Invention Grant
- Patent Title: Transition duct arrangement in a gas turbine engine
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Application No.: US14549044Application Date: 2014-11-20
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Publication No.: US10024180B2Publication Date: 2018-07-17
- Inventor: Paul G. Hicks , William W. Pankey
- Applicant: Siemens Energy, Inc.
- Applicant Address: US FL Orlando
- Assignee: SIEMENS ENERGY, INC.
- Current Assignee: SIEMENS ENERGY, INC.
- Current Assignee Address: US FL Orlando
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F01D9/02

Abstract:
An arrangement for a gas turbine engine includes a combustor for producing a working medium by combustion of a mixture of fuel and an oxidant, a turbine section comprising a stationary vane carrier on which a first row of stationary vanes is arranged, and a transition duct for leading the working medium from the combustor to the turbine section. The transition duct has a forward end that adjoins the combustor and an aft end that adjoins the stationary vane carrier. The transition duct has a transition duct axis extending from the forward end to the aft end along a straight line. The transition duct axis is normal to a vane axis of a stationary vane in the first row of stationary vanes.
Public/Granted literature
- US20160146026A1 TRANSITION DUCT ARRANGEMENT IN A GAS TURBINE ENGINE Public/Granted day:2016-05-26
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