发明名称 BLADE WITH A COOLING GROOVE FOR A BLADED WHEEL OF A TURBOMACHINE
摘要 A blade for a turbomachine bladed wheel, the blade including an airfoil and a platform with at least one air injection passage, the platform including a groove running along the pressure side of the airfoil at least in the vicinity of a downstream portion thereof, and formed between the pressure side and a ridge formed on the platform surface at a short distance from said downstream portion of the pressure side, at least one air injection passage being arranged in the groove. Because of the presence of the groove, the air stream injected via the air injection passage(s) is kept close to the pressure side and thus provides effective cooling of the downstream portion thereof.
申请公布号 US2009202358(A1) 申请公布日期 2009.08.13
申请号 US20090367120 申请日期 2009.02.06
申请人 SNECMA 发明人 GROHENS REGIS;ROYAN RENAUD GABRIEL CONSTANT
分类号 F01D5/18 主分类号 F01D5/18
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