发明名称 Modal impact testing assembly, system and method
摘要 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.
申请公布号 EP2824440(A1) 申请公布日期 2015.01.14
申请号 EP20140171264 申请日期 2014.06.05
申请人 THE BOEING COMPANY 发明人 WALLACE, STEVEN G.
分类号 G01M1/16;G01M1/20;G01M1/22;G01M7/08;G01N3/30;G01N3/34 主分类号 G01M1/16
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