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全机结构试验起落架位移补偿加载技术研究
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Research on Landing Gear Displacement Compensation Loading Technology of the Whole Structural Test
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    摘要:

    在全机结构试验中,通常采用起落架三点悬挂方式支持飞机,常规的支持装置为“撬杠-立柱”模式,该装置同时具备起落架垂向加载功能。在考核起落架连接区结构时,起落架在航向和侧向载荷作用下会产生一定变形,由于常规“撬杠-立柱”的撬杠支撑点固定,变形会引起垂向加载力线偏差,导致加载不准确。采用平面随动原理,将常规的撬杠固定支撑点改进为滚珠式随动平台,依靠随动平台的被动移动补偿起落架变形,减小垂向加载力线偏差。通过理论分析和试验验证,改进后的“随动撬杠-立柱”支持装置能够明显降低垂向加载误差,提高加载精度。

    Abstract:

    In the whole machine structure test, the aircraft is usually supported by a threepoint suspension of the landing gear. The conventional support device is a “crowbarcolumn” mode, which also has a vertical loading function of the landing gear. When assessing the structure of the landing gear connection zone, the landing gear will have a certain deformation under the direction of the heading and lateral loads. Since the support point of the conventional “crowbarcolumn” crowbar is fixed, the deformation will cause the vertical landing force line deviation and to result in that loading is not accurate. The principle of plane follower was adopted to improve the conventional crowbar fixed support point into a balltype follower platform. By the passive movement of the follower platform, the deformation of the landing gear was compensated and the deviation of the vertical loading force line was reduced. Through theoretical analysis and experimental verification, it shows that the improved “following crowbarcolumn” support device can significantly reduce the vertical loading error and improve the loading accuracy.

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王鑫涛,夏龙,刘兴科.全机结构试验起落架位移补偿加载技术研究[J].机床与液压,2021,49(8):55-59.
WANG Xintao, XIA Long, LIU Xingke. Research on Landing Gear Displacement Compensation Loading Technology of the Whole Structural Test[J]. Machine Tool & Hydraulics,2021,49(8):55-59

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  • 在线发布日期: 2023-03-01
  • 出版日期: 2021-04-28