Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
FASTENING SYSTEM FOR FASTENING A COMPONENT, COMPONENT ARRANGEMENT, AND AIRCRAFT
A fastening system (10) comprises a structure holding element (12) which can be fastened to a structural component (104). The fastening system (10) further comprises a component holding element (20) which can be fastened to a component (102) that is to be fastened and which is movable relative to the structure holding element (12) between a first operating position and a second operating position. A first lever element (24) of the fastening system (10) is connected to the structure holding element (12) so as to be rotatable about a first rotation axis (A1) and is connected to the component holding element (20) so as to be rotatable about a second rotation axis (A2). Lastly, the fastening system (10) comprises a connection element (38), which is connected to the component holding element (20) so as to be rotatable about a third rotation axis (A3) and which is connected to the structure holding element (12) so as to be displaceable in translation relative to the structure holding element (12), in such a way that the second rotation axis (A2), when the component holding element (20) is transferred from its first operating position into its second operating position, is displaced in a plane (E) extending perpendicularly to the second rotation axis (A2).
一种紧固系统(10)包括结构保持元件(12)，所述结构保持元件能够紧固在结构构件(104)上。此外，所述紧固系统(10)包括构件保持元件(20)，所述构件保持元件能够紧固在要紧固的构件(102)上，并且能够相对于所述结构保持元件(12)在第一操作位置与第二操作位置之间运动。所述紧固系统(10)的第一杆元件(24)以能够围绕第一旋转轴(A1)旋转的方式与所述结构保持元件(12)连接，并且以能够围绕第二旋转轴(A2)旋转的方式与所述构件保持元件(20)连接。最后，所述紧固系统(10)包括连接元件(38)，所述连接元件以能够围绕第三旋转轴(A3)旋转的方式与所述构件保持元件(20)连接，并且所述连接元件以能够相对于所述结构保持元件(12)平移移位的方式与所述结构保持元件(12)连接，使得在所述构件保持元件(20)从其第一操作位置转移到其第二操作位置时，所述第二旋转轴(A2)在垂直于所述第二旋转轴(A2)延伸的平面(E)中移位。
FASTENING SYSTEM FOR FASTENING A COMPONENT, COMPONENT ARRANGEMENT, AND AIRCRAFT
A fastening system (10) comprises a structure holding element (12) which can be fastened to a structural component (104). The fastening system (10) further comprises a component holding element (20) which can be fastened to a component (102) that is to be fastened and which is movable relative to the structure holding element (12) between a first operating position and a second operating position. A first lever element (24) of the fastening system (10) is connected to the structure holding element (12) so as to be rotatable about a first rotation axis (A1) and is connected to the component holding element (20) so as to be rotatable about a second rotation axis (A2). Lastly, the fastening system (10) comprises a connection element (38), which is connected to the component holding element (20) so as to be rotatable about a third rotation axis (A3) and which is connected to the structure holding element (12) so as to be displaceable in translation relative to the structure holding element (12), in such a way that the second rotation axis (A2), when the component holding element (20) is transferred from its first operating position into its second operating position, is displaced in a plane (E) extending perpendicularly to the second rotation axis (A2).
一种紧固系统(10)包括结构保持元件(12)，所述结构保持元件能够紧固在结构构件(104)上。此外，所述紧固系统(10)包括构件保持元件(20)，所述构件保持元件能够紧固在要紧固的构件(102)上，并且能够相对于所述结构保持元件(12)在第一操作位置与第二操作位置之间运动。所述紧固系统(10)的第一杆元件(24)以能够围绕第一旋转轴(A1)旋转的方式与所述结构保持元件(12)连接，并且以能够围绕第二旋转轴(A2)旋转的方式与所述构件保持元件(20)连接。最后，所述紧固系统(10)包括连接元件(38)，所述连接元件以能够围绕第三旋转轴(A3)旋转的方式与所述构件保持元件(20)连接，并且所述连接元件以能够相对于所述结构保持元件(12)平移移位的方式与所述结构保持元件(12)连接，使得在所述构件保持元件(20)从其第一操作位置转移到其第二操作位置时，所述第二旋转轴(A2)在垂直于所述第二旋转轴(A2)延伸的平面(E)中移位。
FASTENING SYSTEM FOR FASTENING A COMPONENT, COMPONENT ARRANGEMENT, AND AIRCRAFT
用于紧固构件的紧固系统、构件组件和飞行器
EGGERT PHILIPP (Autor:in) / MARCULESCU BOGDAN-FLORIN (Autor:in)
14.01.2022
Patent
Elektronische Ressource
Chinesisch
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