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主起落架是大型飞机重要的部件,其结构和载荷都十分复杂。为对主起落架进行详细的应力分析,本文不但提出一种整体制作主起落架三维光弹性模型的方法;而且将应变片电测技术应用于光弹性模型上,成功地为主起落架关键部件——活塞杆进行了方案的优化,并使其最大应力下降了40%;同时提出一种载波计算机自动测量边界应力的方法。以上说明,对主起落架等复杂而重要的结构,实验应力分析方法是一种优化设计的有效工具。 相似文献
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飞机起落架着陆与滑跑性能分析 总被引:3,自引:0,他引:3
阐述了一个能准确模拟飞机着陆与滑跑冲击特性的起落架分析模型,并通过落震试验的真实载荷-行程与该模型模拟计算结果的对比,显示了这种模型的有效性.为起落架设计与改进设计提供了一个实用的工程方法. 相似文献
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Landing gear noise control using perforated fairings 总被引:2,自引:0,他引:2
K. Boorsma X. Zhang N. Molin 《Acta Mechanica Sinica》2010,26(2):159-174
Landing gears of commercial aircraft make an important contribution to total aircraft noise in the approach configuration. Using fairings to shield components from high speed impingement reduces noise. Furthermore, perforating these fairings has been confirmed by flight tests to further enable noise reduction. Following an earlier fundamental study of the application of perforated fairings, a study has been performed to investigate and optimize the benefits of bleeding air through landing gear fairings. By means of wind tunnel tests, an aerodynamic and acoustic survey has been performed on a simplified generic main landing gear to explore the influence of (perforated) fairings on the lower part of the gear. The results show that for this specific case, the application of impermeable fairings reduces noise in the mid- and high frequency range by shielding sharp edged components from high velocity impingement. However, below 1 kHz the noise is shown to increase significantly. Application of the perforations is shown to diminish this low frequency increase whilst maintaining the reduction in the mid- and high frequency range. The aerodynamic and acoustic measurements point in the direction of the separated flow of the fairings interacting with the downstream gear components responsible for the low frequency noise increase. Bleeding of the air through the fairings reduces the large scale turbulence in the proximity of these components and hence diminishes the low frequency noise increase. 相似文献
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在飞机起降过程中,起落架噪声作为主要的机体噪声,越来越受到广泛的关注。串列双圆柱绕流是飞机起落架的简化模型,能够体现起落架复杂流动现象以及气动噪声的主要特征。本文采用基于SST湍流模型的自适应尺度模拟方法(SST-SAS),结合FW-H(Ffowcs Williams-Hawkings)方程的数值计算方法研究了来流雷诺数为1.66×105且两圆柱圆心之间的距离与圆柱直径之比为3.7的串列双圆柱绕流的流动特征和声场特性。将结果与已有文献中的数据作了详细地比较,二者吻合很好,平均误差在5%以内。验证了本文气动声学数值计算方法对高雷诺数下大分离流动模拟的可靠性和有效性。 相似文献
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