公开(公告)号：US20160201491A1

公开(公告)日：2016-07-14

申请号：US14912476

申请日：2014-08-13

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Raymond SURACE ,  Eric A. HUDSON

IPC: F01D9/06 ,  F01D17/16

CPC classification number: F01D17/162 ,  F01D9/065 ,  F01D11/24 ,  F01D17/16 ,  F02C7/12 ,  F05D2260/205

Abstract: A variable area turbine arrangement according to an exemplary aspect of the present disclosure includes, among other things, a variable vane assembly and a secondary flow system associated with the variable vane assembly. Flow modulation of a cooling fluid through the secondary flow system is changed simultaneously with actuation of the variable vane assembly.

Abstract translation: 根据本公开的示例性方面的可变区域涡轮机布置包括与可变叶片组件相关联的可变叶片组件和二次流动系统。 通过二次流动系统的冷却流体的流动调节与可变叶片组件的致动同时改变。

公开(公告)号：US20160123165A1

公开(公告)日：2016-05-05

申请号：US14896738

申请日：2014-06-06

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Michael G. McCaffrey ,  Tracy A. Propheter-Hinckley ,  Raymond SURACE

IPC: F01D9/02 ,  F01D17/16

CPC classification number: F01D9/02 ,  F01D5/18 ,  F01D17/162 ,  F05D2230/60 ,  F05D2260/201 ,  F05D2300/20

Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a shell defining an interior, a spar extending into the interior and a first flange attached to the spar. The spar is configured to pivot to change a positioning of the shell.

Abstract translation: 根据本公开的示例性方面的部件包括限定内部的壳体，延伸到内部的翼梁和附接到翼梁的第一凸缘。 翼梁被配置为枢转以改变壳体的定位。

公开(公告)号：US20160186600A1

公开(公告)日：2016-06-30

申请号：US14909209

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Raymond SURACE

IPC: F01D17/16 ,  F01D9/06

CPC classification number: F01D17/162 ,  F01D9/041 ,  F01D9/06 ,  F02C9/20 ,  F05D2220/32

Abstract: A variable area turbine arrangement according to an exemplary aspect of the present disclosure includes, among other things, a first turbine section having at least a first variable vane row and a second turbine section downstream from the first turbine section and having at least a second variable vane row. A transition duct is disposed between the first turbine section and the second turbine section.

Abstract translation: 根据本公开的示例性方面的可变区域涡轮机布置包括第一涡轮部分，其具有至少第一可变叶片排和在第一涡轮部分下游的第二涡轮部分，并且具有至少第二变量 叶片排。 过渡管道设置在第一涡轮部分和第二涡轮部分之间。