Invention Grant
- Patent Title: Transition duct for use in a turbine engine and method of assembly
- Patent Title (中): 用于涡轮发动机的过渡管和组装方法
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Application No.: US13624543Application Date: 2012-09-21
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Publication No.: US09222437B2Publication Date: 2015-12-29
- Inventor: Joseph Machnaim , Brian David Keith , Scott Michael Carson
- 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: General Electric Company
- Agent William Scott Andes
- Main IPC: F04D29/54
- IPC: F04D29/54 ; F02K3/065 ; B23P11/00 ; F01D9/02

Abstract:
A transition duct for use in a turbine engine is provided. The transition duct includes a radially inner wall and a radially outer wall positioned about the radially inner wall defining a flow passage therebetween. The radially outer wall extends and is contoured from an upstream end to a downstream end of the transition duct. As such, the slope of the radially outer wall increases from the upstream end to a predetermined axial location and decreases from the predetermined axial location to the downstream end.
Public/Granted literature
- US20140086739A1 TRANSITION DUCT FOR USE IN A TURBINE ENGINE AND METHOD OF ASSEMBLY Public/Granted day:2014-03-27
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