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AEROSPACE 410 AEROSPACE PROPULSION AFTRF AXIAL FLOW TURBINE RESEARCH FACILITY

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AEROSPACE 410 AEROSPACE PROPULSION AFTRF AXIAL FLOW TURBINE RESEARCH FACILITY TURBOMACHINERY AERO HEAT TRANSFER LABORATORY 47 Hammond Building PENNSYLVANIA STATE UNIVERSITY. Dr. Cengiz Camci. AXIAL FLOW TURBINE. AFTRF Operational Details. Axial Flow Turbine Research Facility - PowerPoint PPT Presentation

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Page 1: AEROSPACE 410 AEROSPACE PROPULSION AFTRF AXIAL FLOW TURBINE RESEARCH FACILITY
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AEROSPACE 410

AEROSPACE PROPULSION

AFTRF AXIAL FLOW TURBINE RESEARCH FACILITY

TURBOMACHINERY AERO HEAT TRANSFERLABORATORY

47 Hammond BuildingPENNSYLVANIA STATE UNIVERSITY

Dr. Cengiz Camci

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AXIAL FLOWTURBINE

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AFTRF Operational Details

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Axial Flow Turbine Research Facility(AFTRF)

Pennsylvania State University

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AFTRF PARAMETER value

Number of Rotor Blades 29

Hub Radius 0.3331 m

Tip Radius 0.4582 m

Tip Clearance 0.0097 m

Hub to Tip Ratio 0.7269

Rotor Turning Angle 95 o at Tip126 o at Hub

Number of Nozzle Guide Vanes 23

Nozzle Turning Angle 70 o

Design RPM 1322

Design Mass Flow Rate 11.4 kg/ s

Total-to-T otal Effi ciency ηtt 0.893

Stato r Effi ciency ηs 0.994

Rotor Eff iciency ηr 0.882

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EXAMPLES FROMACTUAL

AXIAL FLOW TURBINE

DESIGNS

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PW-4000

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PW-229

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SOLAR TURBINES CENTAUR

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CENTAUR FIRST STAGE

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CENTAUR SECOND STAGE

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