公开(公告)号：US20110233338A1

公开(公告)日：2011-09-29

申请号：US13037404

申请日：2011-03-01

Applicant: David Mark STEWART

Inventor： David Mark STEWART

IPC: B64C3/00 ,  B64C1/00 ,  B23P11/00 ,  B23P17/00

CPC classification number: B64C3/28 ,  Y10T29/49771 ,  Y10T29/49826

Abstract: A joint between an aircraft wing box cover and a leading/trailing edge structure, the cover and the structure having flush aerodynamic outer surfaces, wherein the structure has an integrally formed land that extends over an inner surface of the cover, and the land of the structure is fastened to the cover. Also a method of forming the joint.

Abstract translation: 飞机翼盒盖与前缘/后缘结构之间的接头，盖和结构具有冲洗的空气动力学外表面，其中该结构具有在盖的内表面上延伸的整体形成的平台， 结构固定在盖上。 也是形成接头的方法。

公开(公告)号：US20110186690A1

公开(公告)日：2011-08-04

申请号：US13018537

申请日：2011-02-01

Applicant: David Mark STEWART

Inventor： David Mark STEWART

IPC: B64C3/50 ,  B64C1/38 ,  B23P17/00

CPC classification number: B23P17/00 ,  B64C1/38 ,  B64C3/50 ,  B64C7/00 ,  B64C9/02 ,  Y10T29/49622

Abstract: A bridging seal comprising a stack of two or more layers of elastomer, the bridging seal having a first edge and a second edge opposite the first edge, adjacent layers being attached to each other at the first and second edges, wherein adjacent layers of the bridging seal have opposing surfaces and a substantial portion of the opposing surfaces is unbonded. The bridging seal may be used to seal a gap between two aerodynamic surfaces on an aircraft.

Abstract translation: 桥接密封件包括两层或更多层弹性体的叠层，所述桥接密封件具有第一边缘和与所述第一边缘相对的第二边缘，相邻层在所述第一边缘和第二边缘处彼此附接，其中所述桥接 密封件具有相对的表面，并且相对表面的大部分是未粘合的。 桥接密封件可用于密封飞机上的两个空气动力学表面之间的间隙。

公开(公告)号：US20110095133A1

公开(公告)日：2011-04-28

申请号：US12897988

申请日：2010-10-05

Applicant: David Mark STEWART

Inventor： David Mark STEWART

IPC: B64C3/10 ,  B64C3/18 ,  B23P11/00

CPC classification number: B64C3/26 ,  B64C3/28 ,  Y10T29/49826

Abstract: An aircraft wing assembly, comprising a front spar, a rear spar, and upper and lower wing covers extending between the front and rear spars, wherein the upper and/or lower wing cover overhangs the rear spar and has a non-linear trailing edge profile forming an array of tabs and cut-outs. Also, a method of assembling the aircraft wing.

Abstract translation: 一种飞机机翼组件，包括前翼梁，后翼梁以及在前后翼梁之间延伸的上下翼翼盖，其中上翼和/或下翼盖悬挂在后翼梁上，并且具有非线性后缘轮廓 形成一系列标签和切口。 另外，组装飞机机翼的方法。