发明名称 DISPOSITIF DE SUPPORT D'UN RENFORT POUR LE COLLAGE DE CE RENFORT SUR LE BORD D'ATTAQUE D'UNE AUBE DE TURBOMACHINE
摘要 The device (10) has immobilization units (18, 20) for immobilizing a reinforcement (12) in a predetermined bonding position by tightening a junction part. A spacing unit forms a space between wings, and comprises movable elements (34, 36), which are connected to a pumping unit for pumping of air so as create depression between the movable elements and the wings to attach the one of the wings and an aspiration element. A controlling unit controls displacement of the movable elements to draw aside from the other wing, which is interdependent by depression. An independent claim is also included for a method for fixing a reinforcement of leading edge of a blade of a turboshaft engine.
申请公布号 FR2994884(B1) 申请公布日期 2016.09.02
申请号 FR20120058278 申请日期 2012.09.05
申请人 SNECMA 发明人 LE BRAS LUC;ALLIX VINCENT;MAGNAUDEIX DOMINIQUE
分类号 B29C65/78;B29C65/48;F04D29/38 主分类号 B29C65/78
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