Skip to main navigation Skip to search Skip to main content

Matching of two-stage supercharging aircraft piston engines

  • Bin Xu*
  • , Shao Jun Xia
  • , Shi Chun Yang
  • , Fen Zhu Ji
  • , Yan Ling Hu
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

Through the single stage supercharging piston engine's research, two-stage supercharging applications in this type were applied. The air compressor series and the turbine wheel parallel scheme of arrangement were used to establish the modeling of the engine with GT-Power. According to same-flow method, two-stage supercharger matching was conducted and the waste gate valve flow regulation was calculated. The result demonstrates the turbine wheel and the air compressor in the overall height moves in the high efficiency area, and two levels of supercharging system's developments have provided the good foundation.

Original languageEnglish
Pages (from-to)496-500
Number of pages5
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume27
Issue number3
StatePublished - Mar 2012

Keywords

  • Aircraft piston engines
  • Full-height matching
  • Regulation
  • Same-flow turbines
  • Two-stage supercharging

Fingerprint

Dive into the research topics of 'Matching of two-stage supercharging aircraft piston engines'. Together they form a unique fingerprint.

Cite this