Invention Grant
US09458732B2 Transition duct assembly with modified trailing edge in turbine system
有权
在涡轮机系统中具有改进的后缘的过渡管道组件
- Patent Title: Transition duct assembly with modified trailing edge in turbine system
- Patent Title (中): 在涡轮机系统中具有改进的后缘的过渡管道组件
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Application No.: US14063358Application Date: 2013-10-25
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Publication No.: US09458732B2Publication Date: 2016-10-04
- Inventor: Kevin Weston McMahan , Carl Gerard Schott , Clint Luigie Ingram , Gunnar Leif Siden , Sylvain Pierre
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D5/14

Abstract:
Transition duct assemblies for turbine systems and turbomachines are provided. In one embodiment, a transition duct assembly includes a plurality of transition ducts disposed in a generally annular array and comprising a first transition duct and a second transition duct. Each of the plurality of transition ducts includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of each transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct assembly further includes an aerodynamic structure defined by the passages of the first transition duct and the second transition duct. The aerodynamic structure includes a pressure side, a suction side, and a trailing edge, the trailing edge having a modified aerodynamic contour.
Public/Granted literature
- US20150114003A1 TRANSITION DUCT ASSEMBLY WITH MODIFIED TRAILING EDGE IN TURBINE SYSTEM Public/Granted day:2015-04-30
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