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AIRCRAFT LIGHTNING COMPATIBILITY TEST OBJECT DETERMINATION METHOD AND LIGHTNING RESISTANCE COMPATIBILITY PROOF METHOD

机译:飞机雷电相容性测试对象确定方法和耐雷电相容性证明方法

摘要

PROBLEM TO BE SOLVED: To provide method capable of efficiently proving the lightning resistance compatibility of a fastening section of an aircraft where many patterns are present.SOLUTION: A method of determining a test object for a test of proving the lightning resistance compatibility of a fastening section 10F, executes: a structure-pattern-population generating step S1 of generating a population of structure patterns each identified by a combination of a plurality of properties inherent in the fastening section 10F; a region extracting step S2 of extracting each region disposed in a wet area 10W where fuel or fuel steam of an aircraft is present out of regions A, B, and C of a fastening member 30 from each structure pattern in the population; a group setting step S3 of setting a group having predetermined common properties per region to each structure pattern; and a representative-pattern selecting step S4 of selecting a representative pattern representing the group from the structure patterns belonging to the group, and determines a structure pattern to which the structure patterns are narrowed down through the steps as the object under test.
机译:解决的问题:提供一种能够有效地证明存在许多图案的飞机的紧固部的耐雷击性的方法。解决方案:一种确定用于验证紧固的耐雷击性的测试的测试对象的方法部10F执行:结构图案群生成步骤S1,生成由通过紧固部10F固有的多个特性的组合来识别的结构图案群。区域提取步骤S2,从总体中的每个结构图案中,从紧固构件30的区域A,B和C中提取设置在存在飞机的燃料或燃料蒸汽的湿区10W中的每个区域;组设置步骤S3,将每个区域具有预定共同特性的组设置到每个结构图案;代表图案选择步骤S4,其从属于该组的结构图案中选择代表该组的代表图案,并确定通过这些步骤缩小了结构图案的结构图案作为被测试对象。

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