| Citation: | ZHAO Zhao, XIONG Jianjun, RAN Lin, et al. Hot air supply anti/de-icing test technology in large-scale icing wind tunnel[J]. Journal of Aerospace Power, 2024, 39（5）：20210582 doi: 10.13224/j.cnki.jasp.20210582
|
The establishment of hot air supply anti/de-icing test system in icing wind tunnel is the main means to carry out hot air anti/de-icing test. In order to meet the requirements of anti/de-icing system design and icing airworthiness certification for a series of domestic aircrafts, China Aerodynamics Research and Development Center (CARDC) carried out research on the hot air supply anti/de-icing test technology based on the 3 m×2 m large-scale icing wind tunnel, and independently developed the hot air supply anti/de-icing system. The digital valve flow control unit, electric heater unit, flow control unit and other test systems were designed and developed, and the test process and method were established. The perfect multi-channel hot sir supply anti/de-icing test technology was constructed, moreover, the dual-channel hot sir supply anti/de-icing test of a small aero-engine inlet was carried out. The test results indicated that the hot air supply anti/de-icing test system can simulate the hot air from the real compressor, allowing for multi-channel hot air supply test. The temperature control accuracy can reach ±1 ℃ and the flow control accuracy can reach ±1%. Meanwhile, it can provide a strong support for the anti/de-icing test system design and airworthiness certification of aircraft in China.
| [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.
|
| [2] |
易贤,李维浩,王应宇,等. 飞机结冰传感器安装位置确定方法[J]. 实验流体力学,2018,32(2): 48-54. YI Xian,LI Weihao,WANG Yingyu,et al. Method of determining the location for aircraft icing prober[J]. Journal of Experiments in Fluid Mechanics,2018,32(2): 48-54. (in Chinese
YI Xian, LI Weihao, WANG Yingyu, et al. Method of determining the location for aircraft icing prober[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(2): 48-54. (in Chinese)
|
| [3] |
雷桂林,郑梅,董威,等. 积冰密度对机翼除冰过程影响的数值研究[J]. 空气动力学学报,2018,36(6): 958-965. LEI Guilin,ZHENG Mei,DONG Wei,et al. Numerical investigation of ice density effects on airfoil de-icing process[J]. Acta Aerodynamica Sinica,2018,36(6): 958-965. (in Chinese
LEI Guilin, ZHENG Mei, DONG Wei, et al. Numerical investigation of ice density effects on airfoil de-icing process[J]. Acta Aerodynamica Sinica, 2018, 36(6): 958-965. (in Chinese)
|
| [4] |
CAO Yihua,TAN Wenyuan,WU Zhenlong. Aircraft icing: an ongoing threat to aviation safety[J]. Aerospace Science and Technology,2018,75: 353-385. doi: 10.1016/j.ast.2017.12.028
|
| [5] |
王华阁. 航空发动机设计手册:第16册 空气系统及传热分析[M]. 北京: 航空工业出版,2001.
|
| [6] |
冯丽娟,李冬,易贤. 民用航空发动机进气道防冰系统设计方法研究[J]. 航空工程进展,2017,8(3): 335-341. FENG Lijuan,LI Dong,YI Xian. Civil aero-engine inlet anti-icing system power requirement definition methodology investigation[J]. Advances in Aeronautical Science and Engineering,2017,8(3): 335-341. (in Chinese
FENG Lijuan, LI Dong, YI Xian. Civil aero-engine inlet anti-icing system power requirement definition methodology investigation[J]. Advances in Aeronautical Science and Engineering, 2017, 8(3): 335-341. (in Chinese)
|
| [7] |
常士楠,杨波,冷梦尧,等. 飞机热气防冰系统研究[J]. 航空动力学报,2017,32(5): 1025-1034. CHANG Shinan,YANG Bo,LENG Mengyao,et al. Study on bleed air anti-icing system of aircraft[J]. Journal of Aerospace Power,2017,32(5): 1025-1034. (in Chinese
CHANG Shinan, YANG Bo, LENG Mengyao, et al. Study on bleed air anti-icing system of aircraft[J]. Journal of Aerospace Power, 2017, 32(5): 1025-1034. (in Chinese)
|
| [8] |
倪章松,刘森云,张军,等. 环境参数对飞机防冰热载荷的影响规律[J]. 航空动力学报,2021,36(1): 8-14. NI Zhangsong,LIU Senyun,ZHANG Jun,et al. Influnce of environment parameters on anti-icing heat load for aircraft[J]. Journal of Aerospace Power,2021,36(1): 8-14. (in Chinese
NI Zhangsong, LIU Senyun, ZHANG Jun, et al. Influnce of environment parameters on anti-icing heat load for aircraft[J]. Journal of Aerospace Power, 2021, 36(1): 8-14. (in Chinese)
|
| [9] |
陆林杰. 飞机结冰影响与除防冰技术综述[J]. 科技创新与应用,2020(16): 136-138.
|
| [10] |
YEOMAN K. Efficiency of a bleed air powered inlet icing protective system[R]. AIAA 94-0717,1994.
|
| [11] |
PAPADAKIS M,WONG S H,YEONG H W,et al. Icing tests of a wing model with a hot-air ice protection system[R]. AIAA-2010-7833,2010.
|
| [12] |
GRAY V H,GLAHN U. Effect of ice and frost formations on drag of NACA 65(sub 1)-212 airfoil for various modes of thermal ice protection[R]. NACA TN-2962,1953.
|
| [13] |
PAPADAKIS M,RODRIGUEZ A O Z,DOMINGOS R H. Experimental and computer model results for a bleed air ice protection system[R]. SAE Technical Paper 2011-38-0034,2011.
|
| [14] |
WHALEN E A,BROEREN A P,BRAGG M B,et al. Characteristics of runback ice accretions on airfoils and their aerodynamic effects[R]. AIAA-2005-1065,2005.
|
| [15] |
PAPADAKIS M,WONG S H,YEONG H W,et al. Experimental investigation of a bleed air ice protection system[R]. SAE Technical Paper 2007-01-3313,2007.
|
| [16] |
裘燮纲,韩凤华. 飞机防冰系统[M]. 北京: 航空专业教材编审组,2004.
|
| [17] |
倪章松,刘森云,王桥,等. 3 m×2 m结冰风洞试验技术研究进展[J]. 实验流体力学,2019,33(6): 46-53. NI Zhangsong,LIU Senyun,WANG Qiao,et al. Research progress of test technologies for 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2019,33(6): 46-53. (in Chinese
NI Zhangsong, LIU Senyun, WANG Qiao, et al. Research progress of test technologies for 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(6): 46-53. (in Chinese)
|
| [18] |
王梓旭,沈浩,郭龙,等. 3 m×2 m结冰风洞云雾参数校测方法[J]. 实验流体力学,2018,32(2): 61-67. WANG Zixu,SHEN Hao,GUO Long,et al. Cloud calibration method of 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2018,32(2): 61-67. (in Chinese
WANG Zixu, SHEN Hao, GUO Long, et al. Cloud calibration method of 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(2): 61-67. (in Chinese)
|
| [19] |
郭向东,张平涛,赵照,等. 大型结冰风洞云雾场适航应用符合性验证[J]. 航空学报,2020,41(10): 205-219. GUO Xiangdong,ZHANG Pingtao,ZHAO Zhao,et al. Airworthiness application compliance verification of cloud flowfield in large icing wind tunnel[J]. Acta Aeronautica et Astronautica Sinica,2020,41(10): 205-219. (in Chinese
GUO Xiangdong, ZHANG Pingtao, ZHAO Zhao, et al. Airworthiness application compliance verification of cloud flowfield in large icing wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10): 205-219. (in Chinese)
|
| [20] |
胡卜元,黄勇,章贵川,等. 低速TPS试验内式流量控制技术研究[J]. 实验流体力学,2019,33(6): 54-58. HU Buyuan,HUANG Yong,ZHANG Guichuan,et al. Internal mass flow control technology of low speed TPS tests[J]. Journal of Experiments in Fluid Mechanics,2019,33(6): 54-58. (in Chinese
HU Buyuan, HUANG Yong, ZHANG Guichuan, et al. Internal mass flow control technology of low speed TPS tests[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(6): 54-58. (in Chinese)
|
DownLoad:
