公开(公告)号：US20150259079A1

公开(公告)日：2015-09-17

申请号：US14669582

申请日：2015-03-26

申请人： THE BOEING COMPANY

发明人： Brad L. Kirkwood ,  Paul S. Gregg ,  Gerald D. Miller ,  Jeff D. Will ,  David W. Evans

IPC分类号： B64F5/00 ,  B23K3/08

CPC分类号： B64F5/0009 ,  B23K3/087 ,  B23K31/00 ,  B64C3/185 ,  B64F5/10 ,  Y10T403/4605

摘要： The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.

摘要翻译： 本发明涉及飞机中的安装装置。 在本发明的一个方面，公开了一种组装安装装置的金属固定件的方法。 在本发明的另一方面，公开了一种安装装置。 在本发明的另一方面，公开了一种用于在飞行器中安装和使用安装装置的方法。

公开(公告)号：US20160068922A1

公开(公告)日：2016-03-10

申请号：US14942997

申请日：2015-11-16

申请人： The Boeing Company

发明人： Brad L. Kirkwood ,  Marc R. Matsen ,  Tony Shen ,  Wesley B. Crow

IPC分类号： C21D1/42 ,  C22F1/18 ,  C21D6/00 ,  B23F17/00 ,  C21D1/60 ,  C21D1/613 ,  C21D1/74 ,  B21K29/00 ,  C22F1/10 ,  C21D1/62

CPC分类号： C21D1/42 ,  B21K29/00 ,  B23F17/006 ,  C21D1/10 ,  C21D1/60 ,  C21D1/613 ,  C21D1/62 ,  C21D1/74 ,  C21D6/00 ,  C21D6/02 ,  C21D9/32 ,  C21D10/005 ,  C21D2211/004 ,  C22F1/10 ,  C22F1/183 ,  C23C14/06 ,  Y02P10/253 ,  Y10T29/4948

摘要： A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.

摘要翻译： 存在用于制造零件的方法和装置。 该部件由金属合金构成，并且定位成形成定位部件。 产生加热定位部件的电磁场。 定位部件的表面暴露于惰性气体中，同时产生电磁场以在定位部件的外部和定位部件的内部部分之间产生反向热梯度，以形成热处理部分。

公开(公告)号：US10179940B2

公开(公告)日：2019-01-15

申请号：US14942997

申请日：2015-11-16

申请人： The Boeing Company

发明人： Brad L. Kirkwood ,  Marc R. Matsen ,  Tony Shen ,  Wesley B. Crow

IPC分类号： C21D1/42 ,  C21D1/10 ,  C21D6/02 ,  C21D9/32 ,  C21D10/00 ,  C22F1/10 ,  C22F1/18 ,  C23C14/06 ,  B21K29/00 ,  B23F17/00 ,  C21D1/60 ,  C21D1/613 ,  C21D1/62 ,  C21D1/74 ,  C21D6/00

摘要： A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.

公开(公告)号：US09394062B2

公开(公告)日：2016-07-19

申请号：US14669582

申请日：2015-03-26

申请人： THE BOEING COMPANY

发明人： Brad L. Kirkwood ,  Paul S. Gregg ,  Gerald D. Miller ,  Jeff D. Will ,  David W. Evans

IPC分类号： B23K1/20 ,  B23K3/00 ,  B64F5/00 ,  B23K31/00 ,  B64C3/18 ,  B23K3/08

CPC分类号： B64F5/0009 ,  B23K3/087 ,  B23K31/00 ,  B64C3/185 ,  B64F5/10 ,  Y10T403/4605

摘要： The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.

公开(公告)号：US20130097847A1

公开(公告)日：2013-04-25

申请号：US13710624

申请日：2012-12-11

申请人： The Boeing Company

发明人： Brad L. Kirkwood ,  Lee C. Firth ,  Richard D. Widdle ,  Wesley B. Crow

IPC分类号： F16B13/04

CPC分类号： F16B13/04 ,  F16B1/0014 ,  F16B3/00 ,  Y10T29/49865 ,  Y10T29/49954

摘要： A method to join a first structure to a second structure comprises aligning a first hole in the first structure with a second hole in the second structure and inserting a fastener into the first hole and the second hole. The fastener comprises a shape memory alloy which was formed into a first shape having a diameter slightly larger than a diameter of the first hole and the second hole when the shape memory alloy was in an austenite state and reduced to a second shape having a diameter less than the diameter of the first hole and the second hole when the shape memory alloy was in a martensite state. The method further comprises heating the fastener above an austenite start transition temperature.

摘要翻译： 将第一结构连接到第二结构的方法包括将第一结构中的第一孔与第二结构中的第二孔对准，并将紧固件插入第一孔和第二孔。 紧固件包括形状记忆合金，其形状为第一形状，其形状记忆合金处于奥氏体状态时直径略大于第一孔和第二孔的直径，并减小为直径较小的第二形状 比形状记忆合金处于马氏体状态时的第一孔和第二孔的直径大。 该方法还包括将紧固件加热到奥氏体开始转变温度之上。