气膜孔视觉测量系统的设计与搭建

毕超,郝雪,刘孟晨,房建国

计量学报 ›› 2020, Vol. 41 ›› Issue (7) : 775-780.

PDF(1671 KB)
PDF(1671 KB)
计量学报 ›› 2020, Vol. 41 ›› Issue (7) : 775-780. DOI: 10.3969/j.issn.1000-1158.2020.07.02
几何量计量

气膜孔视觉测量系统的设计与搭建

  • 毕超,郝雪,刘孟晨,房建国
作者信息 +

Design and Establishment of the Machine VisionMeasuring System for Film Cooling Holes

  • BI Chao,HAO Xue,LIU Meng-chen,FANG Jian-guo
Author information +
文章历史 +

摘要

为了重建高压涡轮导向叶片气膜孔的三维形貌特征,基于机器视觉原理,设计并搭建了非接触式的气膜孔四轴视觉测量系统。该系统主要由三坐标测量机框架、高精度回转台、叶片专用夹具和图像采集装置构成,将视觉测量技术和三坐标测量技术结合起来以应对气膜孔的检测问题。为了获取气膜孔的三维形貌数据,提出了应用景深合成技术进行孔壁三维形貌重建的方法,并通过实验进行了重建方法的验证。在实验过程中,应用该测量系统对某个高压涡轮导向叶片上的气膜孔特征进行了测量实验,获取了孔深范围内的对焦图像序列,而后对其进行了景深合成与深度信息转化,最终实现了该气膜孔的孔壁形貌的三维重建与显示,并实现了向三维点云数据的转化,充分说明了所搭建的气膜孔视觉测量系统的有效性。

Abstract

In order to reconstruct the 3D shape characters of the film cooling holes of the high-pressure turbine blade, a non-contact machine vision measuring system with four motion axes is designed and then established. Composed of the frame of a coordinate measuring machine (CMM), a high precision turntable, special fixture of blades and image acquisition device etc, the system could combine the advanced vision detection and traditional coordinate measurement together to cope with the inspecting difficulties of the film cooling holes. To derive the 3D shape data of the film cooling holes, the method of depth from focus (DFF) is applied to realize the 3D reconstruction of the shape of the hole wall, which is verified by the follow-up experiment. In the experimental procedure, a film cooling hole of a high-pressure turbine blade is selected and inspected by the machine vision measuring system. With the focus image stack derived within the depth of the film cooling hole, the 3D shape characteristics of the hole is reconstructed by the method of DFF and then converted to the depth information, which could be employed to display the morphology of the hole wall and converted to the 3D data cloud. Therefore, the experimental results show the effectiveness of the vision measuring system for film cooling holes established.

关键词

计量学 / 气膜孔 / 三维形貌 / 视觉测量 / 航空发动机 / 非接触

Key words

metrology / film cooling hole / 3D shape / vision measurement / aero engine / non-contact

引用本文

导出引用
毕超,郝雪,刘孟晨,房建国. 气膜孔视觉测量系统的设计与搭建[J]. 计量学报. 2020, 41(7): 775-780 https://doi.org/10.3969/j.issn.1000-1158.2020.07.02
BI Chao,HAO Xue,LIU Meng-chen,FANG Jian-guo. Design and Establishment of the Machine VisionMeasuring System for Film Cooling Holes[J]. Acta Metrologica Sinica. 2020, 41(7): 775-780 https://doi.org/10.3969/j.issn.1000-1158.2020.07.02
中图分类号: TB92   

参考文献

[1]梁春华, 王鸣, 刘殿春. 战斗机发动机涡轮叶片层板发散冷却技术的发展 [J]. 航空制造技术, 2013, (9): 90-93.
Liang C H, Wang M, Liu D C. Development of laminated transpiration-cooled turbine blade for fighter engine [J]. [WTBX][STBX]Aeronautical Manufacturing Technology[STBZ][WTBZ], 2013, (9): 90-93.
[2]张文武, 郭春海, 张天润, 等. 涡轮叶片先进气膜冷却与相关激光打孔技术进展 [J]. 航空制造技术, 2016, 59(22): 26-31.
Zhang W W, Guo C H, Zhang T R, et al. Advanced Film Cooling Technology of Turbine Blades and Progress in Relevant Laser Drilling Technology [J]. [WTBX][STBX]Aeronautical Manufacturing Technology[STBZ][WTBZ], 2016, 59(22): 26-31.
[3]董一巍, 吴宗璞, 李效基, 等. 叶片气膜孔加工与测量技术的现状及发展趋势 [J]. 航空制造技术, 2018, 61(13): 16-25.
Dong Y W, Wu Z P, Li X J, et al. Current situation and development trend of processing and measurement technology for turbine blade film cooling hole [J]. [WTBX][STBX]Aeronautical Manufacturing Technology[STBZ][WTBZ], 2018, 61(13): 16-25.
[4]Davdas S, Tom E, Claudio C, et al. New approach to the inspection of cooling holes in aero-engine [J]. [WTBX][STBX]Optics and Lasers in Engineering[STBZ][WTBZ], 2009, 47: 686-694.
[5]张望先, 仲思东, 隋莉斌, 等. 基于三坐标测量机的大尺寸非接触测量 [J]. 武汉大学学报(工学版), 2004, 37(5): 112-115.
Zhang W X, Zhong S D, Sui L B, et al. Nocontact measurement of big dimension object based on coordinate measuring machine [J]. [WTBX][STBX]Engineering Journal of Wuhan University[STBZ][WTBZ], 2004, 37(5): 112-115.
[6]郭继平, 于冀平, 彭翔, 等. 无限变焦3D形貌仪在几何量微纳米检测中的应用 [J]. 计量学报, 2012, 33(5A): 36-40.
Guo J P, Yu J P, Peng X, et al. Variation in dimensional Micro-nano measurement [J]. [WTBX][STBX]Acta Metrologica Sinica[STBZ][WTBZ], 2012, 33(5A): 36-40.
[7]王呈, 刘涛, 穆轩, 等. 航空发动机叶片气膜孔测量技术研究 [J]. 计测技术, 2012, 32(5): 27-30.
Wang C, Liu T, Mu X, et al. Research on aero engine blade film hole measuring technology [J]. [WTBX][STBX]Metrology & Measurement Technology[STBZ][WTBZ], 2012, 32(5): 27-30.
[8]关军, 王呈. 建立叶片气膜孔工件坐标系的方法研究 [J]. 计测技术, 2013, 33(3): 41-43.
Guan J, Wang C. Study on establishing coordinate system for workpiece of blade gas film holes [J]. [WTBX][STBX]Metrology & Measurement Technology[STBZ][WTBZ], 2013, 33(3): 41-43.
[9]鲍晨兴, 王磊, 李凯, 等. 基于CCD的叶片气膜孔快速检测技术研究 [J]. 航空精密制造技术, 2017, 53(2): 52-55.
Bao C X, Wang L, Li K, et al. Research on rapid detection technology of gas film hole based on CCD [J]. [WTBX][STBX]Aviation Precision Manufacturing Technology[STBZ][WTBZ], 2017, 53(2): 52-55.
[10]隋鑫, 徐熙平, 孙健, 等. 应用多传感器技术测量微孔几何参量 [J]. 光学与光电技术, 2009, 7(4): 79-82.
Sui X, Xu X P, Sun J, et al. Microhole geometry measurement applying Multi-sensor technology [J]. [WTBX][STBX]Optics & Optoelectronic Technology[STBZ][WTBZ], 2009, 7(4): 79-82.
[11]蒋睿嵩, 汪文虎, 王增强, 等. 航空发动机涡轮叶片精密成形技术及其发展趋势 [J]. 航空制造技术, 2016, 59(21): 57-62.
Jiang R C, Wang W H, Wang Z Q, et al. Precision forming technology and its development trend of aeroengine turbine blade [J]. [WTBX][STBX] Aeronautical Manufactur-ing Technology[STBZ][WTBZ], 2016, 59(21): 57-62..
[12]王执范, 姚四伟. 涡轮第一级导向叶片的气膜冷却仿真 [J]. 西安航空学院学报, 2015, 33(1): 3-8.
Wang Z F, Yao S W. Discussion on the application of digital assembly technique of aircrafts [J]. [WTBX][STBX]Journal of Xian Aeronautical university[STBZ][WTBZ], 2015, 33(1): 3-8.
[13]Cheng H L, Rock A P, Lan J, et al. Real-time depth measurement for micro-holes drilled by lasers [J]. [WTBX][STBX]Measurement Science and Technology[STBZ][WTBZ], 2010, 21(2): 1-6.
[14]毕超, 吕来鹏, 房建国, 等. 光学坐标测量机的搭建与实现 [J]. 宇航计测技术, 2015, 35(4): 19-23.
Bi C, Lü L P, Fang J G, et al. Establishment and realization of the optical coordinate measuring machine [J]. [WTBX][STBX]Journal of Astronautic Metrology and Measure-ment[STBZ][WTBZ], 2015, 35(4): 19-23.

基金

国家科技重大专项(2018ZX04004001)

PDF(1671 KB)

Accesses

Citation

Detail

段落导航
相关文章

/