公开(公告)号：WO2014152238A3

公开(公告)日：2014-11-06

申请号：PCT/US2014027107

申请日：2014-03-14

Applicant: GEN ELECTRIC

Inventor： LUTHRA KRISHAN LAL ,  CORMAN GREGORY SCOT

IPC: C04B41/89 ,  C04B35/565 ,  C04B35/571 ,  C04B35/589 ,  C04B41/45 ,  C04B41/50 ,  C23C4/04 ,  C23C28/04 ,  F01D5/28

CPC classification number: F01D9/02 ,  C04B22/06 ,  C04B35/565 ,  C04B35/571 ,  C04B35/587 ,  C04B35/589 ,  C04B35/597 ,  C04B35/806 ,  C04B41/009 ,  C04B41/5024 ,  C04B41/5044 ,  C04B41/52 ,  C04B41/85 ,  C04B41/87 ,  C04B41/89 ,  C04B2235/3206 ,  C04B2235/3208 ,  C04B2235/3213 ,  C04B2235/3215 ,  C04B2235/3224 ,  C04B2235/3225 ,  C04B2235/3227 ,  C04B2235/3229 ,  C04B2235/3427 ,  C04B2235/3481 ,  C23C28/04 ,  C23C28/042 ,  C23C28/044 ,  F01D5/284 ,  F01D5/288 ,  F05D2300/6033 ,  Y02T50/672 ,  C04B41/455 ,  C04B41/4582 ,  C04B41/5045 ,  C04B41/5096 ,  C04B41/5059 ,  C04B41/522 ,  C04B41/5066

Abstract: The disclosure relates generally to recession resistant gas turbine engine articles that comprise a silicon containing substrate, and related coatings and methods. The present disclosure is directed, inter alia, to an engine article comprising a silicon substrate which is coated with a chemically stable porous oxide layer. The present disclosure also relates to articles comprising a substrate and a bond coat on top comprising a two phase layer of interconnected silicon and interconnected oxide, followed by a layer of silicon. The present disclosure further relates to a recession resistant article comprising an oxide in a silicon containing substrate, such that components of the silicon containing substrate is interconnected with oxides dispersed in the substrate and form the bulk of the recession resistant silicon containing article.

Abstract translation: 本公开总体上涉及包括含硅基底的抗衰退燃气涡轮发动机制品以及相关的涂层和方法。 本发明尤其涉及一种包含涂覆有化学稳定的多孔氧化物层的硅基底的发动机制品。 本发明还涉及包含基材和顶部上的粘合涂层的制品，其包含互连硅和互连氧化物的双相层，接着是硅层。 本公开还涉及在含硅基材中包含氧化物的抗衰退制品，使得含硅基材的组分与分散在基材中的氧化物相互连接并形成大部分抗衰退含硅制品。

公开(公告)号：WO2015041823A8

公开(公告)日：2016-03-31

申请号：PCT/US2014053034

申请日：2014-08-28

Applicant: GEN ELECTRIC

Inventor： LUTHRA KRISHAN LAL ,  CORMAN GREGORY SCOT ,  RAMAMURTHI BADRI NARAYAN

IPC: C04B35/80 ,  C04B35/00 ,  C04B38/00 ,  C04B41/45

CPC classification number: C04B35/806 ,  C04B35/565 ,  C04B35/58092 ,  C04B35/584 ,  C04B35/80 ,  C04B38/0003 ,  C04B38/0032 ,  C04B2235/3804 ,  C04B2235/3813 ,  C04B2235/3817 ,  C04B2235/3839 ,  C04B2235/3843 ,  C04B2235/483 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/5252 ,  C04B2235/5256 ,  C04B2235/614 ,  C04B2235/94

Abstract: The present disclosure relates to ceramic matrix composites made by chemical vapor infiltration, methods of making the ceramic matrix composites, and ceramic matrix composite turbine components for use in a hot gas pathway. A method of fabricating a ceramic matrix composite is provided that can include the steps of: (i) forming a plurality of holes in a ceramic matrix composite preform of desired shape; and (ii) densifying the preform by a chemical vapor infiltration process to form a part or most of the matrix. A ceramic matrix composite is also provided that can be used in hot combustion gases made according to the aforementioned ceramic matrix composite fabrication method described herein.

Abstract translation: 本公开内容涉及通过化学气相渗透制备的陶瓷基体复合材料，制备陶瓷基复合材料的方法，以及用于热气体通路中的陶瓷基复合涡轮机部件。 提供了一种制造陶瓷基复合材料的方法，其可以包括以下步骤：（i）在所需形状的陶瓷基复合预型件中形成多个孔; 和（ii）通过化学气相渗透法致密化预成型体以形成基体的一部分或大部分。 还提供了可用于根据本文所述的上述陶瓷基体复合制造方法制备的热燃气中的陶瓷基复合材料。