Backfire tests of an aircraft piston engine

Zhi Qiang Zhang*, Jun He, Ming Shan Wei, Jin Zhang, Xiao Zhu Liu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

7 Citations (Scopus)

Abstract

In order to solve the problem of one aircraft piston engine that the backfire test must be conducted to acquire the airworthiness type certificate (TC) pursuant to article 33.51 of part CCAR-33 "Airworthiness standard of aircraft piston engine", a new test method was proposed based on the photoelectric signals through the study on single-cylinder engine. The experiments showed that the proposed method can well detect the backfire. Based on the above research, the inducing backfire method was conducted through reducing the flow rate of fuel by operating lean/rich joystick. The experiments on the tested engine show the engine is tendency to backfire in its operating conditions and the engine works well after 57 times artificial induction backfire on the tested engine. The tested engine meets the requirements of airworthiness certification.

Original languageEnglish
Pages (from-to)1696-1701
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume28
Issue number8
Publication statusPublished - Aug 2013

Keywords

  • Aircraft piston engine
  • Airworthiness certification
  • Artificial inducement of backfire
  • Backfire tests
  • Backfire tests method

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