首页 | 本学科首页   官方微博 | 高级检索  
     

变循环压缩系统的一体化通流设计方法
引用本文:刘宝杰,贾少锋,于贤君. 变循环压缩系统的一体化通流设计方法[J]. 航空动力学报, 2016, 31(11): 2750-2756. DOI: 10.13224/j.cnki.jasp.2016.11.025
作者姓名:刘宝杰  贾少锋  于贤君
作者单位:1. 北京航空航天大学能源与动力工程学院,北京100191;北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室,北京100191;先进航空发动机协同创新中心,北京100191;2. 北京航空航天大学能源与动力工程学院,北京,100191
基金项目:国家自然科学基金(51376014,51476004)
摘    要:以双外涵和三外涵两款典型的涡扇发动机的变循环压缩系统为研究对象发展了一个基于流线曲率法的一体化通流设计方法,以期简化变循环压缩系统的设计流程,缩短设计周期.通过一个三外涵变循环压缩系统的设计实例,验证了方法的正确性和程序的功能完整性,得到了以下主要结论:①第1,2外涵道的连通使压缩系统各部件之间的气动关系变得复杂,正确处理各部件之间的匹配关系是一体化设计的关键;②流线曲率法适用于变循环压缩系统的通流设计,其流量边界条件可方便地用于模拟前可调面积涵道引射器的调节功能;③第1,2外涵道的掺混过程对上游叶片区域的流场影响微弱,采用简单的掺混模型能够满足计算需求.

关 键 词:变循环  压缩系统  一体化设计  通流  流线曲率法
收稿时间:2015-04-30

Integrated throughflow design method of variable-cycle compression system
LIU Bao-jie,JIA Shao-feng and YU Xian-jun. Integrated throughflow design method of variable-cycle compression system[J]. Journal of Aerospace Power, 2016, 31(11): 2750-2756. DOI: 10.13224/j.cnki.jasp.2016.11.025
Authors:LIU Bao-jie  JIA Shao-feng  YU Xian-jun
Affiliation:School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China,School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China and School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China
Abstract:Targeting the two typical variable-cycle compressor system of turbofan engines, double-bypass engine and triple-bypass engine, an integrated throughflow design method based on streamline curvature method was proposed for simplifying the design process of a variable-cycle compression system and shortening the design cycle. By solving the flow filed of a triple-bypass variable-cycle compression system, the feasibility of the method and the capability of the code was proven. Three main conclusions were drawn:(1) The connection of the first and second bypasses complicates the aerodynamic correlations of the components and correctly reflecting the correlations is the key of an integrated design method. (2) Streamline curvature method is suitable for variable-cycle compression system design and its mass flow boundary conditions can be used for modeling the function of the front area-variable bypass injector. (3) The mixing process of the first and second bypasses flow will not influence the upstream blade flow field, and simple mixing model can meet the requirements for simulation of such a process.
Keywords:variable-cycle  compression system  integrated design  throughflow  streamline curvature method
本文献已被 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号