公开(公告)号：US07326469B2

公开(公告)日：2008-02-05

申请号：US10907845

申请日：2005-04-18

申请人： David Forrest Dye ,  John Frederick Ackerman ,  Bhupendra Kumar Gupta ,  Jennifer Ann Pinson ,  Brian Thomas Pothier ,  Anthony Wayne Reynolds

发明人： David Forrest Dye ,  John Frederick Ackerman ,  Bhupendra Kumar Gupta ,  Jennifer Ann Pinson ,  Brian Thomas Pothier ,  Anthony Wayne Reynolds

IPC分类号： B32B15/04 ,  B32B18/00

CPC分类号： C23C16/06 ,  C23C16/44 ,  C23C16/448 ,  C23C28/322 ,  C23C28/345 ,  C23C28/3455 ,  F05B2230/90 ,  F05B2260/63 ,  F05B2260/95 ,  Y10T428/12611

摘要： A coating system for reducing the tendency for hydrocarbon fluids, such as fuels and oils, to form carbonaceous deposits that adhere to fluid containment surfaces. The coating system combines an outermost layer of platinum with an inner ceramic barrier layer of silica and/or tantala. The platinum layer catalyzes the hydrocarbon fluid to form particles of carbonaceous gum substances, and the ceramic barrier layer seals the containment surface from the hydrocarbon fluid to eliminate attachments points for deposits and inhibit interdiffusion between the platinum layer and the containment surface. The invention also encompasses a coating apparatus and process for depositing the coating system.

摘要翻译： 一种用于降低烃流体（例如燃料和油）倾向于形成粘附到流体容纳表面的碳质沉积物的涂层系统。 涂层系统将最外层的铂与二氧化硅和/或氧化铝的内部陶瓷阻挡层组合。 铂层催化碳氢化合物流体以形成碳质胶体物质的颗粒，并且陶瓷阻挡层将密封表面与烃流体密封，以消除沉积物的附着点，并抑制铂层与容纳表面之间的相互扩散。 本发明还包括用于沉积涂料体系的涂布装置和方法。

公开(公告)号：US20100081009A1

公开(公告)日：2010-04-01

申请号：US12239629

申请日：2008-09-26

申请人： Warren Arthur Nelson ,  David Vincent Bucci ,  David Forrest Dye ,  Anthony W. Reynolds

发明人： Warren Arthur Nelson ,  David Vincent Bucci ,  David Forrest Dye ,  Anthony W. Reynolds

IPC分类号： C23C4/10 ,  C23C4/18 ,  B32B9/00 ,  B05C5/00

CPC分类号： C23C8/02 ,  C23C4/123 ,  C23C4/18 ,  C23C26/00 ,  C23C28/042 ,  Y02T50/67 ,  Y02T50/6765

摘要： Methods and systems of applying a liquid precursor for a calcium-magnesium-aluminosilicate (CMAS) resistant coating to a turbine engine component are provided. In one embodiment, a method of manufacturing a turbine engine includes spraying a liquid compound, wherein the liquid component is stored with a carrier gas, applying the compound to a component of a turbine engine, such that the compound is disposed on a thermal barrier coating of the component, and forming an oxide layer on the thermal barrier coating of the component. In another embodiment, a system includes a turbine engine component and a sprayer containing a compound and a carrier gas, wherein the sprayer is configured to apply the compound to a thermal barrier coating of the component such that the compound forms an oxide on the thermal barrier coating.

摘要翻译： 提供了将用于钙镁镁硅酸盐（CMAS）抗性涂层的液体前体施加到涡轮发动机部件的方法和系统。 在一个实施例中，一种制造涡轮发动机的方法包括喷射液体化合物，其中液体组分与载气一起储存，将该化合物施加到涡轮发动机的部件上，使得化合物设置在热障涂层 的组分，并在组件的热障涂层上形成氧化物层。 在另一个实施方案中，系统包括涡轮发动机部件和含有化合物和载体气体的喷雾器，其中所述喷雾器被配置为将所述化合物施加到所述部件的热障涂层上，使得所述化合物在所述热障壁上形成氧化物 涂层。