发明名称 A method of manufacture of an aircraft landing gear component
摘要 A method of manufacturing a complex aircraft landing gear component (2) having a plurality of sub-components, the method comprising: forming a first metal sub-component (4); and joining a second metal sub-component (6) to the first metal sub-component by hot isostatic pressing (HIP or HIPing) to form the complex aircraft landing gear component. The two sub-components may be made from similar or dissimilar materials and they may be formed of powdered metal or of solid metal. Preferably the sub-components are machined prior to the joining process such that the joining process renders a component in the final or near-final shape. Optionally a third metal sub-component is positioned between the first and second sub-components in order to facilitate the bonding and to reduce the galvanic potential between the two materials. Another preferred mode is to provide interlocking interfaces between the first and second sub-components in order to improve said bonding.
申请公布号 GB2510894(A) 申请公布日期 2014.08.20
申请号 GB20130002802 申请日期 2013.02.18
申请人 MESSIER-DOWTY LIMITED 发明人 GERMAIN FORGEOUX;ANDRAZ VATOVEC;JEAN-PHILIPPE VILLAIN-CHASTRE;SIMON D HARRIS
分类号 B23K20/02;B22F3/15;B23K20/16 主分类号 B23K20/02
代理机构 代理人
主权项
地址