某航空活塞发动机进气系统优化设计

Translated title of the contribution: Intake system optimization study and design for an aircraft piston engine

Huasheng Cui, Zhenfeng Zhao, Enhua Wang, Qiongyao Yang, Yuhang Liu

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

A one-dimensional thermal dynamic model and three dimensional CFD model about the intake pipe for a specific aero-piston engine were established respectively for analyzing intake uniformity. These models verified the phenomenon about intake uniformity when the engine worked under external characteristic condition and figured out the causality of this phenomenon. An intake system was designed. The intake uniformity phenomenon could be improved by taking this intake system. The calculation results showed that: by adopting the new intake system, the engine's intake air non-uniformity decreased from 20% to 6% when the engine was at 5000r/min. By using this intake system, the average air intake quality increased by 19% when the engine was at 5500r/min, the maximum air intake quality increased by 34.1% and the minimum by 12.9%.

Translated title of the contributionIntake system optimization study and design for an aircraft piston engine
Original languageChinese (Traditional)
Pages (from-to)2063-2070
Number of pages8
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume34
Issue number9
DOIs
Publication statusPublished - 1 Sept 2019

Fingerprint

Dive into the research topics of 'Intake system optimization study and design for an aircraft piston engine'. Together they form a unique fingerprint.

Cite this