公开(公告)号：US10093434B2

公开(公告)日：2018-10-09

申请号：US14387790

申请日：2013-03-25

Applicant: ROSEBANK ENGINEERING PTY LTD

Inventor： Neil Matthews ,  Rhys Jones

IPC: B64F5/00 ,  C23C22/73 ,  C23C24/04 ,  B22F7/08 ,  B05D1/06 ,  F16B19/04 ,  C23C24/00 ,  B05D1/02 ,  C23C24/02 ,  F16B5/04 ,  B05D1/10 ,  B22F7/00 ,  B05D1/12 ,  B05D7/04 ,  B64C1/06 ,  B64C1/10 ,  B64C1/12 ,  B05D7/14 ,  B23P6/04 ,  B23P6/00 ,  B64F5/40

Abstract: The present invention relates to methods for repairing a structural weakness in an aircraft fuselage, or preventing the advancement of a structural weakness in an aircraft fuselage. Cold spray methods such as supersonic particle deposition have been shown to positively affect structural characteristics of sheet metal and lap joints as used in fuselage construction.

公开(公告)号：US20150063903A1

公开(公告)日：2015-03-05

申请号：US14387790

申请日：2013-03-25

Applicant: ROSEBANK ENGINEERING PTY LTD

Inventor： Neil Matthews ,  Rhys Jones

IPC: B64F5/00 ,  C23C24/04 ,  C23C22/73

CPC classification number: B64F5/00 ,  B05D1/02 ,  B05D1/06 ,  B05D1/10 ,  B05D1/12 ,  B05D7/04 ,  B05D7/14 ,  B22F7/00 ,  B22F7/08 ,  B23P6/00 ,  B23P6/04 ,  B64C1/06 ,  B64C1/061 ,  B64C1/064 ,  B64C1/065 ,  B64C1/068 ,  B64C1/069 ,  B64C1/10 ,  B64C1/12 ,  B64F5/40 ,  C23C22/73 ,  C23C24/00 ,  C23C24/02 ,  C23C24/04 ,  F16B5/04 ,  F16B19/04 ,  Y10T403/472

Abstract: The present invention relates to methods for repairing a structural weakness in an aircraft fuselage, or preventing the advancement of a structural weakness in an aircraft fuselage. Cold spray methods such as supersonic particle deposition have been shown to positively affect structural characteristics of sheet metal and lap joints as used in fuselage construction.

Abstract translation: 本发明涉及用于修复飞机机身中的结构性弱点的方法，或者防止飞机机身中的结构性弱点的发展。 冷喷涂方法如超音速颗粒沉积已经显示出正面影响机身结构中使用的金属板和搭接接头的结构特性。