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Improved High Pressure Ratio Centrifugal Compressor

Krain, H. and Hoffmann, B. and Rohne, K.-H. and Eisenlohr, G. and Richter, F.-A. (2007) Improved High Pressure Ratio Centrifugal Compressor. In: ASME TURBO EXPO 2007, pp. 1-9. ASME TURBO EXPO 2007, 2007-05-14 - 2007-05-17, Montreal, Kanada.

Full text not available from this repository.

Abstract

The paper describes the development and the experimental as well as theoretical investigation of a new transonic, high specific speed centrifugal compressor rotor of 6.2:1 pressure ratio. Performance measurement results, laser measurements and calculated 3D results are shown for the new rotor and are compared with the corresponding data of a same type predecessor rotor.

Document Type:Conference or Workshop Item (Paper)
Title:Improved High Pressure Ratio Centrifugal Compressor
Authors:
AuthorsInstitution or Email of Authors
Krain, H.UNSPECIFIED
Hoffmann, B.UNSPECIFIED
Rohne, K.-H.ABB Turbo Systems, Baden, Schweiz
Eisenlohr, G.Consultant, Oberursel
Richter, F.-A.MAN TURBO AG, Oberhausen
Date:14 May 2007
Journal or Publication Title:ASME TURBO EXPO 2007
Refereed publication:Yes
In ISI Web of Science:Yes
Page Range:pp. 1-9
Editors:
EditorsEmail
ASME, UNSPECIFIED
Series Name:ASME Paper GT2007-27100
Status:Published
Keywords:Centrifugal compressor, performance measurement, laser measurements, 3D calculations
Event Title:ASME TURBO EXPO 2007
Event Location:Montreal, Kanada
Event Type:international Conference
Event Dates:2007-05-14 - 2007-05-17
Organizer:American Society of Mechanical Engineering
HGF - Research field:Energy
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: Dr.-Ing. Hartmut Krain
Deposited On:29 Jun 2007
Last Modified:15 Jan 2010 00:55

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