公开(公告)号：US07126096B1

公开(公告)日：2006-10-24

申请号：US08470168

申请日：1995-06-06

申请人： Marc R. Matsen ,  Douglas A. McCarville ,  Michael M. Stepan

发明人： Marc R. Matsen ,  Douglas A. McCarville ,  Michael M. Stepan

IPC分类号： H05B6/10

CPC分类号： C22C47/068 ,  B21D26/055 ,  B22F3/105 ,  B22F2003/1046 ,  B22F2003/1053 ,  B22F2998/00 ,  B29C33/06 ,  B29C65/34 ,  B29C65/3476 ,  B29C65/3492 ,  B29C65/364 ,  B29C65/3644 ,  B29C65/3676 ,  B29C66/634 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7392 ,  B29C66/91411 ,  B29C66/91443 ,  B29C66/91645 ,  B29C66/91655 ,  B29C66/91951 ,  B29C70/44 ,  B29C70/542 ,  B29C2035/0811 ,  B32B2309/62 ,  B64C3/18 ,  H05B6/365 ,  Y02P10/253 ,  Y02T50/43 ,  C22C47/20 ,  B29K2071/00

摘要： Rib and spar webs are joined in a composite wingbox to eliminate fasteners by welding the webs along bondlines defined by overlapping sections of the webs. Heat to produce the weld is generally achieved resistively by connecting a multistrip susceptor positioned along the bond line to a current source, since the geometry makes it difficult to heat these web joints inductively. The wingbox is completed without fasteners by welding skins to the rib-spar wingbox.

摘要翻译： 肋和翼梁腹板连接在复合翼箱中，以通过沿腹板的重叠部分限定的粘合线焊接腹板来消除紧固件。 通常通过将沿着接合线定位的多脚架基座连接到电流源来实现焊接的热量，因为几何形状使得难以感应地加热这些纤维网接头。 翼形框架通过将表皮焊接到肋翼翼箱而完成无紧固件。