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METHOD FOR REPAIRING THE WING CAISSON WITH THE NETTED COMPOSITE RIBS, COMPOSITE SKIN AND METALLIC SPARS

机译:用网状复合肋骨,复合皮和金属稀疏修复机翼沉箱的方法

摘要

FIELD: aircraft engineering.;SUBSTANCE: invention relates to aeronautical and space technology and relates to the method for repairing the torsion box skin and netted of the wing caisson with mesh composite ribs, with the composite lining and metal spars. When repairing the skin and/or reticular rib of the wing of the flying device (LA) the damaged area is determined by means of nondestructive testing. Then the damaged area is cut out and the glue is applied to the edges of the cutout. Then, the repair patch is molded directly onto the place of the cutout and it is installed on top of the cutout with the help of glue, which is applied to the edges of the cutout. After that, the mechanical fasteners are installed, which fix the repair patch on the sections between the power elements of the mesh composite rib and on the side members of the wing caisson.;EFFECT: increased manufacturability and simplification of the repair process of the skin and netted rib of the wing caisson is achieved.;8 cl, 3 dwg
机译:技术领域本发明涉及航空航天技术,涉及一种用网状复合肋,复合衬里和金属翼梁修复机翼沉箱的扭转箱蒙皮和网的方法。修复飞行装置(LA)机翼的皮肤和/或网状肋骨时,通过无损检测确定受损区域。然后切掉受损区域,然后将胶水涂抹到切口的边缘。然后,将修补贴片直接模制到切口的位置,并借助胶水将其安装在切口的顶部,然后将胶水粘贴到切口的边缘。之后,安装机械紧固件,将修复补片固定在网状复合肋骨的动力元件之间的部分以及机翼沉箱的侧面构件上;效果:提高了可制造性并简化了皮肤的修复过程并获得机翼沉箱的网状肋骨。; 8 cl,3 dwg

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