Measurement and Evaluation of Swirl-Type Flow in Labyrinth Seals of Conventional Turbine Stages,

Abstract

Previous studies of rotor whirl instability pointed out two different mechanisms inducing lateral forces within non-contacting labyrinth-type seals. Evaluating the part of exciting forces that results from leakage losses is possible by means of variable flow contraction in the gap of a seal with variable clearance at the circumference. The dominating part of exciting forces has its origin in unequal pressure distributions at the circumference of the seal with a shaft in out-of-centre position. The pressure distribution is mainly influenced by swirl-type flow at seal entry.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1982
Accession Number
ADP000361

Entities

People

  • L. Hauck

Tags

DTIC Thesaurus Topics

  • Clearances
  • Instability
  • Labyrinth Seals
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Test And Evaluation
  • Turbomachinery
  • Workshops

Readers

  • Aerodynamics.
  • Control Systems Engineering.
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