公开(公告)号：US20140271109A1

公开(公告)日：2014-09-18

申请号：US13834745

申请日：2013-03-15

Applicant: General Electric Company

Inventor： Jeremy Peter Latimer ,  Eric Richard Bonini ,  John Duong

IPC: F01D11/00

CPC classification number: F01D5/3007 ,  F01D5/085

Abstract: The present application and the resultant patent provide an axial compressor for a gas turbine engine. The compressor may include a rotor disk positioned along an axis of the compressor. The rotor disk may include a slot defined about a radially outer surface of the rotor disk, and the slot may include a slot planar surface facing away from the rotor disk. The compressor also may include a compressor blade coupled to the rotor disk via the slot. The compressor blade may include a platform positioned over the radially outer surface of the rotor disk, and the platform may include a platform sealing edge facing toward the rotor disk. The compressor further may include a gap defined between the platform sealing edge and the slot planar surface, wherein the gap is configured to control a flow of leakage air from a high-pressure side of the compressor blade to a low-pressure side of the compressor blade. The present application and the resultant patent further provide a related method of controlling stage-to-stage leakage in an axial compressor of a gas turbine engine.

Abstract translation: 本申请和所得专利提供了一种用于燃气涡轮发动机的轴向压缩机。 压缩机可以包括沿着压缩机的轴线定位的转子盘。 转子盘可以包括围绕转子盘的径向外表面限定的槽，并且槽可以包括面向转子盘的槽平面。 压缩机还可以包括经由槽连接到转子盘的压缩机叶片。 压缩机叶片可以包括定位在转子盘的径向外表面上方的平台，并且平台可以包括面向转子盘的平台密封边缘。 压缩机还可以包括限定在平台密封边缘和槽平面之间的间隙，其中间隙构造​​成控制从压缩机叶片的高压侧到压缩机的低压侧的泄漏空气流 刀。 本申请和所得专利进一步提供了一种在燃气轮机的轴向压缩机中控制级间泄漏的相关方法。

公开(公告)号：US20140083639A1

公开(公告)日：2014-03-27

申请号：US13705758

申请日：2012-12-05

Applicant: General Electric Company

Inventor： Eric Richard Bonini ,  Ronald Scott Bunker

IPC: B22D25/02

CPC classification number: B23P15/02 ,  B22D15/02 ,  B22D25/02 ,  B23H9/14 ,  B23H9/16 ,  B23K15/085 ,  B23K26/382 ,  B23K26/40 ,  B23K2103/02 ,  B23K2103/08 ,  B23K2103/16 ,  B23K2103/26 ,  B23P2700/06 ,  F01D5/187 ,  F05D2230/13 ,  F05D2230/21 ,  F05D2260/202 ,  Y02T50/672 ,  Y02T50/676 ,  Y10T29/49339 ,  Y10T29/49341 ,  Y10T29/49815

Abstract: A method of machining a component is provided. The component includes a substrate having an outer surface and an inner surface, where the inner surface defines at least one interior space. A core is disposed within each interior space. The method includes forming at least one hole in the substrate while the core is disposed within the respective interior space. Each hole extends through the substrate to provide fluid communication with the respective interior space. The method further includes removing the core from the respective interior space. The core may be a casting core or a subsequently formed core.

Abstract translation: 提供了一种加工部件的方法。 该部件包括具有外表面和内表面的基底，其中内表面限定至少一个内部空间。 每个内部空间内设置核心。 所述方法包括在所述芯设置在相应的内部空间内时在所述基板中形成至少一个孔。 每个孔延伸穿过衬底以提供与相应内部空间的流体连通。 该方法还包括从相应的内部空间移除芯。 芯可以是铸芯或随后形成的芯。