COMPOSITE LAMINATE AND LOAD-INTRODUCTION COMPONENT FOR A LOAD-INTRODUCTION JOINT

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United States of America Patent

APP PUB NO 20190211852A1
SERIAL NO

16359480

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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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.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS HELICOPTERS DEUTSCHLAND GMBH86609 DONAUWÖRTH

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BUESING, Moritz Augsburg, DE 13 22

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