公开(公告)号：US11773734B2

公开(公告)日：2023-10-03

申请号：US15697913

申请日：2017-09-07

Applicant: General Electric Company

Inventor： Glen Harold Kirby ,  Suresh Subramanian ,  Suresh Viswanathan ,  James Dale Steibel

IPC: F01D5/28 ,  F01D25/00 ,  F01D9/04 ,  F23R3/00 ,  C04B41/00 ,  C04B41/52 ,  C04B41/89

CPC classification number: F01D5/288 ,  C04B41/009 ,  C04B41/52 ,  C04B41/89 ,  F01D5/282 ,  F01D9/04 ,  F01D25/005 ,  F23R3/007 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2240/11 ,  F05D2240/35 ,  F05D2250/181 ,  F05D2250/184 ,  F05D2250/294 ,  F05D2260/204 ,  F05D2300/222 ,  F05D2300/6033 ,  F23R2900/00018 ,  C04B41/52 ,  C04B41/4576 ,  C04B41/5096 ,  C04B41/52 ,  C04B41/5024 ,  C04B41/52 ,  C04B41/5042 ,  C04B41/522 ,  C04B41/52 ,  C04B41/5027 ,  C04B41/522

Abstract: A coated component, along with methods of its formation and use, is provided. The coated component may include a substrate having a surface with a plurality of cavities defined therein, a bond coating (e.g., including a silicon material) on the surface of the substrate within the cavities, and an environmental barrier coating over the surface of the substrate and encasing the bond coating within the cavities such that the bond coating, when melted, is contained within the cavities. Such a coated component may be, in one embodiment, a turbine component, such as a CMC component for use in a hot gas path of a gas turbine engine.

公开(公告)号：US20190084892A1

公开(公告)日：2019-03-21

申请号：US15710954

申请日：2017-09-21

Applicant: General Electric Company

Inventor： Suresh Subramanian ,  Mark Eugene Noe ,  James Dale Steibel ,  Jason David Shapiro ,  Brandon ALlanson Reynolds ,  Kurtis C. Montgomery ,  Jared Hogg Weaver ,  Daniel Gene Dunn

IPC: C04B37/00 ,  C04B35/80 ,  C04B35/657 ,  C04B35/628

Abstract: A ceramic matrix composite article includes a chemical vapor infiltration ceramic matrix composite base portion including ceramic fiber reinforcement material in a ceramic matrix material having between 0% and 5% free silicon. The ceramic matrix composite article further includes a melt infiltration ceramic matrix composite covering portion including a ceramic fiber reinforcement material in a ceramic matrix material having a greater percentage of free silicon than the chemical vapor infiltration ceramic matrix composite base portion.

公开(公告)号：US20190071358A1

公开(公告)日：2019-03-07

申请号：US15697895

申请日：2017-09-07

Applicant: General Electric Company

Inventor： Glen Harold Kirby ,  Suresh Subramanian ,  Suresh Viswanathan ,  James Dale Steibel

IPC: C04B35/565 ,  C04B35/584 ,  C04B35/628

Abstract: A coated component, along with method of forming the same, is provided. The coated component may include a substrate having a surface, a silicon-based bond coating on the surface of the substrate, and an EBC on the silicon-based bond coating. The silicon-based bond coating may include a silicon-phase contained within a refractory phase. The silicon-phase, when melted, is contained within the refractory phase and between the surface of the substrate and an inner surface of the environmental barrier coating. Such a coated component may be, in particular embodiments, a turbine component.

公开(公告)号：US10196315B2

公开(公告)日：2019-02-05

申请号：US15403633

申请日：2017-01-11

Applicant: General Electric Company

Inventor： Glen Harold Kirby ,  James Dale Steibel

IPC: C04B35/56 ,  C04B35/80 ,  C04B35/565

Abstract: Methods for forming a ceramic matrix composite (CMC) are generally provided. The method may include melt infiltrating a silicon mixture into a ceramic matrix composite preform, with the silicon mixture including SiGa, SiIn, or a mixture thereof. The silicon mixture may include silicon metal in combination with SiGa, SiIn, or the mixture thereof. Additionally, the silicon mixture may further include B within the SiGa, SiIn, or the mixture thereof (e.g., in the form of SiBGa, SiBIn, or a mixture thereof).

公开(公告)号：US20130167374A1

公开(公告)日：2013-07-04

申请号：US13685038

申请日：2012-11-26

Applicant: General Electric Company

Inventor： Glen Harold Kirby ,  James Dale Steibel ,  Nathaniel David Goss

IPC: C04B35/64 ,  F02C7/00 ,  B32B18/00

CPC classification number: C04B35/64 ,  B32B18/00 ,  C04B35/573 ,  C04B35/58092 ,  C04B35/591 ,  C04B35/6286 ,  C04B35/62863 ,  C04B35/62865 ,  C04B35/62868 ,  C04B35/62871 ,  C04B35/62894 ,  C04B35/806 ,  C04B2235/3418 ,  C04B2235/3826 ,  C04B2235/3839 ,  C04B2235/3856 ,  C04B2235/3873 ,  C04B2235/3886 ,  C04B2235/3891 ,  C04B2235/3895 ,  C04B2235/404 ,  C04B2235/424 ,  C04B2235/428 ,  C04B2235/48 ,  C04B2235/483 ,  C04B2235/5244 ,  C04B2235/5256 ,  C04B2235/5268 ,  C04B2235/614 ,  C04B2235/616 ,  C04B2235/658 ,  C04B2235/6581 ,  C04B2235/72 ,  C04B2235/728 ,  C04B2235/77 ,  C04B2235/80 ,  C04B2237/341 ,  C04B2237/365 ,  C04B2237/368 ,  C04B2237/38 ,  C04B2237/52 ,  C04B2237/525 ,  C04B2237/61 ,  F01D25/00 ,  F02C7/00 ,  F05D2300/2261 ,  F05D2300/6033 ,  H04W4/023 ,  H04W4/80 ,  Y10T29/49236 ,  Y10T428/249986

Abstract: A process for producing a silicon-containing CMC article. The process entails depositing one or more coating layers on silicon carbide (SiC) fibers, drawing the coated SiC fibers through a slurry to produce slurry-coated fiber material, and then processing the slurry-coated SiC fiber material to form unidirectional prepreg tapes. The tapes are stacked and then fired to yield a porous preform. The porous preform is then further densified by infiltrating the porosity therein to yield a CMC article. Infiltration can be achieved by a series of polymer infiltration and pyrolysis (PIP) steps, by melt infiltration (MI) after filling the porosity in the preform with carbon or one or more refractory metal, by chemical vapor infiltration (CVI), or by a combination of these infiltration techniques.

Abstract translation: 一种含硅CMC制品的制造方法。 该方法需要在碳化硅（SiC）纤维上沉积一个或多个涂层，通过浆料拉伸涂覆的SiC纤维以产生浆料涂覆的纤维材料，然后处理浆料涂覆的SiC纤维材料以形成单向预浸带。 将带材堆叠，然后烧制以产生多孔预制件。 然后通过渗透其中的孔隙来进一步致密化多孔预成型件，得到CMC制品。 渗透可以通过一系列聚合物渗透和热解（PIP）步骤，通过在通过化学气相渗透（CVI）或者通过化学气相渗透（CVI）填充碳或一种或多种难熔金属的预制件中填充孔隙之后的熔融渗透（MI） 这些渗透技术的结合。