Numerical simulation of performance of engine lip electro-thermal anti-icing system
-
摘要: 采用三维耦合传热方法对发动机唇口电热防冰系统进行了多状态下的性能仿真,获得了唇口表面平衡温度及动态温升响应时间,以此评估防冰系统性能,并通过与冰风洞试验结果对比,对仿真过程进行了修正。研究表明:唇口表面加热区平衡温度均高于273.15 K,温升响应时间小于60 s,满足防冰需要,较为严酷的防冰状态点主要为飞行速度较大、环境温度较低的状态点;修正唇口材料导热系数后,仿真与试验结果吻合良好。研究结果能有效指导工程研制,对提高防除冰仿真分析结果的准确性提供了很好的借鉴。Abstract: A three-dimensional coupled numerical simulation method was applied to simulate the performance of an engine lip electro-thermal anti-icing system at different conditions. The balance temperature of engine lip surface and the dynamic response time of surface temperature rise were obtained to estimate the performance of the anti-icing system. The simulated results were compared with experimental results in icing tunnel. And based on the comparison,simulated results were corrected. The study showed that the balance temperature of engine lip heating surface was above 273.15 K and the dynamic response time was less than 60 s,indicating that this anti-icing system could meet the requirement,and the severe anti-icing conditions were mainly those with higher flight speed and lower ambient temperature. And after correction the simulation coincided with experiment. The results can effectively guide the engineering development and provide a reference to improve the accuracy of anti-icing simulation.
-
[1] 汪涛,王俊琦,王朝蓬.直升机进气道防冰试验方法设计与试验[J].科学技术与工程,2017,17(20):294-301. WANG Tao,WANG Junqi,WANG Zhaopeng.Method design of helicopter inlet duct anti-ice and experiment[J].Science Technology and Engineering,2017,17(20):294-301.(in Chinese) [2] 裘燮纲,韩凤华.飞机防冰系统[M].北京:国防工业出版社,1985. [3] 张书晔,徐伟,于磊.飞机发动机唇口防冰系统仿真分析[J].飞机设计,2016,36(6):58-64. ZHANG Shuye,XU Wei,YU Lei.Emulation analysis for engine lip anti-ice system[J].Aircraft Design,2016,36(6):58-64.(in Chinese) [4] KEITH T,Jr,DE WITT K J.Numerical simulation of an electrothermally de-iced aircraft surface using the finite element method[R].AIAA 91-0268,1991. [5] MAHDI P,HABASHI W G.Aero-thermal optimization of in-flight electro-thermal ice protection systems in transient de-icing mode[J].International Journal of Heat and Fluid Flow,2015,54:167-182. [6] BU X,YU J,LIN G,et al.Electrothermal airfoil anti-icing system simulation[J].Hkie Transactions,2010,17(2):9-13. [7] 钟国.翼型电热防/除冰系统的数值模拟[J].航空制造技术,2011(4):75-79. ZHONG Guo.Simulation of airfoil electro-thermal anti-ice/de-ice system[J].Aeronautical Manufacturing Technology,2011(4):75-79.(in Chinese) [8] 霍西恒,屠敏,常士楠,等.CJ818客机尾翼周期电热除冰系统计算分析[J].民用飞机设计与研究,2009(增刊1):126-130. HUO Xiheng,TU Min,CHANG Shinan,et al.Cycle electrothermal de-icing system analysis of CJ818 aircraft tail[J].Civil Aircraft Design and Research,2009(Suppl.1):126-130.(in Chinese) [9] REID T,BARUZZI G S,HABASHI W G.FENSAP-ICE:unsteady conjugate heat transfer simulation of electrothermal de-icing[J].Journal of Aircraft,2012,49(4):1101-1109. [10] FAKOREDE O,IBRAHIM H,ILINCA A,et al.Experimental investigation of power requirements for wind turbines electrothermal anti-icing systems[M].Rijeka,Croatia:[s.n.],2016. [11] BUSCHHORN S T,KESSLER S S,LACHMANN N,et al.Electro thermal icing protection of aerosurfaces using conductive polymer nanocomposites[R].AIAA-2013-1729,2013. [12] 杨诗雨,常士楠,高艳欣,等.旋转帽罩电加热防冰瞬态过程研究[J].空气动力学学报,2016,34(3):289-294. YANG Shiyu,CHANG Shinan,GAO Yanxin,et al.Investigation of rotary cone electric heating anti-icing transient process[J].Acta Aerodynamic Sinica,2016,34(3):289-294.(in Chinese) [13] 董威,朱剑鋆,周志翔,等.航空发动机支板热滑油防冰性能试验[J].航空学报,2014,35(7):1845-1853. DONG Wei,ZHU Jianyun,ZHOU Zhixiang,et al.Test on performance of an aero-engine strut hot lubrication oil anti-icing system[J].Acta Aeronautica et Astronuatica Sinica,2014,35(7):1845-1853.(in Chinese) [14] 朱光亚.电加热防冰部件加热功率的分布特性研究[D].南京:南京航空航天大学,2014. ZHU Guangya.Study on heat power distribution characteristic for aircraft anti-ice components[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2014.(in Chinese) [15] 马辉,张大林,孟繁鑫,等.复合材料部件电加热防冰性能试验[J].航空学报,2013,34(8):1846-1853. MA Hui,ZHANG Dalin,MENG Fanxin,et al.Experimental of electro-thermal anti-icing on a composite assembly[J].Acta Aeronautica et Astronuatica Sinica,2013,34(8):1846-1853.(in Chinese) [16] 雷桂林,郑梅,董威,等.航空发动机进气支板电热防冰试验[J].航空学报,2017,38(8):54-65. LEI Guilin,ZHENG Mei,DONG Wei,et al.Test on electrothermal anti-icing of aero-engine inlet strut[J].Acta Aeronautica et Astronautica Sinica,2017,38(8):54-65.(in Chinese) [17] WIROGO S,SRIRAMBHATLA S.An Eulerian method to calculate the collection efficiency on two and three dimensional bodies[R].AIAA-2003-1073,2003. [18] 孙志国,付斌,朱春玲.探头式结冰探测器安装位置分析[J].航空动力学报,2011,26(12):2676-2683. SUN Zhiguo,FU Bin,ZHU Chunling.Analysis on installation location of probe-style ice detectors[J].Journal of Aerospace Power,2011,26(12):2676-2683.(in Chinese) [19] MINGIONE G,BRANDI V,ESPOSITO B.Ice accretion prediction on multi-element airfoils[R].AIAA 97-0178,1997.
点击查看大图
计量
- 文章访问数: 219
- HTML浏览量: 11
- PDF量: 393
- 被引次数: 0