航空活塞二冲程汽油机排气口高度优化研究

科研成果: 期刊稿件文章同行评审

4 引用 (Scopus)

摘要

In order to study the influence on engine performance by a variable-exhaust two-stroke engine as the unmanned aircraft power with removal of the variable exhaust system, the simulation of the cylinder's working process in the engine was established using Fire simulation software. In the model, the characteristics of the engine after removing the variable exhaust system were studied through simulation and test. The results showed that after removing the variable exhaust system under the condition of 2000r/min, 10% throttle opening and 5500r/min, 50% throttle opening, the scavenging efficiency of the engine and the output power were reduced. On this basis, using the simulation study method to optimize the exhaust outlet height parameters, the results showed that: after removing the variable system, the optimal value of the exhaust outlet height was 36. 3mm, which can guarantee the common drone flight speed range. The scavenging efficiency is high under all operating conditions. The loss of engine indicator power is minimal, and the output power can satisfy the drone power demand.

投稿的翻译标题Optimization research of the exhaust height on aviation piston two-stroke gasoline engine
源语言繁体中文
页(从-至)442-450
页数9
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
34
2
DOI
出版状态已出版 - 1 2月 2019

关键词

  • Aero-piston gasoline engine
  • Exhaust height
  • Performance optimization
  • Scavenging efficiency
  • Two-stroke

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