公开(公告)号：US20110052406A1

公开(公告)日：2011-03-03

申请号：US12547066

申请日：2009-08-25

申请人： Robert William Bruce ,  Aaron Dennis Gastrich ,  John William Hanify ,  Roger Owen Barbe

发明人： Robert William Bruce ,  Aaron Dennis Gastrich ,  John William Hanify ,  Roger Owen Barbe

IPC分类号： F01D5/28 ,  C23C16/44

CPC分类号： F01D5/28 ,  C23C16/44 ,  F01D5/288 ,  F04D29/023 ,  F04D29/324 ,  F05D2230/313 ,  F05D2240/121 ,  F05D2240/303 ,  F05D2300/228 ,  F05D2300/611 ,  Y02T50/671 ,  Y02T50/673

摘要： A process for depositing coatings, and particularly erosion-resistant coatings suitable for protecting surfaces subjected to collisions with particles, such as a compressor blade of a gas turbine engine. The blade has an airfoil comprising oppositely-disposed convex and concave surfaces, oppositely-disposed leading and trailing edges defining therebetween a chord length of the airfoil, and a blade tip. An erosion-resistant coating is present on at least the concave surface, but not on the convex surface within at least 20% of the chord length from the leading edge.

摘要翻译： 一种用于沉积涂层的方法，特别是耐腐蚀涂层，适用于保护与颗粒碰撞的表面，例如燃气涡轮发动机的压缩机叶片。 叶片具有包括相对设置的凸形和凹形表面的翼型件，相对设置的前缘和后缘在其间限定翼型的翼弦长度和叶片尖端。 至少在凹形表面上存在防侵蚀涂层，而不存在于来自前缘的至少20％的弦长中的凸表面上。

公开(公告)号：US07313909B2

公开(公告)日：2008-01-01

申请号：US10972552

申请日：2004-10-25

申请人： Andrew Jay Skoog ,  Jane Ann Murphy ,  John Michael Jasany ,  Aaron Dennis Gastrich ,  Timothy Lance Manning

发明人： Andrew Jay Skoog ,  Jane Ann Murphy ,  John Michael Jasany ,  Aaron Dennis Gastrich ,  Timothy Lance Manning

IPC分类号： F02C7/08

CPC分类号： F02K1/825 ,  C23C4/02 ,  C23C24/08 ,  C23C28/042 ,  C23C28/321 ,  C23C28/345 ,  C23C28/3455 ,  C23C30/00 ,  F01D5/288 ,  F05D2230/90 ,  F05D2300/2102 ,  F05D2300/611 ,  Y02T50/67 ,  Y02T50/671

摘要： A high emissivity (Hi-E) coating for use on the exhaust baffles of HIRSS systems. HIRSS systems were developed to reduce the infrared (IR) signature of helicopter engines. Increasing operating temperatures of helicopter engines have made the HIRSS systems less effective. An infrared coating applied over selected portions of the HIRSS reduces the IR of the system. The Hi-E coating comprises, in weight percent, 30-80% refractory oxide pigment, 5-20% binder, 1-15% potassium oxide, optionally up to about 15% glass-forming material and the balance refractory oxide powder. When applied to provide a surface finish of 1100Ra microinches or coarser, the coated HIRSS has a significantly reduced hemispherical reflectance in the IR frequency range.

摘要翻译： 用于HIRSS系统排气挡板的高发射率（Hi-E）涂层。 开发了HIRSS系统来减少直升机发动机的红外（IR）签名。 增加直升机发动机的运行温度使得HIRSS系统的效率降低。 在HIRSS的选定部分施加的红外涂层减少了系统的IR。 Hi-E涂层以重量％计含有30-80％的难熔氧化物颜料，5-20％的粘合剂，1-15％的氧化钾，任选的最多约15％的玻璃形成材料和余量的难熔氧化物粉末。 当应用于提供1100Ra / a或更大的表面光洁度时，涂覆的HIRSS在IR频率范围内具有显着降低的半球反射。

公开(公告)号：US06582834B2

公开(公告)日：2003-06-24

申请号：US09879691

申请日：2001-06-12

申请人： Bangalore Aswatha Nagaraj ,  Ching-Pang Lee ,  William Randolph Stowell ,  Aaron Dennis Gastrich

发明人： Bangalore Aswatha Nagaraj ,  Ching-Pang Lee ,  William Randolph Stowell ,  Aaron Dennis Gastrich

IPC分类号： B32B1504

CPC分类号： C23C16/045 ,  C23C16/40 ,  C23C28/00 ,  F01D5/288 ,  F05D2230/90 ,  F05D2300/611 ,  Y10T428/12458 ,  Y10T428/12611 ,  Y10T428/12618 ,  Y10T428/12736 ,  Y10T428/12944 ,  Y10T428/24975 ,  Y10T428/265

摘要： An anti-stick coating that inhibits the adhesion of contaminants that form deposits on the internal cooling passages of gas turbine engine components. The anti-stick coating is formed as an outer coating of the internal cooling passages, and preferably overlies an environmental coating such as a diffusion aluminide coating formed on the passage surfaces. The outer coating has a thickness of not greater than three micrometers, and is resistant to adhesion by dirt contaminants as a result of comprising at least one layer of tantala, titania, hafnia, niobium oxide, yttria, silica and/or alumina. The outer coating is preferably deposited directly on the environmental coating by chemical vapor deposition.