| 摘要 |
An aircraft interior panel (10) for supporting high-weight loads including a core panel (14) sandwiched between structural plies (16), a panel insert (12) embedded in the panel (10) and passing through and interrupting the core panel (14), the panel insert (12) having an elongate stem (22) capped on each end with an enlarged flange (24), the elongate stem (22) being arranged axially perpendicular to the core panel (14) and the enlarged flanges (24) being arranged parallel to the core panel (14), and facing sheets (20) bonded outward of the panel insert (12) for concealing the panel insert (12) within the aircraft interior panel (10). |
