Load Measurement Scheme of Refueling Receptacles in Aerial Refueling Process and Ground Test Verification
-
摘要: 受油装置作为受油机的重要机构与加油设备建立输油通道,与加油设备对接过程中的载荷大小对于受油装置结构强度设计具有重要意义。本文根据受油装置结构形式,提出基于应变电测原理的受油装置对接载荷测量方法。在空中加油吊舱地面调试试验期间搭建可移动式测试系统,验证对接载荷测量思路及方法,获取了锥套与受油插头对接过程中受油管上的应变数据,分析了对接过程中的载荷变化规律,并结合受油管几何模型估算给出了对接过程中的轴向载荷大小,为后续空中加油过程对接载荷测量进行了原理及可行性验证。Abstract: Oil receiving device is an important mechanism of oil receiving machine and oil filling machine to establish oil transmission channel, its load magnitude during docking with refueling equipment is of great significance to structural strength design of refueling equipment. In this paper, according to the structure of oil receiving device, a method for measuring butt load of oil receiving device based on strain electrical measurement principle is proposed. A portable test system during ground debugging test of aerial refueling pod is built, and the idea and method of docking load measurement are verified. The strain data on the receiving pipe during the butting process between the cone sleeve and the receiving plug are obtained, the law of load variation in docking process is analyzed. Based on the geometric model of the receiving tubing, the axial load in the butting process is estimated, the principle and feasibility of docking load measurement for subsequent aerial refueling process are verified.
-
Key words:
- aerial refueling /
- load measurement /
- strain electrical measurement /
- ground test
-
表 1 不同对接速度下对接载荷计算结果
对接速度/(m·s−1) 0.3 0.6 0.9 1.2 对接载荷/N 3 186 3 259 3 287 4 011 -
[1] 罗志会. 飞机空中加油设备分析研究[J]. 航空科学技术, 2013,(6): 10-13 doi: 10.3969/j.issn.1007-5453.2013.06.004Luo Z H. Analysis and study of air refueling equipment for aircraft[J]. Aeronautical Science & Technology, 2013,(6): 10-13 (in Chinese) doi: 10.3969/j.issn.1007-5453.2013.06.004 [2] 中国人民解放军总装备部. GJB 67.3A-2008 军用飞机结构强度规范 第3部分: 其他载荷[S]. 北京: 中国人民解放军总装备部, 2008Equipment Development Department of People's Republic of China Central Military Commission. GJB67.3A-2008 Military airplane structural strength specification Part 3: Miscellaneous loads[S]. Beijing: Equipment Development Department of People's Republic of China Central Military Commission, 2008 (in Chinese) [3] GJB 2487-1995 飞机空中加油地面和飞行试验要求[S].北京: 中国航空工业总公司, 1995GJB2487-1995 Requirements, ground and flight tests, aircraft, refue lling in flight for[S]. Beijing: Aviation Industry Corporation of China, Ltd., 1995 (in Chinese) [4] 马世强. 中国空中加油技术发展之思考[J]. 中国海军, 2009,(4): 36-45Ma S Q. Development of PLA' s Air-to-air Refuelling Technology[J]. The Chinese PLA-Navy, 2009,(4): 36-45 (in Chinese) [5] J-10首次空中加油失败.受油锥管折断[Z/OL].(2012-07-15)[2013-10-23].http://v.youku.com/v-show/id_XNDI0MDg3ODQw.html (in Chinese)J-10 fails in the first aerial refueling test with the probe being broken[Z/OL]. (2012-07-15)[2013-10-23]. http://v.youku.com/v-show/id_XNDI0MDg3ODQw.html (in Chinese) [6] 张雷雨, 张洪, 杨洋, 等. 空中加油对接过程的动力学建模与仿真[J]. 航空学报, 2012, 33(7): 1347-1354Zhang L Y, Zhang H, Yang Y, et al. Dynamics modeling and simulation of docking process in aerial refueling[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(7): 1347-1354 (in Chinese) [7] 张雷雨, 杨洋, 张洪. 收放式受油装置对接过程的瞬态动力学分析[J]. 飞机设计, 2015, 35(2): 15-18, 25Zhang L Y, Yang Y, Zhang H. Impact behavior analysis of the retractable receptacle device during docking in aerial refueling[J]. Aircraft Design, 2015, 35(2): 15-18, 25 (in Chinese) [8] 刘东升. 固定式空中受油插头装置振动分析[J]. 飞机设计, 2006,(4): 7-10, 19 doi: 10.3969/j.issn.1673-4599.2006.04.002Liu D S. Analysis of vibration of fixed air refueling receptacles[J]. Aircraft Design, 2006,(4): 7-10, 19 (in Chinese) doi: 10.3969/j.issn.1673-4599.2006.04.002 [9] 罗乖林, 王宇. 空中受油管尾流特性研究[J]. 空气动力学报, 2002, 20(3): 367-372Luo G L, Wang Y. Study on the characteristics of flow around air refueling pipe[J]. Acta Aerodynamica Sinica, 2002, 20(3): 367-372 (in Chinese) [10] 彭珂, 周倩, 喻振华. 插头-锥管式空中加油系统加油过程载荷研究[J]. 航空科学技术, 2015, 26(7): 56-60 doi: 10.3969/j.issn.1007-5453.2015.07.013Peng K, Zhou Q, Yu Z H. Research on the loads of probe-and-drogue air refueling system[J]. Aeronautical Science & Technology, 2015, 26(7): 56-60 (in Chinese) doi: 10.3969/j.issn.1007-5453.2015.07.013 [11] Steven B L, Lewis F L. Aircraft control and simulation[M]. 2nd ed. Hoboken: John Wiley & Sons, 2003: 116-137 [12] Bloy A W, Khan M M. Modeling of the receiver aircraft in air-to-air refueling[J]. Journal of Aircraft, 2001, 38(2): 393-396 doi: 10.2514/2.2775 [13] Vachon M J, Ray R J, Walsh K R, et al. F/A-18 performance benefits measured during the autonomous formation flight project[R]. Edwards, California: National Aeronautics and Space Administration, Dryden Flight Research Center, 2003 [14] Markowich B. Omega air 707/F/A-18A-D aerial refueling ground and flight test evaluation and MA-3-1 coupling ground test evaluation[M]. NAWCADPAX/RTR-2000/206, 2001 [15] Omega air 707/F/A-18A-D aerial refueling ground and flight test evaluation and MA-3-1 coupling ground test evaluation. ARSAG Document No. 00-05-01 [16] 刘鸿文. 材料力学[M].北京: 人民教育出版社, 1979Liu H W. Mechanics of materials[M]. Beijing: People′s Education Press, 1979 (in Chinese) [17] 吴宗岱, 陶定祺. 应变电测原理及技术[M].北京: 国防工业出版社, 1982Wu Z D, Tao D Q. Principle and technology of strain measurement[M]. Beijing: National Defence Industry Press, 1982 (in Chinese)