Naval Centrifugal Compressor Design Using CAD Solutions

Constantin Dumitrache; Ioan Calimanescu; Corneliu Comandar

doi:10.4028/www.scientific.net/AMM.658.59

Paper Titles

Chain Tracking System for Solar Thermal Collector
p.35

Algorithms for Noncircular Gear Pitch Curves Generation
p.41

Singularities Classification for Structural Groups of Dyad Type
p.47

Transmission Indices Adoption for 6R Structural Group
p.55

Naval Centrifugal Compressor Design Using CAD Solutions
p.59

Naval Standard Safety Valve Design Using CAD Solutions
p.65

Mechanical Characteristics of Electronic Printed Circuit Obtained by the Vapour Phase Soldering Process
p.71

Evaluation of Loss of Mass due to Corrosion Using Vibration-Based Methods
p.77

Simulation of the Tooth Helix Angle Influence on the Vibration of a Single Stage Helical Gearbox
p.83

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 658Naval Centrifugal Compressor Design Using CAD...

Naval Centrifugal Compressor Design Using CAD Solutions

Abstract:

Centrifugal compressors of turbochargers operate in a wide range of rotational speeds, which depends on the load of the supercharged engine. Current designs of turbocharger compressors exhibit high efficiencies accompanied by high flow capacities [1]. Consequences of aerodynamic optimization are high mean stress values in the blades due to centrifugal loading as well as dynamic stresses due to blade vibrations. Blade vibrations in a turbocharger compressor are assumed to be predominantly excited by unsteady aerodynamic forces [2]. These forces are caused by a variety of sources influencing the flow. Examples include the geometry of the flow channel, elbows, the diffuser vanes or struts. Therefore, an understanding of FSI is essential for further design optimizations.

You might also be interested in these eBooks

Advanced Concepts in Mechanical Engineering I

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 658)

Pages:

59-64

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.658.59

Citation:

Cite this paper

Online since:

October 2014

Authors:

Constantin Dumitrache*, Ioan Calimanescu, Corneliu Comandar

Keywords:

Ansys 13, CAD Nx 8 Siemens, Compressor, Computational Fluid Dynamics (CFD)

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Aungier, R.H., Mean Streamline Aerodynamic Performance Analysis of Centrifugal Compressors, Journal of Turbomachinery, 1995 July, ASME, vol. 117, pp.360-366.

DOI: 10.1115/1.2835669

Google Scholar

[2] Aungier, R.H., Centrifugal Compressors - A Strategy for Aerodynamic Design and Analysis, ASME Press, New York, (2000).

Google Scholar

[3] Dixon, S.L., Fluid Mechanics and Thermodynamics of Turbomachinery, Elsevier Butterworth-Heinemann, (2005).

Google Scholar

[4] Eckardt, D., Detailed Flow Investigations Within a High-Speed Centrifugal Compressor Impeller, Journal of Fluids Engineering, 1976 September, ASME, vol. 98, pp.390-402.

DOI: 10.1115/1.3448334

Google Scholar

[5] Krain, H., A Study on Centrifugal Impeller and Di-user Flow, Journal of Engineering for Power, 1981 October, ASME, vol. 103, pp.688-697.

DOI: 10.1115/1.3230791

Google Scholar

[6] Barhalescu M. L., Comparison of Corrosion Behavior of thin layers from copper, aluminium and chromium, Advanced Materials Research, vol 837, pag. 247-252, 2013, www. scientific. net/AMR. 837. 247.

DOI: 10.4028/www.scientific.net/amr.837.247

Google Scholar