Title: Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine

Abstract

A transition duct system (10) for delivering hot-temperature gases from a plurality of combustors in a combustion turbine engine is provided. The system includes an exit piece (16) for each combustor. The exit piece may include an arcuate connecting segment (36). An arcuate ceramic liner (60) may be inwardly disposed onto a metal outer shell (38) along the arcuate connecting segment of the exit piece. Structural arrangements are provided to securely attach the ceramic liner in the presence of substantial flow path pressurization. Cost-effective serviceability of the transition duct systems is realizable since the liner can be readily removed and replaced as needed.

Inventors:

Wiebe, David J.

Issue Date:

Tue Nov 07 00:00:00 EST 2017

Research Org.:

SIEMENS ENERGY, INC. Orlando, FL (United States)

Sponsoring Org.:

USDOE

OSTI Identifier:

1407947

Patent Number(s):

9810434

Application Number:

15/002,437

Assignee:

SIEMENS ENERGY, INC.

Patent Classifications (CPCs):

F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES

F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

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F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES

F01D9/023 - {Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines

F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

F05D2260/232 - characterized by the cooling medium
F05D2300/20 - Oxide or non-oxide ceramics
F05D2300/6033 - Ceramic matrix composites [CMC]

F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS

F23R2900/00017 - Assembling combustion chamber liners or subparts
F23R2900/03044 - Impingement cooled combustion chamber walls or subassemblies
F23R3/002 - {Wall structures
F23R3/005 - {Combined with pressure or heat exchangers}
F23R3/007 - {constructed mainly of ceramic components}
F23R3/425 - {Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes}
F23R3/46 - Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings
F23R3/50 - Combustion chambers comprising an annular flame tube within an annular casing
F23R3/60 - Support structures

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DOE Contract Number:  

FE0023955

Resource Type:

Patent

Resource Relation:

Patent File Date: 2016 Jan 21

Country of Publication:

United States

Language:

English

Subject:

42 ENGINEERING