发明名称 КОМПОЗИЦИОННАЯ ЛОПАТКА ГАЗОТУРБИННОГО ДВИГАТЕЛЯ С МЕТАЛЛИЧЕСКИМ УСИЛИТЕЛЬНЫМ ЭЛЕМЕНТОМ
摘要 The blade (10) has an aerodynamic surface (12) extending along an axial direction (14) between a leading edge (16) and a trailing edge (18), and along a radial direction (20) between a root (22) and a tip (24). The surface is made of a composite material, and a metal structural reinforcement (32) is adhesively bonded to the edge (16). The reinforcement extends along the axial direction beyond the edge (16) and in the radial direction between the root and the tip. The reinforcement has a recess for absorbing energy produced from the impact of a foreign body e.g. bird, against the edge (16).
申请公布号 RU2007135622(A) 申请公布日期 2009.03.27
申请号 RU20070135622 申请日期 2007.09.25
申请人 СНЕКМА (FR) 发明人 ЖИЮСТИ Стефан (FR);ЖАК Кристоф (FR);ЛОМБАР Жан-Пьер (FR);СЮФФИ Арно (FR)
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
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