| 发明名称 | Process for manufacturing a metal part, such as turbine engine blade reinforcement | ||
| 摘要 | A method for producing a metal component such as a metal turbomachine blade reinforcement, includes positioning a plurality of metal staples in a forming tool having a die and a punch; and hot isostatic pressing the plurality of metal staples causing the agglomeration of the metal staples so as to obtain a solid component. | ||
| 申请公布号 | US9364887(B2) | 申请公布日期 | 2016.06.14 |
| 申请号 | US201214002506 | 申请日期 | 2012.02.29 |
| 申请人 | SNECMA | 发明人 | Godon Thierry;Dambrine Bruno Jacques Gérard;Perroux Alain Robert Yves |
| 分类号 | B23K20/02;B21K3/04;B21D22/02;B21D53/92;B21K25/00;B22F3/15;B23P15/04;C22C14/00;C22C29/06;F01D5/14;F04D29/32 | 主分类号 | B23K20/02 |
| 代理机构 | Pillsbury Winthrop Shaw Pittman LLP | 代理人 | Pillsbury Winthrop Shaw Pittman LLP |
| 主权项 | 1. A process for manufacturing a metal part, comprising: positioning a plurality of metal staples in a forming tool presenting a die and a punch with said plurality of metal staples being metal sections in a rectilinear shape bended in a shape of a U or a V; after positioning the plurality of metal staples in the forming tool, hot isostatic pressing said plurality of metal staples causing agglomeration of the plurality of metal staples so as to obtain a compact metal part, wherein the positioning of said plurality of metal staples is achieved by placing at least two metal staples of said plurality of metal staples at different times in the die or on the punch of said forming tool. | ||
| 地址 | Paris FR | ||