| 摘要 |
An aircraft component includes, but is not limited to, a first panel including a first channel and a second panel including a second channel. The second panel is disposed such that the second channel is aligned with the first channel. The aircraft component further includes, but is not limited to, a web section that disposed adjacent the first and second panels. The web section includes a first engagement portion engaged with the first channel and a second engagement portion engaged with the second channel. The aircraft component further includes, but is not limited to an adhesive that is disposed between the first engagement portion and the first channel and between the second engagement portion and the second channel. The first panel and the second panel are joined together by cooperation of the web section and the adhesive. |
