| 摘要 |
PROBLEM TO BE SOLVED: To provide an aircraft assembly that can suppress thunderstroke on a fastener by suppressing the occurrence of a streamer which is a precursor phase of the thunderstroke at a fastener plate head peripheral part high in the frequency of the thunderstroke. SOLUTION: The aircraft assembly A includes the skin 10 of an aircraft; a structural member 11 supporting the skin 10 from the inside; and the fastener 1 connecting the skin 10 to the structural member 11. A sealing material 18 is filled between the fastener 1 and the skin 10. COPYRIGHT: (C)2011,JPO&INPIT |
