公开(公告)号：US20150345388A1

公开(公告)日：2015-12-03

申请号：US14292969

申请日：2014-06-02

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Paul Stephen DIMASCIO ,  Victor John MORGAN ,  Jason Robert PAROLINI ,  Glenn Curtis TAXACHER ,  Frederic Woodrow ROBERTS, JR. ,  Jacob John KITTLESON ,  John McConnell DELVAUX

IPC: F02C7/00 ,  B23K1/00 ,  B23P6/00 ,  C04B41/91 ,  B24B33/00 ,  C04B41/00 ,  C04B41/53 ,  C04B41/50 ,  C04B41/45 ,  C23C16/24 ,  C04B41/85

CPC classification number: F02C7/00 ,  B23K1/0018 ,  B23P6/002 ,  B23P6/007 ,  B24B33/00 ,  C04B41/009 ,  C04B41/4531 ,  C04B41/5025 ,  C04B41/5096 ,  C04B41/5144 ,  C04B41/53 ,  C04B41/85 ,  C04B41/87 ,  C04B41/88 ,  C04B41/91 ,  C23C16/24 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2300/6033 ,  Y10T156/10 ,  Y10T428/24355 ,  C04B35/00 ,  C04B35/80 ,  C04B41/4529 ,  C04B41/4539 ,  C04B41/5133 ,  C04B41/0072

Abstract: A process of producing a ceramic matrix composite gas turbine component and a ceramic matrix composite gas turbine component are provided. The process includes modifying a surface of the ceramic matrix composite gas turbine component to produce a modified surface with a surface roughness of less than 6 micrometers. The modifying is selected from the group of techniques consisting of applying unreinforced matrix plies to the surface, vapor depositing silicon on the surface, honing the surface, applying braze paste to the surface, and combinations thereof. The component includes a modified surface including a surface roughness of less than 6 micrometers. The modified surface being selected from the group consisting of unreinforced matrix plies applied to a surface of the ceramic matrix composite gas turbine component, silicon vapor deposited on the surface, a honed surface, a braze paste applied to the surface, and combinations thereof.

Abstract translation: 提供了陶瓷基复合燃气轮机部件和陶瓷基复合燃气轮机部件的制造方法。 该方法包括改变陶瓷基复合燃气轮机部件的表面以产生表面粗糙度小于6微米的改性表面。 修饰选自由将未增强的基质层施加到表面，在表面上蒸镀硅，珩磨表面，将钎焊膏施加到表面上的技术组合，以及它们的组合。 该组件包括包括小于6微米的表面粗糙度的改性表面。 所述改性表面选自施加到陶瓷基复合燃气轮机部件的表面的未增强基体层，沉积在表面上的硅蒸汽表面，珩磨表面，施加到表面上的钎焊膏及其组合。

公开(公告)号：US20230193765A1

公开(公告)日：2023-06-22

申请号：US18066664

申请日：2022-12-15

Applicant: General Electric Company

Inventor： Kathen Thomas KOTAY ,  Frederic Woodrow ROBERTS, JR.

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F05D2260/607

Abstract: A filter for an airfoil of a vane of a turbomachine is disclosed. The filter includes a mounting member for mounting to an endwall of the vane. The mounting member has a first flow exit opening defined therethrough for fluid communication with a cooling circuit of the airfoil. A screen frame is coupled to the mounting member to support a wire screen around the first flow exit opening, and a first wire screen is positioned over the screen frame. The screen frame has an exterior shape supporting the wire screen in a manner incapable of having a horizontal surface regardless of a circumferential position of the airfoil around an axis of the turbomachine. A related turbine vane and turbine system are also provided.

公开(公告)号：US20180363508A1

公开(公告)日：2018-12-20

申请号：US15623715

申请日：2017-06-15

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Matthew Troy HAFNER ,  Frederic Woodrow ROBERTS, JR. ,  Glenn Curtis TAXACHER

IPC: F01D25/26 ,  F01D25/00

CPC classification number: F01D25/26 ,  F01D25/005 ,  F05D2260/30 ,  F05D2300/175 ,  F05D2300/603

Abstract: A turbine component including an outer shroud arranged within a turbine and including opposed extending portions. An inner shroud shields the outer shroud from a gas flowing along a gas path within the turbine during its operation and including opposed first and second arcuate portions extending around and in direct contact with a corresponding extending portion of the outer shroud. A first pin and second pin have a respective first end and second end. The first arcuate portion having a first engagement region for engaging the first end, and second arcuate portion having a second engagement region for engaging the second end. In response to engagement of the first engagement region and the first end of the first pin, and engagement of the second engagement region and the second end of the second pin, the inner shroud is prevented from twisting relative to the outer shroud.

公开(公告)号：US20180363485A1

公开(公告)日：2018-12-20

申请号：US15623657

申请日：2017-06-15

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Matthew Troy HAFNER ,  Frederic Woodrow ROBERTS, JR. ,  Glenn Curtis TAXACHER

IPC: F01D11/00 ,  F01D9/04

Abstract: A turbine shroud assembly including an outer shroud arranged within a turbine and further comprising opposed extending portions. The turbine shroud assembly further including an inner shroud shielding the outer shroud from a gas flowing along a gas path within the turbine during operation of the turbine and comprising opposed first and second arcuate portions extending around and in direct contact with a corresponding extending portion of the outer shroud for supporting the inner shroud from the outer shroud. The turbine shroud assembly further including a spline seal extending between the first and second arcuate portions and positioned between the inner shroud and the outer shroud. The turbine shroud assembly further including at least one of the inner shroud, the outer shroud and the spline seal including at least one protrusion for maintaining positive retention of the spline seal during non-operation of the turbine.