公开(公告)号：US08967957B2

公开(公告)日：2015-03-03

申请号：US13288100

申请日：2011-11-03

申请人： Gary Michael Itzel ,  Christopher Michael Penny ,  Aaron Ezekiel Smith ,  Kevin Leon Bruce

发明人： Gary Michael Itzel ,  Christopher Michael Penny ,  Aaron Ezekiel Smith ,  Kevin Leon Bruce

IPC分类号： F04D29/08 ,  F01D11/02 ,  F01D5/28

CPC分类号： F01D11/02 ,  F01D5/288 ,  Y02T50/671

摘要： A rotating airfoil component equipped with one or more angel wings that inhibit the ingress of a hot working fluid into interior regions of a turbomachine in which the component is installed. The component includes an airfoil and a feature for mounting the component to enable rotation of the component within the turbomachine. An angel wing projects from the component to have a first surface facing the airfoil, an oppositely-disposed second surface facing the mounting feature, and at least one lateral surface therebetween. A thermal-insulating coating system is present on the first surface to inhibit heat transfer from the working fluid to the angel wing but not on the second or lateral surfaces so as not to inhibit heat transfer from the second and lateral surfaces of the angel wing.

摘要翻译： 装备有一个或多个天使翼的旋转翼型零件，其阻止热工作流体进入其中安装该部件的涡轮机的内部区域。 该部件包括翼型件和用于安装部件以使部件在涡轮机内旋转的特征。 天使翼从部件突出以具有面向翼型的第一表面，面对安装特征的相对设置的第二表面以及其间的至少一个侧表面。 绝热涂层系统存在于第一表面上以抑制从工作流体传递到天使翼而不是在第二或侧面上的热传递，从而不会妨碍从天使翼的第二和侧面的热传递。