公开(公告)号：US09592901B2

公开(公告)日：2017-03-14

申请号：US14594292

申请日：2015-01-12

Applicant: Textron Innovations Inc.

Inventor： John R. McCullough ,  David Gordon Carlson ,  James Donn Hethcock ,  Paul K. Oldroyd ,  Carl A. May

IPC: B64C1/12 ,  B29D99/00 ,  B64C1/06 ,  F16B5/01 ,  F16B5/12 ,  F16B17/00 ,  B29C65/50 ,  B29C65/56 ,  B29C65/00 ,  B29L31/30 ,  B64C1/00 ,  B29C65/48

CPC classification number: B64C1/12 ,  B29C65/4835 ,  B29C65/5021 ,  B29C65/5057 ,  B29C65/5078 ,  B29C65/5085 ,  B29C65/562 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/1162 ,  B29C66/1282 ,  B29C66/12881 ,  B29C66/43441 ,  B29C66/721 ,  B29C66/72525 ,  B29C66/8416 ,  B29D99/001 ,  B29L2031/3076 ,  B64C1/06 ,  B64C2001/0072 ,  F16B5/01 ,  F16B5/12 ,  F16B17/00 ,  Y02T50/43 ,  Y10T29/49622 ,  Y10T403/70

Abstract: A structural joint includes a first member having a first base portion and a first leg portion. The structural joint further includes a second member having a second base portion and a second base portion. The first base portion and the second base portion are coupled together at an overlapping portion. The first leg portion and the second leg portion form a cavity for structurally coupling to a structural member.

Abstract translation: 结构接头包括具有第一基部和第一腿部的第一构件。 结构接头还包括具有第二基部和第二基部的第二构件。 第一基部和第二基部在重叠部分处连接在一起。 第一腿部分和第二腿部部分形成用于结构上结合到结构构件的空腔。

公开(公告)号：US11161592B2

公开(公告)日：2021-11-02

申请号：US16567519

申请日：2019-09-11

Applicant: Textron Innovations Inc.

Inventor： George Ryan Decker ,  Steven Allen Robedeau, Jr. ,  Tjepke Heeringa ,  David Gordon Carlson

IPC: B64C3/26 ,  B64C3/18 ,  B64C1/00 ,  B64C29/00

Abstract: A wing assembly for an aircraft includes a torque box sleeve having an open end and a plurality of integral sides including leading, aft, top and bottom sides that jointlessly form a continuous surface having a generally airfoil shape. The wing assembly includes an internal support subassembly having a plurality of ribs coupled to a central spar. The internal support subassembly is formed into a single component outside the torque box sleeve and inserted into the open end of the torque box sleeve as the single component. The internal support subassembly is coupled to an interior of the torque box sleeve.