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General stability and design specification of the back-pressure supported axially compliant orbiting scroll.

Author(s) : BUSH J. W., HALLER D. K., GALANTE C. R.

Summary

A linear, first order relationship may be used to approximate the stability characteristic of the back-pressure supported orbiting scroll. The resulting average tip loads may be similarly represented. Operating zones of incipient orbiting scroll instability are found to approximately follow zones of constant compression ratio. A simple design procedure is presented which may be used to specify axial compliance parameters for stability over an arbitrary operating range and to estimate resulting tip loads.

Details

  • Original title: General stability and design specification of the back-pressure supported axially compliant orbiting scroll.
  • Record ID : 1993-0860
  • Languages: English
  • Publication date: 1992/07/14
  • Source: Source: Proc. 1992 int. Compress. Eng. Conf., Purdue Univ.
    vol. 3; 853-860; 5 fig.; 5 ref.
  • Document available for consultation in the library of the IIR headquarters only.

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