Disclosed is an adjustable fixed structure attachment system (200) for an aircraft wing. The attachment system (200) comprises a bracket (210) and a bush (220). The bracket comprises a wall (212) forconnection to a wing box, a protrusion (214) protruding from the wall (212), a slot (216) extending through the protrusion (214), wherein the slot (216) has width and height. The bush (220) has a bore(222) extending there through for receipt of a pin, wherein the bush (222) is insertable into the slot (216) and the bush (220) is dimensioned relative to the slot (216) so that the bush (220) is substantially immovable in a width-wise direction of the slot (216), and is moveable in a height-wise direction of the slot (216) to thereby vary a position of the bush (220) within the slot (216). Alsodisclosed are fixed structure attachment arrangements for aircraft wings, modular aircraft wing portions, leading or trailing edge attachment systems for aircraft wings, and an aircraft.
公开了一种用于飞行器机翼的可调节固定结构附接系统(200),该附接系统(200)包括支架(210)和衬套(220),支架(210)包括:用于连接至翼盒的壁(212)、从壁(212)突出的突出部(214)以及延伸穿过突出部(214)的槽(216),其中,槽(216)具有高度和宽度,该衬套(220)具有延伸穿过衬套以用于接纳销的孔眼(222),其中,衬套(222)能够插入槽(216)中并且相对于槽(216)定尺寸,使得衬套(220)基本上不能在槽(216)的宽度方向上移动而能够在槽(216)的高度方向上移动,从而改变衬套(220)在槽(216)内的位置。还公开了用于飞行器机翼的固定结构附接装置、模块化飞行器机翼部分、用于飞行器机翼的前缘或后缘附接系统以及飞行器。
Modular attachment for leading and trailing edge structures
用于前缘结构和后缘结构的模块化附接件
2020-04-24
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Modular attachment for leading and trailing edge structures
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