| 摘要 |
The present invention provides a method for producing a connector (100), in particular for repair, in particular in the field of aviation and aerospace, comprising the steps of: providing a base layer (102); attaching a first layer (200) of fibre composite material having a first rigidity to the base layer (102); attaching a second layer (202) of fibre composite material having a second rigidity to the first layer (200), offset therefrom, the second rigidity being greater than the first rigidity; and riveting the first layer (200) to the base layer (102) and riveting the second layer (202) to the first layer (200) and to the base layer (102). |
