Invention Grant
- Patent Title: Composite laminate and load-introduction component for a load-introduction joint
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Application No.: US14877077Application Date: 2015-10-07
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Publication No.: US10280953B2Publication Date: 2019-05-07
- Inventor: Moritz Buesing
- Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
- Applicant Address: DE Donauworth
- Assignee: AIRBUS HEICOPTERS DEUTSCHLAND GMBH
- Current Assignee: AIRBUS HEICOPTERS DEUTSCHLAND GMBH
- Current Assignee Address: DE Donauworth
- Agency: Brooks Kushman P.C.
- Priority: EP14400047 20141008
- Main IPC: F16B1/00
- IPC: F16B1/00 ; B29C65/56 ; B29C65/82 ; B29C65/00 ; B64C27/48 ; F16B31/02 ; B64C27/00 ; B64C27/473 ; B64D45/00 ; B29L31/30 ; F16B5/02 ; B29L31/08

Abstract:
A composite laminate for connection to at least one attachment component in a load-introduction joint, said composite laminate comprising an opening that is adapted to receive a load-introduction component of said load-introduction joint, wherein a prefailure indication element is provided in the region of said opening, said prefailure indication element being modifiable by said load-introduction component in a prefailure mode of said load-introduction joint for indication of an impending function-affecting failure of said composite laminate. The invention is further related to a corresponding load-introduction component.
Public/Granted literature
- US20160102688A1 COMPOSITE LAMINATE AND LOAD-INTRODUCTION COMPONENT FOR A LOAD-INTRODUCTION JOINT Public/Granted day:2016-04-14
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