发明名称 COOLING OF THE TIP OF A BLADE
摘要 A turbine blade including an open cavity at its distal tip, the cavity being defined by a bottom wall and a side wall extending along the perimeter of the distal tip in an extension of the upper and lower walls of the blade, the side wall of the cavity including an opening in a vicinity of the leading edge of the blade opening into the cavity. A deflector extends at least in the middle portion of the cavity between the leading edge and the trailing edge.
申请公布号 US2011135496(A1) 申请公布日期 2011.06.09
申请号 US20090921295 申请日期 2009.03.04
申请人 SNECMA 发明人 BOTREL ERWAN;GROHENS REGIS
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
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