主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
典型布局民用飞机的地面系留特性研究
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上海飞机设计研究院 气动能源所飞行物理部

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V211.4

基金项目:


The Ground Tie-Down Characteristic Research of Typical Civil Aircraft
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Affiliation:

Shanghai Aircraft Design and Research Institute of COMAC

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    摘要:

    飞机在地面停机时会受到恶劣天气影响,对飞机停机情况的气动力研究是评估停机安全的关键。为了分析典型布局民用飞机的地面侧风气动力差异,确定典型系留载荷,本文针对两种典型布局民用飞机,在风洞中采用缩比模型和固定地板模拟飞机停机,测量飞机在0°~180°地面侧风情况下的气动力,进一步通过部件组拆测量方法分析尾翼部件气动力耦合效应;确认垂尾平尾布局耦合效应是在侧风情况下低平尾布局飞机抬头力矩较大、以及高平尾布局飞机抬头力矩较小的原因,采用工程估算方法得到后倾翻情况的前起落架系留载荷。结果表明:俯仰气动力差异导致低平尾布局飞机的前起落架系留载荷明显增加,而对高平尾布局飞机影响较小。

    Abstract:

    The aircraft is impact by severe weather on parking apron, and the aerodynamic research of parking is most important for parking safety. In order to analyze the aerodynamic difference of typical civil aircraft induced by ground cross-wind, and determine the typical Tie-Down loads, the paper aim at two typical civil aircraft layout, adopt scale mode and fixed ground plate in wind tunnel to simulate aircraft park, measure the aerodynamic forces of aircraft which induced by cross-wind with the angles from 0 to 180 degree, and furthermore use the disassemble test method to analyze the empennage aerodynamic coupling. The research confirm the empennage aerodynamic coupling is the reason of large pitching moment of high HTP layout and small pitching moment of low HTP layout at cross-wind, finally estimate the nose landing gear Tie-Down loads for rear tipping condition. In this paper, the aerodynamic characteristics of two typical civil aircraft on ground cross-wind are compared completely, it’s useful for the aerodynamic research of parking and taxing civil aircraft , which is significant for parking Tie-Down load analysis.

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引用本文

白峰,王奇志.典型布局民用飞机的地面系留特性研究[J].航空工程进展,2022,13(5):171-178

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  • 收稿日期:2021-09-08
  • 最后修改日期:2022-01-20
  • 录用日期:2022-01-25
  • 在线发布日期: 2022-06-23
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