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Eddy current crack detection capability assessment approach using crack specimens with differing electrical conductivity

机译:涡流裂纹检测能力评估方法使用不同电导率的裂纹标本

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Like other NDE methods, eddy current surface crack detectability is determined using probability of detection (POD) demonstration. The POD demonstration involves eddy current testing of surface crack specimens with known crack sizes. Reliably detectable flaw size, denoted by, a_(90/95) is determined by statistical analysis of POD test data. The surface crack specimens shall be made from a similar material with electrical conductivity close to the part conductivity. A calibration standard with electro-discharged machined (EDM) notches is typically used in eddy current testing for surface crack detection. The calibration standard conductivity shall be within +/- 15% of the part conductivity. This condition is also applicable to the POD demonstration crack set. Here, a case is considered, where conductivity of the crack specimens available for POD testing differs by more than 15% from that of the part to be inspected. Therefore, a direct POD demonstration of reliably detectable flaw size is not applicable. Additional testing is necessary to use the demonstrated POD test data. An approach to estimate the reliably detectable flaw size in eddy current testing for part made from material A using POD crack specimens made from material B with different conductivity is provided. The approach uses additional test data obtained on EDM notch specimens made from materials A and B. EDM notch test data from the two materials is used to create a transfer function between the demonstrated a_(90/95) size on crack specimens made of material B and the estimated a_(90/95) size for part made of material A. Two methods are given. For method A, a_(90/95) crack size for material B is given and POD data is available. Objective of method A is to determine a_(90/95) crack size for material A using the same relative decision threshold that was used for material B. For method B. target crack size a_(90/95) for material A is known. Objective is to determine decision threshold for inspecting material A.
机译:与其他NDE方法一样,使用检测概率(POD)演示确定涡流表面裂纹可检测性。 POD示范涉及具有已知裂纹尺寸的表面裂纹样品的涡流测试。通过POD测试数据的统计分析来确定由A_(90/95)确定的可靠可检测的缺陷尺寸。表面裂纹标本应由与靠近零件电导率的导电性的类似材料制成。具有电气放电加工(EDM)凹口的校准标准通常用于涡流测试以进行表面裂纹检测。校准标准电导率应在零件电导率的+/- 15%之内。这种情况也适用于POD示范裂缝集。这里,考虑一种情况,其中可用于POD测试的裂缝样本的导电性与待检查部件的裂缝试样的电导率不同。因此,可靠可检测缺陷尺寸的直接POD示范不适用。需要进行额外的测试以使用显示的POD测试数据。提供一种方法来估计涡流测试中的可靠检测缺陷尺寸,用于使用具有不同导电性的材料B制成的荚裂纹裂缝A的材料A.该方法采用在由材料A和B的EDM凹口标本上获得的额外测试数据。来自两种材料的EDM缺口测试数据用于在由材料B制成的裂纹样本上产生所示的A_(90/95)尺寸之间的传递函数估计的A_(90/95)尺寸为材料A.给出了两种方法。对于方法A,给出了材料B的A_(90/95)裂纹尺寸,并且可以使用POD数据。方法A的目的是使用用于材料B的相同的相对判定阈值来确定材料A的A_(90/95)裂纹尺寸。对于方法B.材料A的目标裂纹尺寸A_(90/95)是已知的。目的是确定用于检查材料A的决策阈值。

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