发明名称 MODAL IMPACT TESTING ASSEMBLY, SYSTEM AND METHOD BACKGROUND
摘要 <p>There is disclosed an assembly (10), a system (12) and a method (150) for modal impact testing. The assembly (10) has a first set of components (14). The first set of components (14) include an impact assembly (16), a cycle control element (18) coupled to the impact assembly (16), and a signal response measuring device (20) positioned opposite the impact assembly (16). The assembly (10) further has a second set of components (28) separate from the first set of components (14). The second set of components (28) include a first controller (30) coupled to the cycle control element (18) and a second controller (34) coupled to the signal response measuring device (20). The first set of components (14) and the second set of components (28) form a modal impact testing assembly (10) for modal impact testing. The impact assembly (16) of the modal impact testing assembly (10) is configured to impact a test element (46) rotating at operational speeds.</p>
申请公布号 IN1158DE2014(A) 申请公布日期 2015.06.05
申请号 IN2014DE01158 申请日期 2014.04.29
申请人 THE BOEING COMPANY 发明人 STEVEN G. WALLACE
分类号 G01N3/30 主分类号 G01N3/30
代理机构 代理人
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