| 摘要 |
PROBLEM TO BE SOLVED: To provide a joint assembly for an aircraft that mitigates drawbacks such as being expensive to manufacture, time-consuming and difficult to assemble, and heavy.SOLUTION: A joint assembly 400 for an aircraft includes: a single main fitting 402 including a first flange 410, a second flange 412, and a third flange; an external spar component 404 coupled to the first flange 410 using at least one fastener; an internal spar component 406 coupled to the second flange 412 using at least one fastener; and a body rib 408 coupled to the third flange using at least one fastener. |
