航空活塞二冲程汽油机排气口高度优化研究

Translated title of the contribution: Optimization research of the exhaust height on aviation piston two-stroke gasoline engine

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

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.

Translated title of the contributionOptimization research of the exhaust height on aviation piston two-stroke gasoline engine
Original languageChinese (Traditional)
Pages (from-to)442-450
Number of pages9
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume34
Issue number2
DOIs
Publication statusPublished - 1 Feb 2019

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