Icing and anti-icing test technology of aero-engine based on large-scale icing wind tunnel

LAI Qingren; LIU Qinglin; GUO Long; ZHANG Pingtao; YI Xian

doi:10.11729/syltlx20200067

Volume 35 Issue 3

Jun. 2021

Turn off MathJax

Article Contents

Article Navigation > Journal of Experiments in Fluid Mechanics > 2021 > 35(3): 1-8

LAI Qingren, LIU Qinglin, GUO Long, et al. Icing and anti-icing test technology of aero-engine based on large-scale icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(3): 1-8. doi: 10.11729/syltlx20200067

Citation:

PDF( 9469 KB)

Icing and anti-icing test technology of aero-engine based on large-scale icing wind tunnel

doi: 10.11729/syltlx20200067

LAI Qingren^{1, 2
,},
LIU Qinglin^{1, 2},
GUO Long^{1, 2},
ZHANG Pingtao^{1, 2},
YI Xian^{1, 2
,
,}

1.
Key Laboratory of Icing and Anti/De-Icing, China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China
2.
Low Speed Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China

Received Date: 2020-05-25
Rev Recd Date: 2020-07-28
Publish Date: 2021-06-25

Abstract

Abstract

The icing and anti-icing process of the aero-engine is complex, which can not be simulated accurately by numerical calculation. As a result, experiment is an indispensable means for the engine research. The first large-scale icing wind tunnel of our country has been built, which has the capacity to carry out icing tests on the aircraft wing section. But further development of the icing and anti-icing test technology is needed to meet the requirement of the next stage model designing and airworthiness certification for aero-engines in our country. Supported by the 3 m×2 m large-scale icing wind tunnel, the inlet gas simulation technology and hot-air supply technology were developed first, then a set of test procedures and methods was put forward, and finally the icing wind tunnel test for the inlet part of an aero-engine was carried out. The results indicate that the system can simulate the internal and external flow coupling of the engine and the anti-icing state of the compressor. The procedures and method of icing wind tunnel test are reasonable and feasible, and the test dynamic process and the flow field pressure in the inlet are successfully measured. It provides a technical support for the design of ice protection system and the verification of airworthiness on aero-engines.
- icing wind tunnel,
- aero-engine,
- inlet gas simulation,
- hot-air supply,
- tests

FullText(HTML)

References(19)

References

[1]	林贵平, 卜雪琴, 申晓斌. 飞机结冰与防冰技术[M]. 北京: 北京航空航天大学出版社, 2016. LIN G P, BU X Q, SHEN X B. Aircraft icing and anti-icing technology[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2016.
[2]	《航空发动机设计手册》总编委会. 航空发动机设计手册-第16册[M]. 北京: 航空工业出版社, 2001. Aero-engine Design Manual Editorial Board. Aero-engine design manual, Volume 16[M]. Beijing: Aviation Industry Press, 2001.
[3]	中国民用航空局. 航空发动机适航规定(CCAR-33R2)[Z]. 2011. Civil Aviation Administration of China. Airworthiness Regulations for aero-engine (CCAR-33R2)[Z]. 2011.
[4]	MASON J G, STRAPP J W, CHOW P. The ice particle threat to engine in flight[R]. AIAA 2006-206, 2006.
[5]	VENKATARAMANI K S, BALAN C, CANEY R D, et al. Wind tunnel tests and modeling studies of ice accretion relevant to aircraft engines[R]. AIAA 2003-906, 2003.
[6]	HAMED A, DAS K, BASU D. Numerical simulations of ice droplet trajectories and collection efficiency on aero-engine rotating machinery[R]. AIAA-2005-1248, 2005. doi: 10.2514/6.2005-1248
[7]	JIN W, TAGHAVI R. A computational study of icing effects on performance of S-duct inlets[R]. AIAA-2008-4584, 2008. doi: 10.2514/6.2008-4584
[8]	LEE S, LOTH E, KIM S, et al. Simulation of icing on a cascade of stator blades[R]. AIAA-2006-0208, 2006. doi: 10.2514/6.2006-208
[9]	LUTTRELL J, WEST T. F-22 inlet shed ice particle sizing test[R]. AIAA-2001-16026, 2001. doi: 10.2514/6.2001-91
[10]	AL-KHALIL K, HITZIGRATH R, PHILIPPI O, et al. Icing analysis and test of a business jet engine inlet duct[R]. AIAA 2000-1040, 2000. doi: 10.2514/6.2000-1040
[11]	RAGNI A, AULETTA A, CASERTA G, et al. Air induction system icing certification for general aviation: the case of the vulcanair VF600w mission aircraft[R]. AIAA-2005-476, 2005. doi: 10.2514/6.2005-476
[12]	FERRIGNO F, INVERNO M, VERNILLO P, et al. NH90 air intake version T700/T6-E1 icing qualification tests[R]. AIAA-2005-477, 2005. doi: 10.2514/6.2005-477
[13]	PAPADAKIS M, YEONG H W, WONG S C, et al. Comparison of experimental and computational ice shapes for an engine inlet[R]. AIAA-2010-7671, 2010. doi: 10.2514/6.2010-7671
[14]	刘华, 郭文, 杨军, 等. 发动机进气帽罩防冰热载荷的数值模拟研究[J]. 燃气涡轮试验与研究, 2012, 25(1): 44-48. https://www.cnki.com.cn/Article/CJFDTOTAL-RQWL201201013.htm LIU H, GUO W, YANG J, et al. Numerical investigation of anti-icing thermal loads for engine inlet cowl[J]. Gas Turbine Experiment and Research, 2012, 25(1): 44-48. https://www.cnki.com.cn/Article/CJFDTOTAL-RQWL201201013.htm
[15]	徐磊, 周建军, 张大林, 等. 发动机进口支板防冰热负荷数值模拟[J]. 航空发动机, 2009, 35(4): 16, 21-24. https://www.cnki.com.cn/Article/CJFDTOTAL-HKFJ200904007.htm XU L, ZHOU J J, ZHANG D L, et al. Numerical simulation of anti-icing heat load for strut of aeroengine inlet[J]. Aeroengine, 2009, 35(4): 16, 21-24. https://www.cnki.com.cn/Article/CJFDTOTAL-HKFJ200904007.htm
[16]	王波, 董葳, 崔浩. 防冰状态下涡轴发动机零级导叶壁面温度场的计算[J]. 能源技术, 2007(3): 129-132. https://www.cnki.com.cn/Article/CJFDTOTAL-LYJI200703003.htm WANG B, DONG W, CUI H. Temperature field calculation of turbo-shaft engine's inlet guide vane under anti-icing condition[J]. Energy Technology, 2007(3): 129-132. https://www.cnki.com.cn/Article/CJFDTOTAL-LYJI200703003.htm
[17]	董葳, 侯玉柱, 闵现花. 进口导向叶片热气防冰系统试验[J]. 上海交通大学学报, 2010, 44(11): 1579-1582. doi: 10.16183/j.cnki.jsjtu.2010.11.020 DONG W, HOU Y Z, MIN X H. Experimental study of hot air anti-icing system of inlet guide vane[J]. Journal of Shanghai Jiao Tong University, 2010, 44(11): 1579-1582. doi: 10.16183/j.cnki.jsjtu.2010.11.020
[18]	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. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201407009.htm DONG W, ZHU J J, ZHOU Z X, et al. Test on performance of an aero-engine strut hot lubrication oil anti-icing system[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(7): 1845-1853. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201407009.htm
[19]	杨军, 张靖周, 郭文, 等. 航空发动机进口支板结冰和防冰试验[J]. 航空动力学报, 2014, 29(2): 277-283. doi: 10.13224/j.cnki.jasp.2014.02.005 YANG J, ZHANG J Z, GUO W, et al. Experiment of anti-icing and icing on inlet strut of aero-engine[J]. Journal of Aerospace Power, 2014, 29(2): 277-283. doi: 10.13224/j.cnki.jasp.2014.02.005