公开(公告)号：US20100015396A1

公开(公告)日：2010-01-21

申请号：US12176508

申请日：2008-07-21

申请人： Curtis Alan Johnson ,  Reza Sarrafi-Nour ,  Daniel Gene Dunn

发明人： Curtis Alan Johnson ,  Reza Sarrafi-Nour ,  Daniel Gene Dunn

IPC分类号： B32B5/16 ,  B05D1/08 ,  B32B5/02 ,  B32B18/00

CPC分类号： C04B41/87 ,  C04B35/573 ,  C04B35/6264 ,  C04B35/806 ,  C04B41/009 ,  C04B41/5025 ,  C04B41/5059 ,  C04B2235/3826 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/6025 ,  Y10T428/24364 ,  Y10T428/249928 ,  Y10T428/268 ,  C04B41/4539 ,  C04B35/565 ,  C04B35/584

摘要： Disclosed herein is an article comprising a substrate; the substrate comprising a ceramic or a ceramic matrix composite; and a layer comprising coarse particles disposed upon the substrate; the coarse particles having an average particle size of 0.1 to about 1000 micrometers. Disclosed herein too is a method comprising disposing coarse particles on a substrate; the substrate comprising a ceramic or a ceramic matrix composite; the coarse particles having an average particle size of 0.1 to about 1000 micrometers.

摘要翻译： 本文公开了包含基材的制品; 所述基材包含陶瓷或陶瓷基复合材料; 以及包括设置在所述基板上的粗颗粒的层; 粗颗粒的平均粒径为0.1至约1000微米。 这里公开的方法是将粗颗粒设置在基材上; 所述基材包含陶瓷或陶瓷基复合材料; 粗颗粒的平均粒度为0.1至约1000微米。

公开(公告)号：US06884030B2

公开(公告)日：2005-04-26

申请号：US10325085

申请日：2002-12-20

申请人： Toby George Darkins, Jr. ,  Daniel Gene Dunn ,  Christopher Grace ,  Gregory Scot Corman ,  Mark Stewart Schroder

发明人： Toby George Darkins, Jr. ,  Daniel Gene Dunn ,  Christopher Grace ,  Gregory Scot Corman ,  Mark Stewart Schroder

IPC分类号： F01D9/04

CPC分类号： F01D9/042 ,  F05B2260/301 ,  F05D2240/10 ,  Y10T29/49323

摘要： A method for securing a nozzle for a turbine is provided. The nozzle includes an airfoil having a suction side and a pressure side connected at a leading edge and a trailing edge such that a cooling cavity is defined within the airfoil, the airfoil extending between an inner band and an outer band. The method includes extending at least one member through the airfoil, and at least one of the inner band and the outer band. The method further includes securing the nozzle assembly in position with at least one fastener such that the at least one member is coupled adjacent to at least one of the inner band and the outer band.

摘要翻译： 提供一种用于固定涡轮喷嘴的方法。 喷嘴包括具有吸入侧和连接在前缘和后缘处的压力侧的翼型，使得在翼型内限定冷却腔，翼型件在内带和外带之间延伸。 该方法包括使至少一个构件延伸穿过翼型，以及内带和外带中的至少一个。 该方法还包括用至少一个紧固件固定喷嘴组件就位，使得至少一个构件与内带和外带中的至少一个相邻地连接。