Research on pressure measuring device installation at AIP of inlet

Zhang Xiaofei; Jiang Jian; Tian Xiaoping; Fu Xiaogang

doi:10.11729/syltlx20150147

Volume 30 Issue 5

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Journal of Experiments in Fluid Mechanics > 2016 > 30(5): 80-87. > DOI: 10.11729/syltlx20150147

Zhang Xiaofei, Jiang Jian, Tian Xiaoping, Fu Xiaogang. Research on pressure measuring device installation at AIP of inlet[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(5): 80-87. DOI: 10.11729/syltlx20150147

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Research on pressure measuring device installation at AIP of inlet

Engine Department, Chinese Flight Test Establishment, Xi'an 710089, China

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Received Date: December 16, 2015
Revised Date: May 06, 2016

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Abstract

Abstract

To discuss the transition part deformation of installing test equipment at AIP during inlet/engine compatibility flight tests, an evaluation index of transition part radial deformation is developed and applied in engineering calculation. Moreover, influences of perforating, installing static pressure base and total pressure test rake on the radial size of the transition part are compared and analyzed. Accordingly, it is indicated that installing pressure test device at AIP may force the radial size to deviate from the designed value and standard circle; welding static pressure test base may introduce obvious deformation while riveting may introduce less deformation relatively; restricting on both sides of the total pressure test rake may not seriously influence the radial size whereas effectively restrain its vibration amplitude. The optimized installation scheme of the pressure measuring device has been adopted in engineering.
- inlet/engine compatibility,
- total pressure test rake,
- static pressure probe base,
- pressure measuring device,
- deformation,
- flight test

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[1]	和永进, 史建邦, 邢雁, 等.某型飞机进气道测量耙研制[J].燃气涡轮试验与研究, 2008:21(3):59-62. http://www.cnki.com.cn/Article/CJFDTOTAL-RQWL200803016.htm He Y J, Shi J B, Xing Y, et al. Development of intake measurement rake for an aircraft[J]. Gas Turbine Experiment and Research, 2008:21(3):59-62. http://www.cnki.com.cn/Article/CJFDTOTAL-RQWL200803016.htm
[2]	马燕荣.空气流量组合测量耙的研制及试验[J].燃气涡轮试验与研究, 2014, 27(3):54-59. http://www.cnki.com.cn/Article/CJFDTOTAL-RQWL201403013.htm Ma Y R. Development and experiment of jointed rake for airflow and boundary-layer measurement[J]. Gas Turbine Experiment and Research, 2014, 27(3):54-59. http://www.cnki.com.cn/Article/CJFDTOTAL-RQWL201403013.htm
[3]	Yuhas A J, Ray R J, Burley R R, et al. Design and development of an F/A-18 inlet distortion rake:a cost and time saving solution[R]. NASA TM-4722, 1995.
[4]	汪涛, 姜健, 史建邦.进气道/发动机相容性试飞总压畸变的采集与处理[J].燃气涡轮试验与研究, 2012, 25(2):54-58. http://www.cnki.com.cn/Article/CJFDTOTAL-RQWL201202014.htm Wang T, Jiang J, Shi J B. Acquisition and processing of total pressure distortion data in inlet/engine compatibility flight test[J]. Gas Turbine Experiment and Research, 2012, 25(2):54-58. http://www.cnki.com.cn/Article/CJFDTOTAL-RQWL201202014.htm
[5]	张福渊, 离绍建, 萧亮壮, 等.概率统计及随机过程[M].北京:北京航空航天大学出版社, 2000. Zhang F Y, Li S J, Xiao L Z, et al. Probability and Stochastic Processes[M]. Beijing:Beihang University Press, 2000.
[6]	刘大响, 叶培梁, 胡俊, 等.航空燃气涡轮发动机稳定性设计与评定技术[M].北京:航空工业出版社, 2004.Liu D X, Ye P L, Hu J, et al. Stability design and evaluation technology for aero gas turbine engine[M]. Beijing:Aviation Industry Press, 2004.
[7]	李庆扬, 王能超, 易大义.数值分析[M].武汉:华中科技大学出版社, 2006. Li Q Y, Wang N C, Yi D Y. Numerical analysis[M]. Wuhan:Huazhong University of Science & Technology Press, 2006.
[8]	徐士良. FORTRAN常用算法程序集[M].北京:清华大学出版社, 1992. Xu S L. FORTRAN common program algorithm set[M]. Beijing:Tsinghua University Press, 1992.
[9]	王会峰, 刘上乾, 汪大宝, 等.三次样条插值在变径内腔重建中的应用[J].中北大学学报(自然科学版), 2010, 31(1):65-70. http://www.cnki.com.cn/Article/CJFDTOTAL-HBGG201001013.htm Wang H F, Liu S Q, Wang D B, et al. Application of cubic spline interpolation to variable-diameter lumen surface reconstruction[J]. Journal of North University of China(Natural Science Edition), 2010, 31(1):65-70. http://www.cnki.com.cn/Article/CJFDTOTAL-HBGG201001013.htm
[10]	付永生, 李颉.大尺寸立式钢制筒体焊接变形研究[J].黑龙江电力, 2012, 34(1):65-67. http://www.cnki.com.cn/Article/CJFDTOTAL-HEIL201201017.htm Fu Y S, Li J. Study on welding distortions for large-size vertical steel tank[J]. Heilongjiang Electric Power, 2012, 34(1):65-67. http://www.cnki.com.cn/Article/CJFDTOTAL-HEIL201201017.htm
[11]	李良碧, 万正权, 王自力, 等.环肋圆柱壳结构焊接残余应力和变形的数值模拟[J].焊接技术, 2011, 40(3):9-12. http://www.cnki.com.cn/Article/CJFDTOTAL-HSJJ201103004.htm Li L B, Wan Z Q, Wang Z L, et al. Numerical simulation on welding residual stresses and deformation of ring-stiffened circular cylindrical shell[J]. Welding Technology, 2011, 40(3):9-12. http://www.cnki.com.cn/Article/CJFDTOTAL-HSJJ201103004.htm
[12]	Zhang K F, Cheng H, Li Y. Riveting process modeling and simulating for deformation analysis of aircraft's thin-walled sheet-metal parts[J]. Chinese Journal of Aeronautics, 2011, 24(3):369-377. DOI: 10.1016/S1000-9361(11)60044-7
[13]	冯晓, 谢兰生.铆接变形的有限元分析[J].机械制造与自动化, 2009, 22(2):62-63, 80. http://www.cnki.com.cn/Article/CJFDTOTAL-ZZHD200902022.htm Feng X, Xie L S. Rivet deformation and finite element analysis[J]. Machine Building & Automation, 2009, 22(2):62-63, 80. http://www.cnki.com.cn/Article/CJFDTOTAL-ZZHD200902022.htm
[14]	冯伟干, 张建华, 朱元夫.圆筒形铆接结构中铆钉的数值模拟[J].强度与环境, 2010, 37(1):30-34. http://www.cnki.com.cn/Article/CJFDTOTAL-QDHJ201001007.htm Feng W G, Zhang J H, Zhu Y F. The numerical simulation of rivet in riveted joint cylindric structure[J]. Structure & Environment Engineering, 2010, 37(1):30-34. http://www.cnki.com.cn/Article/CJFDTOTAL-QDHJ201001007.htm

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