Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 95
Book Description
The objective of this program was the design and fabrication of a air-cooled high-temperature radial turbine (HTRT) intended for experimental evaluation in a warm turbine test facility at the Lewis Research Center. The rotor and vane were designed to be tested as a scaled version (rotor diameter of 14.4 inches diameter) of a 8.021 inch diameter rotor designed to be capable of operating with a rotor inlet temperature (RIT) of 2300 deg. F, a nominal mass flow of 4.56 lbm/sec, a work level of equal or greater than 187 Btu/lbm, and an efficiency of 86% or greater. The rotor was also evaluated to determine it's feasibility to operate at 2500 deg F RIT. The rotor design conformed to the rotor blade flow path specified by NASA for compatibility with their test equipment. Fabrication was accomplished on three rotors, a bladeless rotor, a solid rotor, and an air-cooled rotor.
Cooled High-Temperature Radial Turbine Program. Phase 2
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 95
Book Description
The objective of this program was the design and fabrication of a air-cooled high-temperature radial turbine (HTRT) intended for experimental evaluation in a warm turbine test facility at the Lewis Research Center. The rotor and vane were designed to be tested as a scaled version (rotor diameter of 14.4 inches diameter) of a 8.021 inch diameter rotor designed to be capable of operating with a rotor inlet temperature (RIT) of 2300 deg. F, a nominal mass flow of 4.56 lbm/sec, a work level of equal or greater than 187 Btu/lbm, and an efficiency of 86% or greater. The rotor was also evaluated to determine it's feasibility to operate at 2500 deg F RIT. The rotor design conformed to the rotor blade flow path specified by NASA for compatibility with their test equipment. Fabrication was accomplished on three rotors, a bladeless rotor, a solid rotor, and an air-cooled rotor.
Publisher:
ISBN:
Category :
Languages : en
Pages : 95
Book Description
The objective of this program was the design and fabrication of a air-cooled high-temperature radial turbine (HTRT) intended for experimental evaluation in a warm turbine test facility at the Lewis Research Center. The rotor and vane were designed to be tested as a scaled version (rotor diameter of 14.4 inches diameter) of a 8.021 inch diameter rotor designed to be capable of operating with a rotor inlet temperature (RIT) of 2300 deg. F, a nominal mass flow of 4.56 lbm/sec, a work level of equal or greater than 187 Btu/lbm, and an efficiency of 86% or greater. The rotor was also evaluated to determine it's feasibility to operate at 2500 deg F RIT. The rotor design conformed to the rotor blade flow path specified by NASA for compatibility with their test equipment. Fabrication was accomplished on three rotors, a bladeless rotor, a solid rotor, and an air-cooled rotor.
Cooled High-Temperature Radial Turbine
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781730936142
Category : Science
Languages : en
Pages : 98
Book Description
The objective of this program was the design and fabrication of a air-cooled high-temperature radial turbine (HTRT) intended for experimental evaluation in a warm turbine test facility at the LeRC. The rotor and vane were designed to be tested as a scaled version (rotor diameter of 14.4 inches diameter) of a 8.021 inch diameter rotor designed to be capable of operating with a rotor inlet temperature (RIT) of 2300 F, a nominal mass flow of 4.56 lbm/sec, a work level of equal or greater than 187 Btu/lbm, and efficiency of 86 percent or greater. The rotor was also evaluated to determine it's feasibility to operate at 2500 F RIT. The rotor design conformed to the rotor blade flow path specified by NASA for compatibility with their test equipment. Fabrication was accomplished on three rotors, a bladeless rotor, a solid rotor, and an air-cooled rotor. Snyder, Philip H. Unspecified Center...
Publisher: Independently Published
ISBN: 9781730936142
Category : Science
Languages : en
Pages : 98
Book Description
The objective of this program was the design and fabrication of a air-cooled high-temperature radial turbine (HTRT) intended for experimental evaluation in a warm turbine test facility at the LeRC. The rotor and vane were designed to be tested as a scaled version (rotor diameter of 14.4 inches diameter) of a 8.021 inch diameter rotor designed to be capable of operating with a rotor inlet temperature (RIT) of 2300 F, a nominal mass flow of 4.56 lbm/sec, a work level of equal or greater than 187 Btu/lbm, and efficiency of 86 percent or greater. The rotor was also evaluated to determine it's feasibility to operate at 2500 F RIT. The rotor design conformed to the rotor blade flow path specified by NASA for compatibility with their test equipment. Fabrication was accomplished on three rotors, a bladeless rotor, a solid rotor, and an air-cooled rotor. Snyder, Philip H. Unspecified Center...
Cooled Radial In-flow Turbines for Advanced Gas Turbine Engines
Author: J. M. Lane
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Paper presents the results of several Army-sponsored programs, the first of which addresses the performance potential for high-temperature radial turbine.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Paper presents the results of several Army-sponsored programs, the first of which addresses the performance potential for high-temperature radial turbine.
Development of high temperature turbine subsystem technology to a "technology readiness status".
Author: General Electric Company. Gas Turbine Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 580
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 580
Book Description
Development of High Temperature Turbine Subsystem Technology to a "technology Readiness Status" Phase II
Author: General Electric Company. Gas Turbine Division
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 214
Book Description
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 214
Book Description
Radial Turbine Cooling
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Cooling of Gas Turbines
Author: W. Byron Brown
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26
Book Description
Cooling of Gas Turbines
Author: W. Byron Brown
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
A Summary of Design Information for Water-cooled Turbines
Author: John C. Freche
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 30
Book Description
Gas Turbine Heat Transfer and Cooling Technology
Author: Je-Chin Han
Publisher: CRC Press
ISBN: 9781560328414
Category : Science
Languages : en
Pages : 666
Book Description
This book is intended to be a reference book for engineers working and interested in gas turbine heat transfer analysis and cooling design for advanced research. The methods presented in this book can be applied to heat exchangers, nuclear power plants and electronic component cooling.
Publisher: CRC Press
ISBN: 9781560328414
Category : Science
Languages : en
Pages : 666
Book Description
This book is intended to be a reference book for engineers working and interested in gas turbine heat transfer analysis and cooling design for advanced research. The methods presented in this book can be applied to heat exchangers, nuclear power plants and electronic component cooling.