TY - JOUR
T1 - 航空活塞二冲程汽油机排气口高度优化研究
AU - Wang, Lei
AU - Zhao, Zhenfeng
AU - Yu, Chuncun
AU - Zhang, Fujun
N1 - Publisher Copyright:
© 2019, Editorial Department of Journal of Aerospace Power. All right reserved.
PY - 2019/2/1
Y1 - 2019/2/1
N2 - 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.
AB - 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.
KW - Aero-piston gasoline engine
KW - Exhaust height
KW - Performance optimization
KW - Scavenging efficiency
KW - Two-stroke
UR - http://www.scopus.com/inward/record.url?scp=85065791153&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.2019.02.020
DO - 10.13224/j.cnki.jasp.2019.02.020
M3 - 文章
AN - SCOPUS:85065791153
SN - 1000-8055
VL - 34
SP - 442
EP - 450
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 2
ER -