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飞机压力加油系统管道泄漏检测方法研究
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V21;TH137

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Study of Pipeline Leak Detection of Aircraft Ground Pressure Fueling System
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    摘要:

    提出基于最小阶非线性观测器的设计方法,通过对管路两端点处的压力流量在线采集处理,运用状态解耦技术,选择适当的状态线性变换方式,有效地分离出反映管路中间节点状态的残差数值,进而对非线性状态方程序列生成相应的系统残差集,以达到对管内泄漏的有效定位。该方法在飞机压力加油系统地面模拟试验中成功地进行了验证,得到了较为满意的结果。

    Abstract:

    A new design approach based on the minimal order nonlinear observer is presented to detect and locate leaks in complicated pipelines, since the measurements of pressure and flow are realizable only at the two extremes of the ducts, the state decoupling technology is utilized in generating the residual values and an appropriate method of linear coordinate transformation is selected. Then the residual sets are attained according to a series of state equations, which are sensitive to the leak set. Finally the performance of the approach is demonstrated by using the experimental data taken from the airplane refueling pipelines with leaks, and satisfactory results are obtained.

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周瑞祥,苏新兵.飞机压力加油系统管道泄漏检测方法研究[J].空军工程大学学报,2002,(6):7-9

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  • 在线发布日期: 2015-11-17
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