| 翼型测力天平的研制 |
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| 引用本文： | 李勇,赵长辉,李国文,王为铭.翼型测力天平的研制[J].气动实验与测量控制,2012(3):107-110. |
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| 作者姓名： | 李勇 赵长辉 李国文 王为铭 |
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| 作者单位： | [1]中国航空工业空气动力研究院,沈阳110034 [2]沈阳航空航天大学,沈阳110136 |
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| 摘 要： | 为研究翼型结冰状态下的载荷变化规律，对翼型进行测力实验。研制一台三分量翼型测力天平。天平设计的突出难点为设计载荷极不匹配，阻力测量载荷很小。设计时，针对翼型载荷的特点，采用片梁组合方式测量阻力，四柱梁测量法向力及俯仰力矩，并采用有限元方法对结构进行了验证计算。主要介绍天平的设计、校准及应用情况。
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| 关 键 词： | 翼型结冰 测力天平 有限元法 天平设计 风洞实验 |
Design of force measurement balance for airfoil |
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| Authors: | LI Yong ZHAO Chang-huiI LI Guo-wen WANG Wei-ming |
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| Institution: | 1 (1. AVIC Aerodynamics Research Institute, Shenyang 110034, China; 2. Shenyang Aerospace University, Shenyang 110136, China) |
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| Abstract: | In order to study load change rule of airfoil in icing state, a force test is conducted by using a newly developed three-component force measurement balance. The greatest difficulty in the process of balance design is mismatch of design loads for the drag load is too small relatively. According to the load character of airfoil, sheet-beams are used to drag measurement, four column beams to measure normal force and pitch moment. Furthermore, a verification calculation is done by means of finite element method. The paper mainly introduces the design, calibration and application of the balance. |
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| Keywords: | icing airfoil force measurement balance finite element method balance design wind tunnel test |
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