Experimental Investigation and Validation of High Cycle Fatigue Design Systems for Centrifugal Compressors

Schrift Standard Fett
Login

Forschungsstelle

INNOSUISSE

Projektnummer

9507.2;6 PFIW-IW

Projekttitel

Experimental Investigation and Validation of High Cycle Fatigue Design Systems for Centrifugal Compressors

Projekttitel Englisch

Experimental Investigation and Validation of High Cycle Fatigue Design Systems for Centrifugal Compressors.

Texte zu diesem Projekt

	Deutsch	Französisch	Italienisch	Englisch
Kurzbeschreibung		-	-
Abstract		-	-

Erfasste Texte

Kategorie	Text
Kurzbeschreibung (Deutsch)	Experimental Investigation and Validation of High Cycle Fatigue Design Systems for Centrifugal Compressors
Kurzbeschreibung (Englisch)	Experimental Investigation and Validation of High Cycle Fatigue Design Systems for Centrifugal Compressors.
Abstract (Deutsch)	Most of the compressive turbomachines in use for turbocharger and industrial applications are of the radial flow type. Manufacturers of centrifugal compressors operate in a very competitive international market and rely on newest technology in order to maintain and to improve their market share. This requires the continuous improvement of their technology. The scope of this project addresses blade vibration in a centrifugal compressor. The need for reliable data to advance the understanding of forced response in centrifugal compressors is one of the motivations for the proposed work. Secondly, there is a need to develop and validate computational tools to be used in the design process to guarantee mechanical integrity.
Abstract (Englisch)	Most of the compressive turbomachines in use for turbocharger and industrial applications are of the radial flow type. Manufacturers of centrifugal compressors operate in a very competitive international market and rely on newest technology in order to maintain and to improve their market share. This requires the continuous improvement of their technology. The scope of this project addresses blade vibration in a centrifugal compressor. The need for reliable data to advance the understanding of forced response in centrifugal compressors is one of the motivations for the proposed work. Secondly, there is a need to develop and validate computational tools to be used in the design process to guarantee mechanical integrity.