首页> 外国专利> METHOD OF DIMENSIONING AND PRODUCING STIFFENED STRUCTURAL COMPONENTS, USE OF STRUCTURAL CONDITION SENSORS AND AN AIRCRAFT

METHOD OF DIMENSIONING AND PRODUCING STIFFENED STRUCTURAL COMPONENTS, USE OF STRUCTURAL CONDITION SENSORS AND AN AIRCRAFT

机译:尺寸和生产加劲的结构部件的方法,结构条件传感器的使用和飞机

摘要

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.
机译:本发明涉及一种尺寸确定和生产加强结构部件(4)的方法,该结构部件包括至少一个壳体部件(6)和至少一个可以与其连接的加强部件(8),其中壳体部件(6)和至少一个至少一个加强构件(8)的尺寸是基于至少一个加强构件的完整性而确定的,并且考虑到预定的安全系数和/或预定的结构检查间隔,其中壳体构件中没有预定的最大裂纹扩展被超过和/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确定尺寸的结构部件的至少一个加强元件(8)配备有至少一个结构部件状态传感器(30),用于检测完好性;以及在飞机,尤其是客机中使用结构状态传感器。

著录项

  • 公开/公告号EP1968851B1

    专利类型

  • 公开/公告日2012-06-27

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号EP20060841380

  • 发明设计人 TELGKAMP JENS;SCHMIDT HANS-JÜRGEN;

    申请日2006-12-15

  • 分类号B64C1/06;B64F5;

  • 国家 EP

  • 入库时间 2022-08-21 17:17:01

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