| Citation: | WEI Longtao, ZUO Chenglin, GUO Xiangdong, et al. Application of 3D ice shape laser measurement technology in icing wind tunnel[J]. Journal of Aerospace Power, 2024, 39(11):20220958 doi: 10.13224/j.cnki.jasp.20220958 |
The principle of measuring 3D structure for ice accretion in icing wind tunnel with ROMER measuring instrument was introduced, and a fast reconstruction method for model with ice shape was proposed. Typical rime ice, rough ice and horned ice were obtained by wind tunnel test. The 3D morphology of ice accretion was measured by ROMER instrument, and the 3D data of ice accretion on the surface of the model were obtained. The results showed that 3D results of rime ice were highly consistent with the actual ice shape, and the detailed characteristics of ice accumulation can be accurately measured. 3D scanning technology can measure the rough ice results which can not be obtained by hot knife method. Compared with the ice trajectory of the shorn ice obtained by the hot knife method, the ice trajectory of the 3D ice shape in the same section had the same icing range and icing level, with the average thickness deviation of ice up to 2.5 mm.
| [1] |
LYNCH F T,KHODADOUST A. Effects of ice accretions on aircraft aerodynamics[J]. Progress in Aerospace Sciences,2001,37(8): 669-767. doi: 10.1016/S0376-0421(01)00018-5
|
| [2] |
范洁川,于涛. 飞机结冰风洞试验模拟研究[J]. 实验流体力学,2007,21(1): 68-72,92. FAN Jiechuan,YU Tao. A study of simulation for airplane icing tests in icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2007,21(1): 68-72,92. (in Chinese doi: 10.3969/j.issn.1672-9897.2007.01.014
FAN Jiechuan, YU Tao. A study of simulation for airplane icing tests in icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2007, 21(1): 68-72, 92. (in Chinese) doi: 10.3969/j.issn.1672-9897.2007.01.014
|
| [3] |
KIND R J,POTAPCZUK M G,FEO A,et al. Experimental and computational simulation of in-flight icing phenomena[J]. Progress in Aerospace Sciences,1998,34(5/6): 257-345.
|
| [4] |
易贤. 飞机积冰的数值计算与积冰试验相似准则研究[D]. 四川 绵阳: 中国空气动力研究与发展中心,2007. YI Xian. Numerical computation of aircraft icing and study on icing test scaling law[D]. Mianyang Sichuan: China Aerodynamics Research and Development Center,2007. (in Chinese
YI Xian. Numerical computation of aircraft icing and study on icing test scaling law[D]. Mianyang Sichuan: China Aerodynamics Research and Development Center, 2007. (in Chinese)
|
| [5] |
郭向东,胡站伟,丁亮,等. 大型结冰风洞中冰晶热/力平衡特性数值研究[J]. 航空动力学报,2022,37(3): 478-491. GUO Xiangdong,HU Zhanwei,DING Liang,et al. Numerical investigation of thermal and mechanical equilibrium characteristics of ice crystal in large icing wind tunnel[J]. Journal of Aerospace Power,2022,37(3): 478-491. (in Chinese
GUO Xiangdong, HU Zhanwei, DING Liang, et al. Numerical investigation of thermal and mechanical equilibrium characteristics of ice crystal in large icing wind tunnel[J]. Journal of Aerospace Power, 2022, 37(3): 478-491. (in Chinese)
|
| [6] |
王斌,刘桂华,张利萍,等. 基于线结构光的冰横截面轮廓测量[J]. 实验流体力学,2016,30(3): 14-20. WANG Bin,LIU Guihua,ZHANG Liping,et al. Ice cross sectional profile measurement based on line structured light[J]. Journal of Experiments in Fluid Mechanics,2016,30(3): 14-20. (in Chinese doi: 10.11729/syltlx20160040
WANG Bin, LIU Guihua, ZHANG Liping, et al. Ice cross sectional profile measurement based on line structured light[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(3): 14-20. (in Chinese) doi: 10.11729/syltlx20160040
|
| [7] |
郭龙,秦三春,李强,等. 基于机器视觉的飞机模型冰形轮廓提取方法研究[J]. 自动化与仪器仪表,2020(6): 15-20. GUO Long,QIN Sanchun,LI Qiang,et al. Research on ice contour extraction of aircraft model based on machine vision[J]. Automation & Instrumentation,2020(6): 15-20. (in Chinese
GUO Long, QIN Sanchun, LI Qiang, et al. Research on ice contour extraction of aircraft model based on machine vision[J]. Automation & Instrumentation, 2020(6): 15-20. (in Chinese)
|
| [8] |
康含玉,刘桂华,王斌,等. 冰形表面激光光带中心线快速提取方法[J]. 实验流体力学,2017,31(5): 81-87. KANG Hanyu,LIU Guihua,WANG Bin,et al. A fast method of extracting the laser light bar’s centerline in the ice model[J]. Journal of Experiments in Fluid Mechanics,2017,31(5): 81-87. (in Chinese doi: 10.11729/syltlx20170058
KANG Hanyu, LIU Guihua, WANG Bin, et al. A fast method of extracting the laser light bar’s centerline in the ice model[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(5): 81-87. (in Chinese) doi: 10.11729/syltlx20170058
|
| [9] |
柳庆林,倪章松,张平涛,等. 低温环境下复杂冰形快速三维测量技术[J]. 光学技术,2020,46(6): 641-646. LIU Qinglin,NI Zhangsong,ZHANG Pingtao,et al. Fast 3D measurement technology of complex ice shape in low temperature environment[J]. Optical Technique,2020,46(6): 641-646. (in Chinese
LIU Qinglin, NI Zhangsong, ZHANG Pingtao, et al. Fast 3D measurement technology of complex ice shape in low temperature environment[J]. Optical Technique, 2020, 46(6): 641-646. (in Chinese)
|
| [10] |
李伟斌,易贤,杜雁霞,等. 基于变分分割模型的结冰冰形测量方法[J]. 航空学报,2017,38(1): 120167. LI Weibin,YI Xian,DU Yanxia,et al. A measurement approach for ice shape based on variational segmentation model[J]. Acta Aeronautica et Astronautica Sinica,2017,38(1): 120167. (in Chinese
LI Weibin, YI Xian, DU Yanxia, et al. A measurement approach for ice shape based on variational segmentation model[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(1): 120167. (in Chinese)
|
| [11] |
郭龙,马军,李明,等. 基于三维扫描技术的结冰风洞冰形非接触测量研究[J]. 中国测试,2018,44(9): 18-22. GUO Long,MA Jun,LI Ming,et al. Non-contact measurement of ice shape in icing wind tunnel based on 3D scanning technology[J]. China Measurement & Test,2018,44(9): 18-22. (in Chinese doi: 10.11857/j.issn.1674-5124.2018.09.004
GUO Long, MA Jun, LI Ming, et al. Non-contact measurement of ice shape in icing wind tunnel based on 3D scanning technology[J]. China Measurement & Test, 2018, 44(9): 18-22. (in Chinese) doi: 10.11857/j.issn.1674-5124.2018.09.004
|
| [12] |
易贤,王斌,李伟斌,等. 飞机结冰冰形测量方法研究进展[J]. 航空学报,2017,38(2): 520711. YI Xian,WANG Bin,LI Weibin,et al. Research progress on ice shape measurement approaches for aircraft icing[J]. Acta Aeronautica et Astronautica Sinica,2017,38(2): 520711. (in Chinese
YI Xian, WANG Bin, LI Weibin, et al. Research progress on ice shape measurement approaches for aircraft icing[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(2): 520711. (in Chinese)
|
| [13] |
郭向东,柳庆林,赖庆仁,等. 大型结冰风洞气流场适航符合性验证[J]. 空气动力学学报,2021,39(2): 184-195. GUO Xiangdong,LIU Qinglin,LAI Qingren,et al. Airworthiness compliance verification of aerodynamic flowfield of a large-scale icing wind tunnel[J]. Acta Aerodynamica Sinica,2021,39(2): 184-195. (in Chinese doi: 10.7638/kqdlxxb-2019.0086
GUO Xiangdong, LIU Qinglin, LAI Qingren, et al. Airworthiness compliance verification of aerodynamic flowfield of a large-scale icing wind tunnel[J]. Acta Aerodynamica Sinica, 2021, 39(2): 184-195. (in Chinese) doi: 10.7638/kqdlxxb-2019.0086
|
| [14] |
郭向东,张平涛,张珂,等. 3 m×2 m结冰风洞热流场品质提高及评估[J]. 实验流体力学,2021,35(4): 41-51. GUO Xiangdong,ZHANG Pingtao,ZHANG Ke,et al. Improvement and evaluation of thermal flow-field quality in CARDC icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2021,35(4): 41-51. (in Chinese doi: 10.11729/syltlx20200118
GUO Xiangdong, ZHANG Pingtao, ZHANG Ke, et al. Improvement and evaluation of thermal flow-field quality in CARDC icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(4): 41-51. (in Chinese) doi: 10.11729/syltlx20200118
|
| [15] |
郭向东,张平涛,赵献礼,等. 大型结冰风洞热流场符合性验证[J]. 实验流体力学,2020,34(5): 79-88. GUO Xiangdong,ZHANG Pingtao,ZHAO Xianli,et al. The compliance verification of thermodynamic flowfield in the large icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2020,34(5): 79-88. (in Chinese doi: 10.11729/syltlx20190113
GUO Xiangdong, ZHANG Pingtao, ZHAO Xianli, et al. The compliance verification of thermodynamic flowfield in the large icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(5): 79-88. (in Chinese) doi: 10.11729/syltlx20190113
|
| [16] |
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 doi: 10.11729/syltlx20180115
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) doi: 10.11729/syltlx20180115
|
| [17] |
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 doi: 10.11729/syltlx20170163
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) doi: 10.11729/syltlx20170163
|
| [18] |
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): 123879. 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): 123879. (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): 123879. (in Chinese)
|
| [19] |
LEE S,BROEREN A P,ADDY H E,et al. Development of 3D ice accretion measurement method[C]// 4th AIAA Atmospheric and Space Environments Conference. New Orleans, Louisiana, US: AIAA,2012: 1-17.
|
| [20] |
LEE S,BROEREN A P,KREEGER R E,et al. Implementation and validation of 3-D ice accretion measurement methodology[R]. AIAA 2014-2613,2014.
|