首页> 外国专利> AIRFOIL VANE, BAFFLE FOR AN AIRFOIL VANE ASSEMBLY AND METHOD OF ASSEMBLING A CERAMIC MATRIX COMPOSITE AIRFOIL VANE

AIRFOIL VANE, BAFFLE FOR AN AIRFOIL VANE ASSEMBLY AND METHOD OF ASSEMBLING A CERAMIC MATRIX COMPOSITE AIRFOIL VANE

机译:翼型叶片,用于翼型叶片组件的挡板和组装陶瓷矩阵复合翼型叶片的方法

摘要

An airfoil vane (100) includes an airfoil section (106) including an outer wall (108) that defines an internal cavity (110); and a baffle (112; 212; 312; 412) situated in the internal cavity, the baffle including a baffle wall (113; 213; 313; 413) that defines a central cavity (114; 214; 314; 414) having a leading end (113a; 213;a 313a; 413a) and a trailing end (113b; 213b; 313b; 413b) corresponding to a leading end and a trailing end of the airfoil section, and a tail (118; 218; 318; 418) extending from the baffle wall, the tail including at least one feature configured to disturb an airflow surrounding the tail. A baffle for the airfoil vane assembly and a method of assembling a ceramic matrix composite airfoil vane are also disclosed.
机译:翼型叶片(100)包括翼型部分(106),该翼型部分(106)包括限定内腔(110)的外壁(108);位于内腔中的挡板(112; 212; 312; 412),该挡板包括挡板壁(113; 213; 313; 413),其限定中心腔(114; 214; 314; 414)具有前导的端部(113a; 213; 313a; 413a)和对应于翼型部分的前端和尾部的后端和尾部(118; 218; 318; 418)的后端(113b; 213b; 313b; 413b)从挡板壁延伸,尾部包括至少一个特征,该特征被配置为干扰围绕尾部的气流。还公开了一种用于翼型叶片组件的挡板和组装陶瓷基质复合翼型叶片的方法。

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