| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a laminar composite for a machine body structure of an aircraft and a machine body structure of aircraft superior in thunder resistance and electrostatic diffusivity. <P>SOLUTION: The laminar composite 10 is constituted by laminating the first fiber reinforced plastic composite layer 11 (e.g., CFRP layer), an electroconductive layer (e.g., metal foil) 13 formed in one face of the layer 11, an insulating layer (e.g., CFRP layer) 14 formed in the other face thereof, and the second fiber reinforced plastic composite layer (e.g., CFRP layer) 12 formed in the opposite face of the face of the insulating layer, contacting the layer 11. Another laminar composite 30 is constituted by laminating a fiber reinforced plastic composite layer (e.g., CFRP layer) 31, an insulating layer (e.g., CFRP layer) 32 formed in one face of the layer 31, an electroconductive layer (e.g., metal foil) 33 formed in the opposite face of the insulating layer, contacting the layer 31, and a high resistance electroconductive layer (e.g., carbon-containing primer) 34 formed in the other face of the layer 31. The electroconductive layer 13 or the electroconductive layer 33 is arranged in the outer face of the machine body. <P>COPYRIGHT: (C)2012,JPO&INPIT |
