Invention Grant
US08528865B2 Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component
有权
用于连接用于飞行器或航天器和壳体部件的具有不同横截面轮廓的两个加强元件的连接装置
- Patent Title: Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component
- Patent Title (中): 用于连接用于飞行器或航天器和壳体部件的具有不同横截面轮廓的两个加强元件的连接装置
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Application No.: US12838950Application Date: 2010-07-19
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Publication No.: US08528865B2Publication Date: 2013-09-10
- Inventor: Stefan Tacke , Hauke Lengsfeld , Volker Reye
- Applicant: Stefan Tacke , Hauke Lengsfeld , Volker Reye
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: DE102008006834 20080130
- Main IPC: B64C1/06
- IPC: B64C1/06
Abstract:
A connecting arrangement for connecting two reinforcing elements of an aircraft or spacecraft, wherein the reinforcing elements have different cross-sectional profiles with at least one foot portion and at least one comb portion, at least one foot portion connecting element which on one side can be adapted to the geometric shape of the foot portion of the first reinforcing element and on the opposite side can be adapted to the geometric shape of the foot portion of the second reinforcing element and can be connected rigidly thereto; and at least one comb portion connecting element which on one side can be adapted to the geometric shape of the comb portion of the first reinforcing element and on the opposite side can be adapted to the geometric shape of the comb portion of the second reinforcing element and can be connected rigidly thereto.
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