公开(公告)号：US20160201489A1

公开(公告)日：2016-07-14

申请号：US14593998

申请日：2015-01-09

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Yong Weon Kim ,  Tsuhon Lin ,  Jeffrey Stephen Carullo

IPC: F01D9/04

CPC classification number: F01D9/047 ,  F01D5/189 ,  F01D9/02

Abstract: An insert tube of a turbine vane is disclosed. The insert tube includes a pressure side wall, a suction side wall opposite and spaced apart from the pressure side wall, a leading edge, and a trailing edge opposite the leading edge. The insert tube includes a plurality of cooling channels spaced along the pressure side wall. The insert tube includes an indented portion located between the trailing edge and the pressure side wall.

Abstract translation: 公开了一种涡轮叶片的插入管。 插入管包括压力侧壁，与压力侧壁相对且间隔开的吸力侧壁，前缘和与前缘相对的后缘。 插入管包括沿着压力侧壁间隔开的多个冷却通道。 插入管包括位于后缘和压力侧壁之间的凹入部分。

公开(公告)号：US09879554B2

公开(公告)日：2018-01-30

申请号：US14593998

申请日：2015-01-09

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Yong Weon Kim ,  Tsuhon Lin ,  Jeffrey Stephen Carullo

IPC: F01D9/04 ,  F01D5/18 ,  F01D9/02

CPC classification number: F01D9/047 ,  F01D5/189 ,  F01D9/02

Abstract: An insert tube of a turbine vane is disclosed. The insert tube includes a pressure side wall, a suction side wall opposite and spaced apart from the pressure side wall, a leading edge, and a trailing edge opposite the leading edge. The insert tube includes a plurality of cooling channels spaced along the pressure side wall. The insert tube includes an indented portion located between the trailing edge and the pressure side wall.

公开(公告)号：US20140099190A1

公开(公告)日：2014-04-10

申请号：US13646526

申请日：2012-10-05

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Christopher J. Meyer ,  Tsuhon Lin ,  Edward T. Ramirez

IPC: F01D25/14 ,  B23P6/00

CPC classification number: F01D25/14 ,  Y10T29/49726 ,  Y10T29/49732

Abstract: A turbine housing (430) includes a support housing (440) with an annular shape. The support housing (432) includes an outer surface (433) and an inner surface (434). The inner surface (434) is located radially inward from the outer surface (433). A plurality of cooling holes (431) extols through the support housing(440) from the outer surface (433) to the inner surface (434). The cooling holes (431) include a stadium shape. The stadium shape includes a rectangle with a top and bottom of a first length and ends capped with semicircles with a radius of a second length. The cooling holes (431) are disposed at an angle (98) from thirty to sixty degrees. The angle (98) is between a line (96) projected to the outer surface (433) from an axis of the turbine housing (430) and a line (97) extending through a center of each cooling hole (431) parallel to the first length.

Abstract translation: 涡轮壳体（430）包括具有环形形状的支撑壳体（440）。 支撑壳体（432）包括外表面（433）和内表面（434）。 内表面（434）从外表面（433）径向向内定位。 多个冷却孔（431）从外表面（433）向内表面（434）伸出支撑壳体（440）。 冷却孔（431）包括体育场形状。 体育场形状包括具有第一长度的顶部和底部的矩形，并以半径为第二长度的半圆封口。 冷却孔（431）以三十到六十度的角度（98°）设置。 角度（98）在从涡轮机壳体（430）的轴线突出到外表面（433）的线（96）和延伸穿过平行于所述涡轮机壳体（430）的每个冷却孔（431）的中心的线（97）之间 第一长。