The invention relates to shear ties for an aircraft wing. An example aircraft wing includes a skin, a composite shear tie, a stringer base charge overlaying the skin, and a stringer overlaying the stringer base charge. The composite shear tie includes a shear-tie web, a first shear-tie flange extending from a first side of the shear-tie web, a second shear-tie flange extending from a second side of the shear-tie web, and a first shear-tie tab extending from an end of the first side of the shear-tie web. The stringer includes a stringer web, a first stringer flange extending from a first side of the stringer web, and a second stringer flange extending from a second side of the stringer web. The first stringer flange is stitched to and integrated with the stringer base charge and the skin. Further, the first shear-tie flange is stitched to and integrated with the first stringer flange.
本申请涉及用于飞机机翼的抗剪带。示例飞机机翼包括蒙皮、复合抗剪带、覆盖蒙皮的桁条基座装料以及覆盖桁条基座装料的桁条。该复合抗剪带包括抗剪带腹板、从抗剪带腹板的第一侧延伸的第一抗剪带法兰、从抗剪带腹板的第二侧延伸的第二抗剪带法兰以及从抗剪带腹板的第一侧的端部延伸的第一抗剪带翼片。桁条包括桁条腹板、从桁条腹板的第一侧延伸的第一桁条法兰以及从桁条腹板的第二侧延伸的第二桁条法兰。第一桁条法兰缝合到桁条基座装料和蒙皮并与桁条基座装料和蒙皮成一体。此外,第一抗剪带法兰缝合到第一桁条法兰并与第一桁条法兰成一体。
Shear ties for aircraft wing
用于飞机机翼的抗剪带
2020-05-26
Patent
Electronic Resource
Chinese