A composite reinforcement structure including a first skin having a first end and a second end and a second skin having a first end and a second end. The first end of the first skin and the first end of the second skin are coupled. A corrugated spar is disposed between the first skin and the second skin and is bonded to the first skin and the second skin.
COMPOSITE REINFORCEMENT STRUCTURES AND AIRCRAFT ASSEMBLIES COMPRISING COMPOSITE REINFORCEMENT STRUCTURES
2018-02-15
Patent
Electronic Resource
English
European Patent Office | 2020
|Bonded Boron/Epoxy Composite Doublers for Reinforcement of Metallic Aircraft Structures
British Library Online Contents | 1996
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