Please wait a minute...
 首页  期刊介绍 期刊订阅 联系我们
 
最新录用  |  预出版  |  当期目录  |  过刊浏览  |  阅读排行  |  下载排行  |  引用排行  |  百年期刊
Journal of Tsinghua University(Science and Technology)    2022, Vol. 62 Issue (3) : 549-554,580     DOI: 10.16511/j.cnki.qhdxxb.2021.26.037
SPECIAL SECTION: AIR-BREATHING ENGINE AND AEROSPACE POWER TECHNOLOGY |
Turboshaft engine compressor design using ANSYS
YAN Huihui, ZHOU Bohao, LI Hao, ZHANG Yuzhou, LAN Xudong
Aero Engine Research Center, School of Aerospace Engineering, Tsinghua University, Beijing 100084, China
Download: PDF(5438 KB)   HTML
Export: BibTeX | EndNote | Reference Manager | ProCite | RefWorks    
Abstract  Turboshaft engines are smaller, lighter and have shorter shafts than large turbofan and turbojet engines. Due to their good high altitude performance and wide power range, turboshaft engines have gradually replaced piston engines in unmanned helicopters. However, piston engines are less expensive, so they still have the absolute advantage in small unmanned helicopters. Further research is needed to develop economical low power turboshaft engines. This study analyzed the design of a 300 kW turboshaft engine using Gas Turb, a thermodynamic turbine analysis software, with the blade modeling module of ANSYS used to design the impeller and blades of the centrifugal compressor. Three-dimensional simulations of the centrifugal compressor verify the feasibility of this design.
Keywords turboshaft engines      engine design      centrifugal compressors      numerical simulations     
Issue Date: 10 March 2022
Service
E-mail this article
E-mail Alert
RSS
Articles by authors
YAN Huihui
ZHOU Bohao
LI Hao
ZHANG Yuzhou
LAN Xudong
Cite this article:   
YAN Huihui,ZHOU Bohao,LI Hao, et al. Turboshaft engine compressor design using ANSYS[J]. Journal of Tsinghua University(Science and Technology), 2022, 62(3): 549-554,580.
URL:  
http://jst.tsinghuajournals.com/EN/10.16511/j.cnki.qhdxxb.2021.26.037     OR     http://jst.tsinghuajournals.com/EN/Y2022/V62/I3/549
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
[1] 《航空发动机设计手册》总编委员会. 航空发动机设计手册第6册:涡桨及涡轴发动机总体[M]. 北京:航空工业出版社, 2001.Editorial board of aeroengine design manual. Aeroengine design manual volume 6:Turboprop and turboshaft engine[M]. Beijing:Aviation Industry Press, 2001. (in Chinese)
[2] 柳子昂. 高压比离心压气机叶型优化与数值研究[D]. 南京:南京航空航天大学, 2013.LIU Z A. The profile optimization and numerical simulation of high pressure ratio centrifugal compressor[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2013. (in Chinese)
[3] 《航空发动机设计手册》总编委员会. 航空发动机设计手册第8册:压气机[M]. 北京:航空工业出版社, 2000.Editorial board of aeroengine design manual. Aeroengine design manual volume 8:Compressor[M]. Beijing:Aviation Industry Press, 2001. (in Chinese)
[4] BONAIUTI D, AMONE A, ERMINI M, et al. Analysis and optimization of transonic centrifugal compressor impellers using the design of experiments technique[J]. Journal of Turbomachinery, 2006, 128(4):786-797.
[5] MALIK A, ZHENG Q. Effect of double splitter blades position in centrifugal compressor impeller[J]. Proceedings of the Institution of Mechanical Engineers, Part A:Journal of Power and Energy, 2019, 233(6):689-701.
[6] 高井辉. 基于CFX的离心式压气机内部流场数值研究[D].大连:大连理工大学, 2011.GAO J H. Numerical investigation on centrifugal compressor based on CFX[D]. Dalian:Dalian University of Technology, 2011. (in Chinese)
[7] 冀国锋, 殷明霞, 桂幸民. 某小型离心压气机气动设计[J]. 航空动力学报, 2010, 25(3):557-564.JI G F, YIN M X, GUI X M. Aerodynamic design of a small centrifugal compressor[J]. Journal of Aerospace Power, 2010, 25(3):557-564. (in Chinese)
[8] 袁鹏. 涡轴发动机气动性能改进研究及离心叶轮改型设计[D]. 南京:南京航空航天大学, 2007.YUAN P. Research on the performance of a turboshaft engine and its centrifugal compressor impeller design[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2007. (in Chinese)
[9] YANG C, LI Z G, JIANG Z K, et al. Numerical investigation of a high-speed centrifugal compressor impeller[J]. Tsinghua Science and Technology, 1999, 4(4):1678-1682.
[10] 杨策, 马朝臣, 王憔, 等. 离心压气机的初步设计及其优化方法[J]. 内燃机学报, 2001(5):454-458.YANG C, MA C C, WANG Q, et al. Preliminary design and optimization of centrifugal compressor[J]. Transactions of CSICE, 2001(5):454-458. (in Chinese)
[11] LOU F Y, KEY N L. Design considerations for the final-stage centrifugal compressor in aeroengines[J]. Journal of Propulsion and Power, 2020(2):1-5.
[12] CHUNG J, KIM N, LEE S, et al. Performance improvement of the pressure ratio and rotational speed calculation of a centrifugal compressor model[J]. International Journal of Automotive Technology, 2020, 21(3):703-711.
[13] 王琦, 单鹏. 径流及斜流压气机任意曲面叶型长短叶片的造型设计方法[J]. 航空动力学报, 2006(4):747-753.WANG Q, SHAN P. Design of radial flow and mixed flow compressor rotor splitter blades[J]. Journal of Aerospace Power, 2006(4):747-753. (in Chinese)
[1] SHI Lin, XU Qianghui. Fundamental studies of air injection for heavy crude oil recovery and its applications[J]. Journal of Tsinghua University(Science and Technology), 2022, 62(4): 722-734.
[2] ZHANG Zhihan, LIU Hui, L�Zhenlei, HOU Yansong, SUN Lifeng, WANG Shi, WU Zhaoxia, LIU Yaqiang. Design and numerical simulations of a large animal SPECT system[J]. Journal of Tsinghua University(Science and Technology), 2022, 62(12): 1875-1883.
[3] CHEN Meng, CHEN Zhao, LIU Rongzheng, LIU Bing, SHAO Youlin, TANG Yaping, LIU Malin. Numerical simulations of particle coating using the fluidized bed-chemical vapor deposition method[J]. Journal of Tsinghua University(Science and Technology), 2022, 62(10): 1645-1659.
[4] Hong ZHANG,Yang LI,Xuanbing CHEN. Simulation and evaluation of the home-purchase limit policy effect based on a search-matching model[J]. Journal of Tsinghua University(Science and Technology), 2015, 55(1): 68-73.
Viewed
Full text


Abstract

Cited

  Shared   
  Discussed   
Copyright © Journal of Tsinghua University(Science and Technology), All Rights Reserved.
Powered by Beijing Magtech Co. Ltd