公开(公告)号：US20170159494A1

公开(公告)日：2017-06-08

申请号：US14960914

申请日：2015-12-07

Applicant: General Electric Company

Inventor： Steven Sebastian Burdgick

IPC: F01D25/24 ,  F01D9/04 ,  F01D5/02

CPC classification number: F01D25/246 ,  F01D5/02 ,  F01D9/041 ,  F01D9/042 ,  F05D2220/31 ,  F05D2240/128 ,  F05D2260/30

Abstract: Various embodiments include a steam turbine diaphragm nozzle segment, related assembly and steam turbine. Particular embodiments include a steam turbine diaphragm nozzle segment having: an airfoil having a contact surface for directing a flow of working fluid through a flow path; and a sidewall coupled with the airfoil and at least partially radially outboard of the airfoil, the sidewall having: a body contacting the airfoil; an axially upstream-extending hook extending axially from the body; a first notch adjacent the axially upstream-extending hook; an axially downstream-extending hook extending axially from the body; and a second notch adjacent the axially downstream-extending hook.

公开(公告)号：US09394797B2

公开(公告)日：2016-07-19

申请号：US13693610

申请日：2012-12-04

Applicant: General Electric Company

Inventor： Debabrata Mukhopadhyay ,  Steven Sebastian Burdgick ,  Prashant Prabhakar Sankolli ,  Moorthi Subramaniyan

IPC: F01D9/02 ,  F01D5/18 ,  F01D11/00

CPC classification number: F01D5/187 ,  F01D5/186 ,  F01D9/02 ,  F01D11/001 ,  F05D2220/31 ,  F05D2240/122

Abstract: Various embodiments include a steam turbine nozzle and turbomachinery including such a nozzle. In various particular embodiments, a steam turbine nozzle includes: a body having: a first sidewall and a second sidewall opposite the first sidewall; a pressure side and a suction side each extending between the first sidewall and the second sidewall; and a leading edge section at a first junction of the pressure side and the suction side, and a trailing edge section at a second junction of the pressure side and the suction side; and a bypass fluid conduit including: a channel having an opening to at least one of the first sidewall or the second sidewall; and an outlet passageway fluidly connected with the channel between the first sidewall and the second sidewall, the outlet passageway including a first opening on at least one of the pressure side of the body, the suction side of the body or the trailing edge section.

Abstract translation: 各种实施例包括蒸汽轮机喷嘴和包括这种喷嘴的涡轮机械。 在各种具体实施例中，蒸汽轮机喷嘴包括：主体，其具有：与第一侧壁相对的第一侧壁和第二侧壁; 压力侧和吸力侧，每个在所述第一侧壁和所述第二侧壁之间延伸; 以及在压力侧和吸力侧的第一接合处的前缘部分和在压力侧和吸力侧的第二接合处的后缘部分; 以及旁通流体导管，包括：通道，具有至少一个第一侧壁或第二侧壁的开口; 以及出口通道，其与所述第一侧壁和所述第二侧壁之间的通道流体连接，所述出口通道包括在所述主体的所述压力侧，所述主体的吸力侧或所述后缘部分中的至少一个上的第一开口。

公开(公告)号：US20140154065A1

公开(公告)日：2014-06-05

申请号：US13692541

申请日：2012-12-03

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Prashant Prabhakar Sankolli ,  Steven Sebastian Burdgick

IPC: F01D9/04

CPC classification number: F01D9/041 ,  F01D9/047 ,  F05D2220/31 ,  F05D2230/26

Abstract: Various embodiments include a turbomachine flow divider. In various particular embodiments, a flow divider for connecting with a first inner diaphragm ring and a second inner diaphragm ring of a turbomachine includes: a body section; and a pair of axially extending flanges extending from the body section, each of the axially extending flanges for engaging with the first inner diaphragm ring and the second inner diaphragm ring, respectively, wherein the flow divider is formed substantially of a rolled plate metal or a sheet metal.

Abstract translation: 各种实施例包括涡轮机分流器。 在各种具体实施例中，用于与涡轮机的第一内隔膜环和第二内隔膜环连接的分流器包括：主体部分; 以及从主体部分延伸的一对轴向延伸的凸缘，每个轴向延伸的凸缘分别与第一内隔膜环和第二内隔膜环接合，其中分流器基本上由轧制板金属或 钣金