A composite structure includes a first composite material, a second composite material bonded to the first composite material, and a corner fillet part provided at a corner part formed by the first composite material and the second composite material. In the composite structure, the rigidity of the corner fillet part is adjustable, and a pull-off stress to be applied to the corner part is adjusted by adjusting the rigidity of the corner fillet part. The pull-off stress to be applied to the corner part is adjusted to be decreased by adjusting the rigidity of the corner fillet part to be decreased.
COMPOSITE STRUCTURE, AIRCRAFT, AND DESIGN METHOD FOR CORNER FILLET PART
2017-09-14
Patent
Electronic Resource
English
COMPOSITE STRUCTURE, AIRCRAFT AND METHOD FOR DESIGNING CORNER FILLET PART
European Patent Office | 2016
|COMPOSITE STRUCTURE, AIRCRAFT, AND METHOD FOR DESIGNING CORNER FILLET SECTION
European Patent Office | 2019
|COMPOSITE STRUCTURE, AIRCRAFT, AND METHOD FOR DESIGNING CORNER FILLET SECTION
European Patent Office | 2016
|Bolt Heads, Hexagon - Large Fillet Aircraft Engine
SAE Technical Papers | 2002