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    • 2. 发明授权
    • Method of dimensioning and producing stiffened structural components, use of structural condition sensors and an aircraft
    • 尺寸和制造加强结构件的方法,结构状态传感器和飞机的使用
    • US07913568B2
    • 2011-03-29
    • US12094841
    • 2006-12-15
    • Jens TelgkampHans-Jürgen Schmidt
    • Jens TelgkampHans-Jürgen Schmidt
    • G01B5/30
    • B64C1/068B64C2001/0081B64F5/10Y02T50/42
    • The invention concerns a method of dimensioning and producing stiffened structural components (4) comprising at least one shell component (6) and at least one stiffening component (8) which can be connected thereto, in which the shell component (6) and the at least one stiffening component (8) is dimensioned on the assumption of intactness of the at least one stiffening component and having regard to a predetermined safety factor and/or a predetermined structural inspection interval in which a predetermined maximum crack progression in the shell component is not to be exceeded and/or the strength of the structural component is not to fall below a predetermined minimum residual strength, and in which the at least one stiffening element (8) of the structural component dimensioned by this method is equipped with at least one structural condition sensor (30) for detecting intactness; as well as the use of structural condition sensors in an aircraft, in particular a passenger aircraft.
    • 本发明涉及一种尺寸和制造加强结构部件(4)的方法,所述加强结构部件(4)包括至少一个壳部件(6)和至少一个可连接到其上的加强部件(8),其中所述壳部件(6)和所述 考虑到预定的安全系数和/或预定的结构检查间隔来确定至少一个加强部件(8)的尺寸,其中所述至少一个加强部件的完整性在壳部件中预定的最大裂纹进展不是 并且/或结构部件的强度不低于预定的最小残余强度,并且其中通过该方法尺寸的结构部件的至少一个加强元件(8)装备有至少一个结构 条件传感器(30),用于检测完整性; 以及在飞行器,特别是客机中使用结构状态传感器。