Research-Article
Starting Characteristic Analysis of a Radial Inflow Turbine for the Regenerative Brayton Cycle
Susumu Nakano,
Susumu Nakano
1
Hitachi Research Laboratory,
e-mail: susumu_nakano@mhps.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: susumu_nakano@mhps.com
1Present address: Research & Development Center, Mitsubishi Hitachi Power Systems, LTD., 1-1 Saiwai-cho, 3-chome, Hitachi, Ibaraki 317-0073, Japan.
Search for other works by this author on:
Tadaharu Kishibe,
Tadaharu Kishibe
1
Hitachi Research Laboratory,
e-mail: tadaharu_kishibe@mhps.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: tadaharu_kishibe@mhps.com
1Present address: Research & Development Center, Mitsubishi Hitachi Power Systems, LTD., 1-1 Saiwai-cho, 3-chome, Hitachi, Ibaraki 317-0073, Japan.
Search for other works by this author on:
Manabu Yagi,
Manabu Yagi
Infrastructure Systems Company,
e-mail: manabu.yagi.cb@hitachi.com
Hitachi, Ltd.
,630, Kandatsu
,Tsuchiura, Ibaraki 300-0013
, Japan
e-mail: manabu.yagi.cb@hitachi.com
Search for other works by this author on:
Kuniyoshi Tsubouchi,
Kuniyoshi Tsubouchi
Hitachi Research Laboratory,
e-mail: Kuniyoshi.tsybouchi.fx@hitachi.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: Kuniyoshi.tsybouchi.fx@hitachi.com
Search for other works by this author on:
Takanori Shibata
Takanori Shibata
1
Hitachi Research Laboratory,
e-mail: takanori_shibata@mhps.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: takanori_shibata@mhps.com
1Present address: Research & Development Center, Mitsubishi Hitachi Power Systems, LTD., 1-1 Saiwai-cho, 3-chome, Hitachi, Ibaraki 317-0073, Japan.
Search for other works by this author on:
Susumu Nakano
Hitachi Research Laboratory,
e-mail: susumu_nakano@mhps.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: susumu_nakano@mhps.com
Tadaharu Kishibe
Hitachi Research Laboratory,
e-mail: tadaharu_kishibe@mhps.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: tadaharu_kishibe@mhps.com
Manabu Yagi
Infrastructure Systems Company,
e-mail: manabu.yagi.cb@hitachi.com
Hitachi, Ltd.
,630, Kandatsu
,Tsuchiura, Ibaraki 300-0013
, Japan
e-mail: manabu.yagi.cb@hitachi.com
Kuniyoshi Tsubouchi
Hitachi Research Laboratory,
e-mail: Kuniyoshi.tsybouchi.fx@hitachi.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: Kuniyoshi.tsybouchi.fx@hitachi.com
Takanori Shibata
Hitachi Research Laboratory,
e-mail: takanori_shibata@mhps.com
Hitachi, Ltd.
,7-1-1, Omika
,Hitachi, Ibaraki 319-1292
, Japan
e-mail: takanori_shibata@mhps.com
1Present address: Research & Development Center, Mitsubishi Hitachi Power Systems, LTD., 1-1 Saiwai-cho, 3-chome, Hitachi, Ibaraki 317-0073, Japan.
Contributed by the Cycle Innovations Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received January 18, 2014; final manuscript received September 9, 2014; published online December 9, 2014. Assoc. Editor: Joost J. Brasz.
J. Eng. Gas Turbines Power. Jun 2015, 137(6): 061701 (7 pages)
Published Online: June 1, 2015
Article history
Received:
January 18, 2014
Revision Received:
September 9, 2014
Online:
December 9, 2014
Citation
Nakano, S., Kishibe, T., Yagi, M., Tsubouchi, K., and Shibata, T. (June 1, 2015). "Starting Characteristic Analysis of a Radial Inflow Turbine for the Regenerative Brayton Cycle." ASME. J. Eng. Gas Turbines Power. June 2015; 137(6): 061701. https://doi.org/10.1115/1.4028765
Download citation file:
Get Email Alerts
Cited By
An Adjustable Elastic Support Structure for Vibration Suppression of Rotating Machinery
J. Eng. Gas Turbines Power
Operation of a Compression Ignition Engine at Idling Load under Simulated Cold Weather Conditions
J. Eng. Gas Turbines Power
In-Cylinder Imaging and Emissions Measurements of Cold-Start Split Injection Strategies
J. Eng. Gas Turbines Power
Related Articles
Design Principles and Measured Performance of Multistage Radial Flow Microturbomachinery at Low Reynolds Numbers
J. Fluids Eng (November,2008)
On the Phenomenon of Pressure Pulses Reflecting Between Blades of Adjacent Blade Rows of Turbomachines
J. Turbomach (April,2011)
Modeling Shrouded Stator Cavity Flows in Axial-Flow Compressors
J. Turbomach (January,2000)
Performance Enhancement of Microturbine Engines Topped With Wave Rotors
J. Eng. Gas Turbines Power (January,2006)
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Introduction
Turbine Aerodynamics: Axial-Flow and Radial-Flow Turbine Design and Analysis
Performance Testing of Combined Cycle Power Plant
Handbook for Cogeneration and Combined Cycle Power Plants, Second Edition