超声速进气道/发动机一体化控制

孙丰勇; 张海波; 叶志锋

doi:10.13224/j.cnki.jasp.2014.10.002

超声速进气道/发动机一体化控制

doi: 10.13224/j.cnki.jasp.2014.10.002

南京航空航天大学能源与动力学院江苏省航空动力系统重点实验室, 南京 210016

基金项目:

航空科学基金（20120652）

详细信息

作者简介:
孙丰勇（1990- ），男，山东泰安人，博士生，主要研究方向为航空发动机建模与控制.

中图分类号: V231
计量
- 文章访问数: 1866
- HTML浏览量: 3
- PDF量: 961
- 被引次数: 0
出版历程
- 收稿日期: 2013-06-17
- 刊出日期: 2014-10-28

Integrated control for supersonic inlet/engine

Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

摘要

摘要: 为了解决超声速进气道/发动机一体化问题，建立了可进行放气调节的超声速进气道部件级数学模型，而后将其与某双轴涡扇发动机部件级模型匹配，实现进气道与发动机共同工作.基于该进气道/发动机一体化部件级模型，分析计算了超声速进气道内流、外流特性，并研究了在超声速工作状态下进气道放气特性，验证了在超声速飞行时，发动机在中间状态与加力状态下，通过进气道放气调节，发动机安装推力提升了3%.
- 超声速进气道 /
- 进气道部件级模型 /
- 放气调节 /
- 安装性能 /
- 进气道/发动机一体化
Abstract: A component-level mathematical model of supersonic inlet with bleeding adjustment was developed to study of integrated performance for supersonic inlet/engine. Meanwhile, a coupling mathematical model of supersonic inlet and turbofan engine was built via a biaxial turbofan engine component-level models and inlet component-level models to describe their collaborate relationship. The properties of outside and inside flux of the intake were calculated base on this integrated component-level model for inlet/engine. Inlet bleeding properties in supersonic working mode were also analyzed. At last, the engine installed thrust was verified to be effectively enhanced 3% by the bleeding adjustment of inlet when the aircraft worked at supersonic flight in the middle and afterburner states.
- supersonic inlet /
- component-level model of inlet /
- bleeding adjustment /
- installed performance /
- integrated performance of inlet/engine

HTML

参考文献(18)

[1]	陈大光,张津.飞机-发动机性能匹配与优化[M].北京:北京航空航天大学出版社,1990.
[2]	Abbot J M,Anderson B H,Rice E J.Inlets,ducts and nozzles[R].NASA CP-3049,1987.
[3]	Orme J S,Conners T R.Supersonic flight test results of a performance seeking control algorithm on a NASA F-15 aircraft[R].AIAA 94-3210,1994.
[4]	Ball W H,Hickcox T E.Rapid evaluation of propulsion system effect[R].Armed Services Technical Information Agency Document,AD B031766,1978.
[5]	Kowalski E J.A computer code for estimating installed performance of aircraft gas turbine engines[R].NASA-CR-159691,1979.
[6]	Batterton P G,Arpasi,D J,Baumbick R.Digital integrated control of a Mach 2.5 mixed-compression supersonic inlet and an augmented mixed-flow turbofan engine[R].NASA-TM-X-307,1974.
[7]	Boksenbom A S,Feder M S.Analysis of parameters for thrust control of a turbojet engine equipped with air-inlet throttle and variable-area exhaust nozzle[R].NACA-RM-E8B27,1993.
[8]	Wakelam C T,Evans S W.Separation control for aero-engine intakes:Part 1 low-speed investigation of control strategies[J].Journal of Propulsion and Power,2012,28(4):758-765.
[9]	Wakelam C T,Evans S W.Separation control for aero-engine intakes:Part 2 high-speed investigations[J].Journal of Propulsion and Power,2012,28(4):766-772.
[10]	张兆,陶洋,黄国川.发动机短舱溢流阻力的数值模拟研究[J].航空学报,2013,34(3):547-553. ZHANG Zhao,TAO Yang,HUANG Guochuan.Numerical simulation and research about the spillage drag of the engine nacelle[J].Acta Aeronautica et Astronautica Sinica,2013,34(3):547-553.(in Chinese)
[11]	乐川,徐大军,蔡国飙.超声速溢流条件下二元超声速进气道附加阻力计算[J].航空动力学报,2010,25(11):2431-2436. YUE Chuan,XU Dajun,CAI Guobiao.Calculation of additional drag coefficient of supersonic inlet under supersonic spillage condition[J].Journal of Aerospace Power,2010,25(11):2431-2436.(in Chinese)
[12]	卢燕,樊思齐,马会民,等.超声速进气道与发动机的匹配[J].推进技术,2003,24(4):323-325. LU Yan,FAN Siqi,MA Huimin,et al.Matching between supersonic inlet and aero-engine[J].Journal of Propulsion Technology,2003,24(4):323-325.(in Chinese)
[13]	卢燕,樊思齐,马会民.超声速进气道数学模型研究[J].推进技术,2002,23(6):468-471. LU Yan,FAN Siqi,MA Huimin.Study for the mathematical model of supersonic inlet[J].Journal of Propulsion Technology,2002,23(6):468-471.(in Chinese)
[14]	钱飞,宋文艳,骆广琦.某型飞机-发动机一体化性能计算[J].航空动力学报,2013,28(5):1112-1118. QIAN Fei,SONG Wenyan,LUO Guangqi,Calculation of integrated performance for aircraft/engines[J].Journal of Aerospace Power,2013,28(5):1112-1118.(in Chinese)
[15]	马志超,唐海龙.某型飞机推进系统建模及超音速巡航优化分析[C]//中国航空学会推进系统气动热力学专业第十届学术交流会论文集.北京:中国航空学会,2005:99-105.
[16]	廉筱纯,吴虎.航空发动机原理[M].西安:西北工业大学出版社,2005.
[17]	樊思齐.航空发动机控制[M].西安:西北工业大学出版社,2008.
[18]	Farokhi S.Aircraft propulsion[M].Hoboken,USA:John Wiley & Sons,Incorporated,2010.