Research on pressure measuring device installation at AIP of inlet
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摘要: 针对进气道/发动机相容性试飞中AIP上测量装置加装而引起过渡段变形问题,建立了过渡段径向形状变化评价指标并应用于工程计算,对比分析了过渡段上开孔、加装静压座、总压测量耙加装对过渡段径向尺寸的影响。结果表明:过渡段AIP面上加装测压装置使得过渡段径向尺寸偏离设计值及标准圆;焊接静压座会使过渡段径向尺寸发生较为明显变形,而铆接静压座则影响相对较小;总压测量耙采用两端约束的方案不会对过渡段径向尺寸造成较为严重的影响,但会有效地抑制测量耙的振动幅值。该结果已经应用于工程中,优化了测压装置加装方案。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.
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表 1 过渡段最终状态差异
Table 1. Final state difference among transition parts
过渡段 过渡段
状态测量耙
状态静压座
加装测量耙
加装过渡段A 上机件 上机件 焊接 螺母+
螺栓+
支撑环过渡段B 上机件 上机件 铆接 过渡段C 试验件 试验件 铆接 表 2 过渡段开孔前后变形指标计算结果
Table 2. Deformation index calculation results of transition part after being perforated
状态 Am/% δt/% Bm/% εt/% 原始状态(B) 0.022 0.022 0 0 开孔状态(B) 0.057 0.035 0.032 0.018 开孔状态(C) 0.109 0.059 0.087 0.041 表 3 加装静压座后变形指标计算结果
Table 3. Deformation index calculation results of transition part after installing static pressure probe base
状态 Am/% δt/% Bm/% εt/% 焊接状态(A) 0.387 0.201 0.401 0.201 铆接状态(B) 0.100 0.060 0.044 0.023 铆接状态(C) 0.244 0.126 0.203 0.118 表 4 过渡段变形评价指标变化(加装静压座)
Table 4. Deformation index changes after installing static pressure probe base
项目 ΔAm/% Δδt/% ΔBm/% Δεt/% 过渡段A +0.365 +0.179 +0.401 +0.201 过渡段B +0.043 +0.025 +0.012 +0.005 过渡段C +0.135 +0.067 +0.116 +0.077 表 5 总压测量耙加装后指标计算结果
Table 5. Deformation index calculation results of transition part after installing total pressure test rake
状态 Am/% δt/% Bm/% εt/% 装机状态(A) 0.554 0.332 0.561 0.332 装机状态(B) 0.089 0.050 0.046 0.024 装机状态(C) 0.227 0.135 0.228 0.129 中间状态(C)
(无静压座)0.172 0.086 0.135 0.069 表 6 过渡段变形评价指标变化(加装测量耙)
Table 6. deformation index changes after installing total pressure test rake
项目 ΔAm/% Δδt/% ΔBm/% Δεt/% 过渡段A +0.167 +0.131 +0.160 +0.131 过渡段B -0.011 -0.010 +0.002 +0.001 过渡段C -0.017 +0.009 +0.025 +0.011 过渡段C
(无静压座)+0.063 +0.027 +0.048 +0.028 表 7 过渡段变形评价指标变化(加装支撑环)
Table 7. Deformation index changes after installing support ring
项目 Am/% δt/% Bm/% εt/% 过渡段B -0.103 -0.037 -0.101 -0.050 过渡段C
(无静压座)+0.005 +0.003 -0.028 -0.010 表 8 测量耙扫频试验结果
Table 8. Sweep frequency results of the test rake sweep frequency
状态 固有频率/Hz 幅值/g 无支撑环 125 112.6 有支撑环 265 18.3 -
[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.htmHe 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.htmMa 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.htmWang 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.LiuD 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.htmWang 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.htmFu 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.htmLi 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.htmFeng 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.htmFeng 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