公开(公告)号：WO2014197042A2

公开(公告)日：2014-12-11

申请号：PCT/US2014/023206

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： EARL, Jonathan J. ,  RICHARDSON, Carl S.

IPC: F01D9/00 ,  F01D11/00 ,  F02C7/20 ,  F02C7/28

CPC classification number: F01D9/04 ,  F01D9/041 ,  F01D11/005 ,  F01D25/246 ,  F05D2230/51 ,  F05D2240/12 ,  F05D2240/129 ,  F05D2240/57 ,  F05D2250/314 ,  Y02T50/671

Abstract: One exemplary embodiment of this disclosure relates to a stator segment. The stator segment includes a first circumferential end face, and a second circumferential end face. Further, the first and second circumferential end faces are misaligned relative to one another.

Abstract translation: 本公开的一个示例性实施例涉及定子段。 定子部分包括第一周向端面和第二圆周端面。 此外，第一和第二圆周端面相对于彼此不对准。

公开(公告)号：WO2014052800A1

公开(公告)日：2014-04-03

申请号：PCT/US2013/062258

申请日：2013-09-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： RICHARDSON, Carl S.

IPC: F01D25/24 ,  F02C7/00 ,  F01D9/00 ,  F02K3/00

CPC classification number: F01D25/246 ,  F01D9/042 ,  F05D2250/131 ,  F05D2260/30

Abstract: An assembly for a turbine engine includes a stator vane arrangement and an anti-rotation lug that is rotatably connected to a turbine engine case. The stator vane arrangement includes a platform, an airfoil and an anti-rotation slot. The platform extends circumferentially around an axial centerline and is engaged with the case. The airfoil extends radially from the platform and is arranged circumferentially around the centerline. The slot extends radially into the platform, and is mated with the lug. The lug is configured with a substantially equilateral polygonal geometry.

Abstract translation: 用于涡轮发动机的组件包括定子叶片装置和可旋转地连接到涡轮发动机壳体的防旋转凸耳。 定子叶片装置包括平台，翼型件和防旋转槽。 平台围绕轴线中心线周向延伸并与壳体接合。 翼型件从平台径向延伸并围绕中心线周向布置。 狭槽径向延伸到平台中，并与凸耳配合。 凸耳配置有基本上等边的多边形几何形状。

公开(公告)号：WO2015050739A1

公开(公告)日：2015-04-09

申请号：PCT/US2014/056864

申请日：2014-09-23

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： ROGERS, Mark J. ,  RICHARDSON, Carl S. ,  HAYFORD, Richard K. ,  CARMAN, Kenneth E. ,  EARL, Jonathan J.

IPC: F01D11/00 ,  F01D5/30 ,  F02C7/28

CPC classification number: F01D11/001 ,  F01D9/041 ,  F05D2260/38

Abstract: A vane seal system includes a non-rotatable vane segment that has an airfoil with a pocket at one end thereof. The pocket spans in an axial direction between forward and trailing sides, with respect to the airfoil, and in a lateral direction between open lateral sides. A seal member extends in the pocket. The seal member includes a seal element and at least one spring portion that is configured to positively locate the seal member in the axial direction in the pocket. A method for positioning the seal member in a vane seal system includes positively locating the seal member in the axial direction in the pocket using the spring portion.

Abstract translation: 叶片密封系统包括不可旋转的叶片段，其具有在其一端具有口袋的翼型件。 口袋相对于翼型件在前后两侧之间的轴向方向上跨过敞开的侧边之间的横向方向。 密封件在口袋中延伸。 密封构件包括密封元件和至少一个弹簧部分，其构造成沿着轴向方向将密封构件正确定位在口袋中。 用于将密封构件定位在叶片密封系统中的方法包括使用弹簧部分将密封构件沿轴向方向定位在凹穴中。

公开(公告)号：WO2015112306A2

公开(公告)日：2015-07-30

申请号：PCT/US2014/072434

申请日：2014-12-26

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： HAYFORD, Richard K. ,  ROGERS, Mark J. ,  CARMAN, Kenneth E. ,  RICHARDSON, Carl S. ,  EARL, Jonathan J.

IPC: F01D9/02 ,  F01D9/04 ,  F01D25/24

CPC classification number: F04D29/542 ,  F01D9/042 ,  F04D29/023 ,  F04D29/522 ,  F04D29/644 ,  F05B2220/302 ,  F05B2240/124 ,  F05B2280/10743 ,  F05B2280/50032 ,  F05D2220/3219 ,  F05D2230/642 ,  F05D2240/129 ,  F05D2300/177 ,  F05D2300/50212

Abstract: A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.

Abstract translation: 燃气涡轮发动机包括可滑动地支撑在内壳体护罩段中的周向阵列的叶片。 多个段彼此固定以提供环形发动机静态结构部分。 内壳护罩段和叶片具有彼此不同的材料性质。

公开(公告)号：WO2014197044A2

公开(公告)日：2014-12-11

申请号：PCT/US2014/023470

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： RICHARDSON, Carl S. ,  SZYMBOR, John A.

IPC: F01D9/02 ,  F01D25/28 ,  F02C7/20

CPC classification number: F01D9/041 ,  B23C3/16 ,  B23C3/18 ,  B23C2215/04 ,  B23C2215/045 ,  B23C2215/44 ,  B23C2260/68 ,  B23C2270/08 ,  B23Q3/06 ,  B23Q3/062 ,  B23Q3/063 ,  B25B11/02 ,  F01D25/246 ,  F05D2230/10 ,  F05D2230/14 ,  F05D2240/12 ,  F05D2300/501 ,  Y02T50/66 ,  Y02T50/672 ,  Y10T29/49316 ,  Y10T29/4932 ,  Y10T29/49336 ,  Y10T409/303752 ,  Y10T409/303808 ,  Y10T409/30868 ,  Y10T409/309016

Abstract: A vane tip machining fixture assembly includes a first clamp ring mountable to a fixture, the first clamp ring includes a rigid back ring mounted to a resilient ring.

Abstract translation: 叶片尖端加工夹具组件包括可安装到夹具的第一夹环，第一夹环包括安装到弹性环的刚性后环。