发明名称 METHOD AND DEVICE FOR DETECTING AN OVERSTEPPING OF DESIGN LOADS OF THE FIN OF AN AIRCRAFT
摘要 The device ( 1 ) comprises a set ( 2 ) of information sources, means ( 3 ) for determining, with the aid of information emanating from said set ( 2 ), a current bending moment, means ( 5 ) for determining, with the aid of information emanating from said set ( 2 ), a current twisting moment, means ( 7 ) for carrying out a comparison by comparing the pair formed by the current bending moment and the current twisting moment with a safety envelope representing a chart formed in a plane on the basis of pairs of values of bending and twisting moments and defined so that, for any pair which lies outside the safety envelope, there exists a risk of appearance of permanent deformations on the fin, and means ( 10 ) for determining whether a structural inspection of the fin has to be performed, at least on the basis of the result of said comparison.
申请公布号 US2007136030(A1) 申请公布日期 2007.06.14
申请号 US20050143704 申请日期 2005.06.03
申请人 AIRBUS FRANCE 发明人 DELAPLACE FRANCK;MARQUIER SYLVIE;MATHIEU GERARD;SQUEGLIA GENNARO
分类号 G06F17/50;B64C5/06;B64D43/02;B64F5/00;G01C5/00;G05D1/00;G06F19/00;G08B21/00;G08B23/00 主分类号 G06F17/50
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