scholarly journals Overview of Gas Turbine Coal-Fired Combustor Concepts

1989 ◽  
Author(s):  
Edward L. Parsons ◽  
John W. Byam
Keyword(s):  
Gas Turbine ◽  
Heat Engine ◽  
Development Program ◽  
Department Of Energy ◽  
Primary Concern ◽  
Gas Turbine Combustor ◽  
Heat Engines ◽  
Program Objective ◽  
Conducting Research ◽  
Environmentally Sound

Since 1982, the Department of Energy (DOE), through the Morgantown Energy Technology Center (METC), has been conducting research for the purpose of verifying the feasibility of using coal fuels in heat engine applications. The heat engines of primary concern are the gas turbine and the diesel engine. The overall program objective is to develop the technology base for an environmentally sound, integrated heat engine system which will produce cost-competitive energy from coal. During the past 2 years the major emphasis of the gas turbine development program has been the coal-fueled combustors. This paper will review the current progress on coal-fueled gas turbine combustor development.

U.S. Department of Energy Coal-Fueled Gas Turbine Program: A Status Report

1988 ◽  
Author(s):  
John W. Byam ◽  
Nelson Rekos
Keyword(s):  
Gas Turbine ◽  
Heat Engine ◽  
Department Of Energy ◽  
Status Report ◽  
Primary Concern ◽  
Heat Engines ◽  
Program Objective ◽  
The Status ◽  
Conducting Research ◽  
Environmentally Sound

Beginning in 1982, the Department of Energy (DOE), through the Morgantown Energy Technology Center (METC), has been conducting research for the purpose of verifying the feasibility of using coal fuels in heat engine applications. The heat engines of primary concern are the gas turbine and the diesel engine. The overall program objective is to develop the technology base for an environmentally sound, integrated heat engine system which will produce cost-competitive energy from coal. This paper will present the status of the gas turbine portion of this program.

Hybrid Heat Engines: The Power Generation Systems of the Future

2000 ◽  
Author(s):  
Abbie Layne ◽  
Scott Samuelsen ◽  
Mark Williams ◽  
Patricia Hoffman
Keyword(s):  
Fuel Cell ◽  
Gas Turbine ◽  
Power Plants ◽  
Technology Development ◽  
Heat Engine ◽  
Combined Cycle ◽  
Heat Engines ◽  
Hybrid Concept ◽  
Hybrid Program ◽  
Power Generation Systems

A hybrid heat engine results from the fusion of a heat engine with a non-heat-engine based cycle (unlike systems). The term combined cycle, which refers to similar arrangements, is reserved for the combination of two or more heat engines (like systems). The resulting product of the integration of a gas turbine and a fuel cell is referred to here as a hybrid heat engine or “Hybrid” for short. The intent of this paper is to provide, to the gas turbine community, a review of the present status of hybrid heat engine technologies. Current and projected activities associated with this emerging concept are also presented. The National Energy Technology Laboratory (NETL) is collaborating with other sponsors and the private sector to develop a Hybrid Program. This program will address the issues of technology development, integration, and ultimately the demonstration of what may be the most efficient of power plants in the world — the Hybrid System. Analyses of several Hybrid concepts have indicated the potential of ultra-high efficiencies (approaching 80%). In the Hybrid, the synergism between the gas turbine and fuel cell provides higher efficiencies and lower costs than either system can alone. Testing of the first Hybrid concept has been initiated at the National Fuel Cell Research Center (NFCRC).

scholarly journals AGT 100 Project Summary

1988 ◽  
Author(s):  
H. E. Helms
Keyword(s):  
Gas Turbine ◽  
Automotive Industry ◽  
Heat Engine ◽  
Ceramic Materials ◽  
Transportation Systems ◽  
Department Of Energy ◽  
General Motors ◽  
Nasa Lewis Research ◽  
Technology Project ◽  
Si Engines

The Allison Gas Turbine Division of General Motors Corporation (GMC) completed the Advanced Gas Turbine Technology Project under contract to the National Aeronautics and Space Administration (NASA) Lewis Research Center (LeRC) using funding received from the Heat Engine Propulsion Division, Office of Transportation Systems in the Conservation and Renewable Energy Group of the Department of Energy (DOE) in the summer of 1987. This advanced, high risk work was initiated in the fall of 1979 under charter from the U. S. Congress to promote an engine for transportation that would provide an alternative to reciprocating spark-ignition (SI) engines for the U. S. automotive industry and simultaneously establish the feasibility of advanced ceramic materials for hot section components to be used in an automotive gas turbine (AGT).

Coal Fueled Aero-Derivative Gas Turbine: Design Approach

1988 ◽  
Author(s):  
M. W. Horner ◽  
P. E. Sabla ◽  
S. G. Kimura
Keyword(s):  
Gas Turbine ◽  
High Efficiency ◽  
Development Program ◽  
Small Scale ◽  
Water Mixture ◽  
Coal Fuel ◽  
Cost Of Energy ◽  
Annular Combustor ◽  
Environmentally Sound ◽  
Turbine Design

The direct use of coal as a gas turbine fuel offers the opportunity to burn coal in an environmentally sound manner at a competitive cost of energy. A development program is underway to verify the feasibility of using coal water mixture to fuel an aero-derivative gas turbine. This paper presents the overall program approach, required gas turbine design modifications, and reports the results from small-scale combustor test facilities. The GE LM500 gas turbine was selected for this program because of its high efficiency and size, which is appropriate for transportation and cogeneration markets. The LM500 gas turbine power system design will be modified to accommodate coal fuel and any required emissions control devices. The design for the modified annular combustor is complete and preparations for coal fired tests of a 140 degree annular sector combustor are in progress. The combustor design and test development are being supported by a component test program with a One Nozzle Segment Combustor and a single can combustor LM500 Turbine Simulator. These test facilities are providing results on coal water mixture handling and fuel nozzle design, air staging requirements, component metal temperatures, combustor temperature performance, ash deposition rates, and emissions abatement for NOx, SOx, and particulates.

Advanced Hydrogen Turbine Development Update

2012 ◽  
Author(s):  
Tim Bradley ◽  
John Marra
Keyword(s):  
Gas Turbine ◽  
System Integration ◽  
Technology Development ◽  
Development Program ◽  
Combined Cycle ◽  
Department Of Energy ◽  
Plant Performance ◽  
Materials Testing ◽  
Development Effort ◽  
Phase 2

Siemens Energy, Inc. was awarded a contract by the U.S. Department of Energy for the first two phases of the Advanced Hydrogen Turbine Development Program. The 3-Phase, multi-year program goals are to develop an advanced syngas, hydrogen and natural gas fired gas turbine fully integrated into coal-based Integrated Gasification Combined Cycle (IGCC) plants. The program goals include demonstrating: • A 3–5% point improvement in combined cycle efficiency above the baseline, • 20–30% reduction in combined cycle capital cost • Emissions of 2 ppm NOx @ 15% O2 by 2015. Siemens is currently well into Phase 2 of the program and has made significant progress in several areas. This includes the ability to attain the 2015 Turbine Program performance goals by developing component and systems level technologies, developing and implementing validation test plans for these systems and components, performing validation testing of component technologies, and performance demonstration through system studies. Siemens and the Advanced Hydrogen Turbine Program received additional funds from the American Recovery and Reinvestment Act (ARRA) in 2010. The additional funding serves to supplement budget shortfalls in the originally planned spend rate. The development effort has focused on engine cycles, combustion technology development and testing, turbine aerodynamics/cooling, modular component technology, materials/coatings technologies and engine system integration/flexibility considerations. High pressure combustion testing continues with syngas and hydrogen fuels on a modified premixed combustor. Advanced turbine airfoil concept testing continues. Novel manufacturing techniques were developed that allow for advanced castings and faster time to market capabilities. Materials testing continues and significant improvements were made in lifing for Thermal Barrier Coatings (TBC’s) at increased temperatures over the baseline. Studies were conducted on gas turbine/IGCC plant integration, fuel dilution effects, varying air integration, plant performance and plant emissions. The results of these studies and developments provide a firm platform for completing the advanced Hydrogen Turbine technologies development in Phase 2.

scholarly journals Ceramic Stationary Gas Turbine Development Program: Design and Life Assessment of Ceramic Components

1995 ◽  
Author(s):  
Paul F. Norton ◽  
Gary A. Frey ◽  
Hamid Bagheri ◽  
Aaron Flerstein ◽  
Chris Twardochleb ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Failure Modes ◽  
Development Program ◽  
The United States ◽  
Department Of Energy ◽  
Life Assessment ◽  
United States Department ◽  
Ceramic Component ◽  
Engine Operation

A program is being performed under the sponsorship of the United States Department of Energy, Office of Industrial Technology, to improve the performance of stationary gas turbines in cogeneration through the selective replacement of hot section components with ceramic parts. It is envisioned that the successful demonstration of ceramic gas turbine technology, and the systematic incorporation of ceramics in existing and future gas turbines will enable more efficient engine operation, resulting in significant fuel savings, increased output power, and reduced emissions. The engine selected for the program, the Centaur 50 (formerly named Centaur ‘H’) will be retrofitted with first stage ceramic blades, first stage ceramic nozzles, and a ceramic combustor liner. The engine hot section is being redesigned to adapt the ceramic parts to the existing metallic support structure. The program currently in Phase II focuses on detailed engine and component design, ceramic component fabrication, ceramic component testing, establishment of a long term materials property database, and the development and application of supporting technologies in the areas of life prediction and non-destructive evaluation. This paper outlines the design activities associated with the introduction of a ceramic first stage nozzle and two configurations of ceramic first stage turbine blade. In addition, probabilistic life assessment of the ceramic parts for major failure modes (fast fracture, slow crack growth and where relevant, creep and oxidation) will be discussed.

Ceramic Stationary Gas Turbine Development Program — Design and Test of a Ceramic Turbine Blade

1998 ◽  
Author(s):  
Oscar Jimenez ◽  
John McClain ◽  
Bryan Edwards ◽  
Vijay Parthasarathy ◽  
Hamid Bagheri ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Turbine Blade ◽  
Gas Turbines ◽  
Fuel Efficiency ◽  
Development Program ◽  
Field Testing ◽  
The United States ◽  
Department Of Energy ◽  
United States Department ◽  
Engine Operation

The goal of the Ceramic Stationary Gas Turbine (CSGT) Development Program, under the sponsorship of the United States Department of Energy (DOE), Office of Industrial Technologies (OIT), is to improve the performance (fuel efficiency, output power, and exhaust emissions) of stationary gas turbines in cogeneration through the selective replacement of hot section components with ceramic parts. This program, which is headed by Solar Turbines Incorporated and supported by various suppliers, and national research institutes, includes detailed engine and component design, procurement, and field testing. A major challenge in the successful introduction of ceramic parts into a gas turbine is the design of the interface between the ceramic parts and metallic hardware. A turbine blade, which incorporated a dovetail root, was designed with such considerations. A relatively thin compliant layer between the ceramic-metallic loading surface was considered for equalizing pressure face load distributions. Five monolithic siliocn nitride ceramic materials were considered: AS800 and GN10, AlliedSignal Ceramic Components; NT164, Norton Advanced Ceramics; SN281 and SN253, Kyocera Industrial Ceramics Corporation. The probability of survival using NASA/CARES for 30,000 hours of engine operation was calculated for each material. The blade frequencies, stresses, and temperatures were predicted. The influence of the dovetail angle was also analyzed to determine the most optimum configuration. Prior to engine installation all blades underwent extensive nondestructive evaluation and spin proof testing. This paper will review the design, life prediction, and testing of the first stage ceramic turbine blade for the Solar Turbines Centaur 5OS engine.

scholarly journals Catalytic Burners for Stationary Combustion Turbines: A Preliminary Design Analysis

1982 ◽  
Author(s):  
L. C. Angello ◽  
P. W. Pillsbury ◽  
J. L. Toof
Keyword(s):  
Gas Turbine ◽  
Development Program ◽  
Design Analysis ◽  
Preliminary Design ◽  
Gas Turbine Combustor ◽  
Combustion Technology ◽  
Catalytic Combustor ◽  
Multi Phase ◽  
Near Future ◽  
Low Nitrogen

The EPRI Stationary Gas Turbine Catalytic Combustor Development Program is a multi-year, multi-phase major contract effort. Its objectives are to design, develop and demonstrate a full-scale, field tested stationary gas turbine combustor, employing catalytic combustion technology for reduced NOx emissions. Its focus is the development of a practical and reliable catalytic combustor for current and near-future stationary gas turbine designs fired with low nitrogen (<500 ppm) distillate fuels. The purpose of this paper is to present the results of a preliminary design analysis conducted under the initial tasks of this program.

Hybrid Fuel Cell Heat Engines: Recent Efforts

2001 ◽  
Author(s):  
Abbie Layne ◽  
Scott Samuelsen ◽  
Mark Williams ◽  
Norman Holcombe
Keyword(s):  
Fuel Cell ◽  
Gas Turbine ◽  
Power Plants ◽  
State Energy ◽  
Technology Development ◽  
Heat Engine ◽  
Combined Cycle ◽  
Heat Engines ◽  
Hybrid Concept ◽  
Hybrid Program

A hybrid heat engine results from the fusion of a heat engine with a non-heat-engine based cycle (unlike systems). The term combined cycle, which refers to similar arrangements, is reserved for the combination of two or more heat engines (like systems). The resulting product of the integration of a gas turbine and a fuel cell is referred to here as a hybrid heat engine or “Hybrid” for short. The intent of this paper is to provide, to the gas turbine community, a review of the present status of hybrid heat engine technologies. Current and projected activities associated with this emerging concept are also presented. The National Energy Technology Laboratory (NETL) is collaborating with other sponsors and the private sector to develop a Hybrid Program. This program will address the issues of technology development, integration, and ultimately the demonstration of what may be the most efficient of power plants in the world—the Hybrid System. In the Hybrid, the synergism between the gas turbine and fuel cell provides higher efficiencies and lower costs than either system can alone. Testing of the first hybrid concept has been initiated at the National Fuel Cell Research Center (NFCRC). FuelCell Energy (FCE) will be testing its first hybrid in 2002. Honeywell’s hybrid program has just begun under the Solid State Energy Conversion Alliance (SECA). SECA fuel cells will ultimately be hybridized with turbines. A competitive SECA solicitation is planned for conceptual studies in 2003. Industry teams will be selected in 2004 to further develop hybrid fuel cell systems.

scholarly journals Application of RQL Coal Combustor Technology to Large Utility Gas Turbines

1993 ◽  
Author(s):  
C. Wilkes ◽  
R. A. Wenglarz ◽  
P. J. Hart ◽  
H. C. Mongia
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Power Plants ◽  
Heat Engine ◽  
Combined Cycle ◽  
Pulverized Coal ◽  
Department Of Energy ◽  
Cycle Performance ◽  
Proof Of Concept ◽  
Combustion System

This paper describes the application of Allison’s rich-quench-lean (RQL) coal combustor technology to large utility gas turbines in the 100 MWe+ class. The RQL coal combustor technology was first applied to coal derived fuels in the 1970s and has been under development since 1986 as part of a Department of Energy (DOE)-sponsored heat engine program aimed at proof of concept testing of coal-fired gas turbine technology. The 5 MWe proof of concept engine/coal combustion system was first tested on coal water slurry (CWS); it is now being prepared for testing on dry pulverized coal. A design concept to adapt the RQL coal combustor technology developed under the DOE program to large utility-sized gas turbines has been proposed for a Clean Coal V program. The engine and combustion system modifications required for application to coal-fueled combined cycle power plants using 100 MWe+ gas turbines are described. Estimates for emissions and cycle performance are given. Included are comparisons with a conventional pulverized coal plant that illustrates the advantages of incorporating a gas turbine on cycle efficiency and emission rate.

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