scholarly journals Development of wood as an alternative fuel for large power-generating systems. Part I. Research on wood-burning gas turbines. Final report

1981 ◽  
Author(s):  
J. Hamrick ◽  
T. Hamrick
Keyword(s):  
Gas Turbines ◽  
Alternative Fuel ◽  
Final Report ◽  
Large Power ◽  
Wood Burning

Biodiesel as an Alternative Fuel in Siemens Dry Low Emissions Combustors: Atmospheric and High Pressure Rig Testing

2009 ◽  
Vol 132 (1) ◽  
Author(s):  
Kexin Liu ◽  
John P. Wood ◽  
Eoghan R. Buchanan ◽  
Pete Martin ◽  
Victoria E. Sanderson
Keyword(s):  
High Pressure ◽  
Gas Turbines ◽  
Alternative Fuel ◽  
Test Results ◽  
Combustion Dynamics ◽  
Pressure Drops ◽  
Air Inlet ◽  
Air Temperatures ◽  
Measured Probability ◽  
Industrial Gas Turbines

Atmospheric and high pressure rig tests were conducted to investigate the feasibility of using biodiesel as an alternative fuel to power industrial gas turbines in one of the world’s leading dry low emissions (DLE) combustion systems, the SGT-100. At the same conditions, tests were also carried out for mineral diesel to provide reference information to evaluate biodiesel as an alternative fuel. In atmospheric pressure rig tests, the likelihood of the machine lighting was identified based on the measured probability of the ignition of a single combustor. Lean ignition and extinction limits at various air temperatures were also investigated with different air assist pressures. The ignition test results reveal that reliable ignition can be achieved with biodiesel across a range of air mass flow rates and air fuel ratios (AFRs). In high pressure rig tests, emissions and combustion dynamics were measured for various combustor air inlet pressures, temperatures, combustor wall pressure drops, and flame temperatures. These high pressure rig results show that biodiesel produced less NOx than mineral diesel. The test results indicate that the Siemens DLE combustion system can be adapted to use biodiesel as an alternative fuel without major modification.

Fault Diagnosis in Gas Turbines Using a Model-Based Technique

1993 ◽  
Author(s):  
Graeme L. Merrington
Keyword(s):  
Gas Turbines ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Physical Processes ◽  
Important Conclusion ◽  
Large Power ◽  
The Past ◽  
Model Based ◽  
Dynamic Components ◽  
Reliable Methods

Reliable methods for diagnosing faults and detecting degraded performance in gas turbine engines are continually being sought. In this paper, a model-based technique is applied to the problem of detecting degraded performance in a military turbofan engine from take-off acceleration type transients. In the past, difficulty has been experienced in isolating effects of some of the physical processes involved. One such effect is the influence of the bulk metal temperature on the measured engine parameters during large power excursions. It will be shown that the model-based technique provides a simple and convenient way of separating this effect from the faster dynamic components. The important conclusion from this work is that good fault coverage can be gleaned from the resultant pseudo steady-state gain estimates derived in this way.

Design Concept for Large Output Graz Cycle Gas Turbines

2006 ◽  
Author(s):  
H. Jericha ◽  
W. Sanz ◽  
E. Go¨ttlich
Keyword(s):  
Gas Turbines ◽  
Fossil Fuels ◽  
Thermal Power ◽  
Cost Effective ◽  
Partial Solution ◽  
Combined Cycle ◽  
Design Concept ◽  
Air Separation ◽  
Pure Oxygen ◽  
Large Power

Introduction of closed cycle gas turbines with their capability of retaining combustion generated CO2 can offer a valuable contribution to the Kyoto goal and to future power generation. Therefore research and development work at Graz University of Technology since the nineties has led to the Graz Cycle, a zero emission power cycle of highest efficiency. It burns fossil fuels with pure oxygen which enables the cost-effective separation of the combustion CO2 by condensation. The efforts for the oxygen supply in an air separation plant are partly compensated by cycle efficiencies far higher than for modern combined cycle plants. Upon the basis of the previous work the authors present the design concept for a large power plant of 400 MW net power output making use of the latest developments in gas turbine technology. The Graz Cycle configuration is changed insofar, as condensation and separation of combustion generated CO2 takes place at the 1 bar range in order to avoid the problems of condensation of water out of a mixture of steam and incondensable gases at very low pressure. A final economic analysis shows promising CO2 mitigation costs in range of 20–30 $/ton CO2 avoided. The authors believe that they present here a partial solution regarding thermal power production for the most urgent problem of saving our climate.

Design Concept for Large Output Graz Cycle Gas Turbines

2007 ◽  
Vol 130 (1) ◽  
Author(s):  
H. Jericha ◽  
W. Sanz ◽  
E. Göttlich
Keyword(s):  
Gas Turbines ◽  
Fossil Fuels ◽  
Thermal Power ◽  
Cost Effective ◽  
Partial Solution ◽  
Combined Cycle ◽  
Design Concept ◽  
Air Separation ◽  
Pure Oxygen ◽  
Large Power

The introduction of closed cycle gas turbines with their capability of retaining combustion generated CO2 can offer a valuable contribution to the Kyoto goal and to future power generation. Therefore research and development work at the Graz University of Technology since the 1990s has led to the Graz Cycle, a zero emission power cycle of highest efficiency. It burns fossil fuels with pure oxygen which enables the cost-effective separation of the combustion CO2 by condensation. The efforts for the oxygen supply in an air separation plant are partly compensated by cycle efficiencies far higher than for modern combined cycle plants. Upon the basis of the previous work, the authors present the design concept for a large power plant of 400 MW net power output making use of the latest developments in gas turbine technology. The Graz Cycle configuration is changed, insofar as condensation and separation of combustion generated CO2 takes place at the 1 bar range in order to avoid the problems of condensation of water out of a mixture of steam and incondensable gases at very low pressure. A final economic analysis shows promising CO2 mitigation costs in the range of $20–30/ton CO2 avoided. The authors believe that they present here a partial solution regarding thermal power production for the most urgent problem of saving our climate.

Gas Turbines in Alternative Fuel Applications: How to Predict the Stability of Olefin-Containing Process Gases

2003 ◽  
Author(s):  
P. A. Glaude ◽  
O. Mahier ◽  
V. Warth ◽  
R. Fournet ◽  
M. Moliere ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Alternative Fuel ◽  
Liquefied Petroleum Gas ◽  
Gaseous Fuels ◽  
Process Gas ◽  
History Of ◽  
Process Gases ◽  
Heavy Duty Gas Turbine ◽  
The Stability

Throughout the history of combustion engines, the Heavy Duty Gas Turbine stands out as the most fuel-flexible prime mover in the field. This gas turbine (GT) is suited for a rich portfolio of gaseous fuels that include: natural gas, liquefied petroleum gas, coal and biomass-derived syngases, and a great variety of process gases with diverse compositions (hydrogen, carbon monoxide, olefins, etc.). Process gas fuels provide a promising array of alternative fuel opportunities in the major sectors of the industry such as the Coal, Oil & Gas, Steel, Chemical and Petrochemical branches. In an increasingly uncertain fuel environment, this significant match between gas turbine capabilities and the energy schemes of industrial plants can lead to further business opportunities.

Finite Element Transient Modelling for Aero-Thermo-Mechanical Analysis of Whole Gas Turbine Engine

2019 ◽  
Author(s):  
Sabrina Giuntini ◽  
Antonio Andreini ◽  
Bruno Facchini
Keyword(s):  
Gas Turbines ◽  
Structural Integrity ◽  
Numerical Procedure ◽  
Mechanical Analysis ◽  
Operating Conditions ◽  
Test Case ◽  
Large Power ◽  
Turbine Engine ◽  
Air System ◽  
Secondary Air

Abstract It is here proposed a numerical procedure aimed to perform transient aero-thermo-mechanical calculations of large power generation gas turbines. Due to the frequent startups and shutdowns that nowadays these engines encounter, procedures for multi-physics simulations have to take into account the complex coupled interactions related to inertial and thermal loads, and seal running clearances. In order to develop suitable secondary air system configurations, guarantee structural integrity and maintain actual clearances and temperature peaks in pre-established ranges, the overall complexity of the structure has to be reproduced with a whole engine modelling approach, simulating the entire machine in the real operating conditions. In the proposed methodology the aerodynamic solution providing mass flows and pressures, and the thermo-mechanical analysis returning temperatures and material expansion, are performed separately. The procedure faces the aero-thermo-mechanical problem with an iterative process with the aim of taking into account the complex aero-thermo-mechanical interactions actually characterizing a real engine, in a robust and modular tool, combining secondary air system, thermal and mechanical analysis. The heat conduction in the solid and the fluid-solid heat transfer are computed by a customized version of the open source FEM solver CalculiX®. The secondary air system is modelled by a customized version of the embedded CalculiX® one-dimensional fluid network solver. In order to assess the physical coherence of the presented methodology the procedure has been applied to a test case representative of a portion of a real engine geometry, tested in a thermal transient cycle for the assessment of the interaction between secondary air system properties and geometry deformations.

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