Experimental investigation on seal characteristics of straight-through labyrinth

Xia Zhang, Xiao Wei Zhang, Hui Ren Zhu, Zhen Wei Wang

Research output: Contribution to journalArticlepeer-review

5 Scopus citations

Abstract

The leakage characteristics of the real-size labyrinth were investigated experimentally. The influences of geometric parameter and rotational speed were analyzed. The results show that: (1) in the experimental range, leakage coefficient increases with increasing Reynolds number. (2) Leakage coefficient decreases with increasing labyrinth number. (3) Leakage coefficient decreases with increasing clearance under the same Reynolds number. (4) Rotational speed has little effect on the leakage coefficient under small clearance (s=0.4, 0.5 mm); when clearance is 0.6 mm, rotational speed has definite effect on the leakage coefficient, i.e. 2000 r/min.

Original languageEnglish
Pages (from-to)1753-1757
Number of pages5
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume25
Issue number8
StatePublished - Aug 2010

Keywords

  • Aircraft engine
  • Leakage coefficient
  • Rotation
  • Seal characteristics
  • Straight-through labyrinth

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