Relevant bibliographies by topics / Fuel rich combustion

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Fuel rich combustion'

Author: Grafiati
Published: 4 June 2021
Last updated: 8 February 2022

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Journal articles on the topic "Fuel rich combustion"

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Nakata, T., M. Sato, T. Ninomiya, and T. Hasegawa. "A Study on Low NOx Combustion in LBG-Fueled 1500°C-Class Gas Turbine." Journal of Engineering for Gas Turbines and Power 118, no. 3 (1996): 534–40. http://dx.doi.org/10.1115/1.2816680.

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Developing integrated coal gasification combined-cycle systems ensures cost-effective and environmentally sound options for supplying future power generation needs. The reduction of NOx emissions and increasing the inlet temperature of gas turbines are the most significant issues in gas turbine development in Integrated Coal Gasification Combined Cycle (IGCC) power generation systems. The coal gasified fuel, which is produced in a coal gasifier of an air-blown entrained-flow type has a calorific value as low as 1/10 of natural gas. Furthermore, the fuel gas contains ammonia when a gas cleaning
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Micklow, G. J., S. Roychoudhury, H. L. Nguyen, and M. C. Cline. "Emissions Reduction by Varying the Swirler Airflow Split in Advanced Gas Turbine Combustors." Journal of Engineering for Gas Turbines and Power 115, no. 3 (1993): 563–69. http://dx.doi.org/10.1115/1.2906744.

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A staged combustor concept for reducing pollutant emissions is currently under investigation. A numerical study was performed to investigate the chemically reactive flow with liquid spray injection for staged combustion. The staged combustor consists of an airblast atomizer fuel injector, a rich burn section, a converging connecting pipe, a quick mix zone, a diverging connecting pipe and a lean combustion zone. For computational efficiency, the combustor was split into two subsystems, i.e., the fuel nozzle/rich burn section and the quick mix/lean burn section. The current study investigates th
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Li, Chaolong, Zhixun Xia, Likun Ma, Xiang Zhao, and Binbin Chen. "Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity." Energies 12, no. 7 (2019): 1235. http://dx.doi.org/10.3390/en12071235.

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Scramjet based on solid propellant is a good supplement for the power device of future hypersonic vehicles. A new scramjet combustor configuration using solid fuel, namely, the solid fuel rocket scramjet (SFRSCRJ) combustor is proposed. The numerical study was conducted to simulate a flight environment of Mach 6 at a 25 km altitude. Three-dimensional Reynolds-averaged Navier–Stokes equations coupled with shear stress transport (SST) k − ω turbulence model are used to analyze the effects of the cavity and its position on the combustor. The feasibility of the SFRSCRJ combustor with cavity is dem
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MORITA, Takakazu, Kenichi TAKANO, Hidenori NAKAZAWA, Satoru YOSHIDA, and Yousuke TACHIBANA. "Combustion Characteristics of Fuel-Rich Solid Propellants." Proceedings of Conference of Kanto Branch 2004.10 (2004): 549–50. http://dx.doi.org/10.1299/jsmekanto.2004.10.549.

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Ahn, Kyubok, and Hwan-Seok Choi. "Combustion Dynamics of Swirl Coaxial Injectors in Fuel-Rich Combustion." Journal of Propulsion and Power 28, no. 6 (2012): 1359–67. http://dx.doi.org/10.2514/1.b34448.

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Chen, Yi, Li Fei, Liming He, Lei Zhang, Chunchang Zhu, and Jun Deng. "The Influence of Dielectric Barrier Discharge Plasma on the Characteristics of Aero-Engine Combustion Chamber." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 37, no. 2 (2019): 369–77. http://dx.doi.org/10.1051/jnwpu/20193720369.

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A test platform was developed to investigate the performance of aero-engine combustor by the dielectric barrier discharge (DBD) plasma assisted combustion (PAC) in the simulated maximum condition. Conventional combustion experiments and plasma-assisted combustion conditions were conducted to study the effect of PAC on the performances including average outlet temperature, combustion efficiency and pattern factor under four different excessive air coefficients five different voltages. The comparative experiment shows that the combustion efficiency is improved after PAC compared with the normal
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Cowell, L. H., R. T. LeCren, and C. E. Tenbrook. "Two-Stage Slagging Combustor Design for a Coal-Fueled Industrial Gas Turbine." Journal of Engineering for Gas Turbines and Power 114, no. 2 (1992): 359–66. http://dx.doi.org/10.1115/1.2906599.

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A full-size combustor for a coal-fueled industrial gas turbine engine has been designed and fabricated. The design is based on extensive work completed through one-tenth scale combustion tests. Testing of the combustion hardware will be completed with a high pressure air supply in a combustion test facility before the components are integrated with the gas turbine engine. The combustor is a two-staged, rich-lean design. Fuel and air are introduced in the primary combustion zone where the combustion process is initiated. The primary zone operates in a slagging mode inertially removing coal ash
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Wu, Horng-Wen, Tzu-Ting Hsu, and Rong-Fang Horng. "Hydrogen-Rich Gas for Clean Combustion in a Dual-Fuel Compression Ignition Engine." Journal of Clean Energy Technologies 5, no. 2 (2017): 135–41. http://dx.doi.org/10.18178/jocet.2017.5.2.358.

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Pein, Roland, and S. Anders. "INVESTIGATION OF FUEL-RICH BORON COMBUSTION IN A PRESSURIZED COMBUSTION BOMB." International Journal of Energetic Materials and Chemical Propulsion 5, no. 1-6 (2002): 427–37. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.460.

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Foelsche, Robert O., Joseph M. Keen, Wayne C. Solomon, Parker L. Buckley, and Edwin Corporan. "Nonequilibrium combustion model for fuel-rich gas generators." Journal of Propulsion and Power 10, no. 4 (1994): 461–72. http://dx.doi.org/10.2514/3.23796.

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Dissertations / Theses on the topic "Fuel rich combustion"

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Kronholm, David Franklin 1967. "Molecular weight growth pathways in fuel-rich combustion." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/8996.

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Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Chemical Engineering, 2000.<br>Includes bibliographical references.<br>Polycyclic aromatic hydrocarbons (P AH) and soot are formed when a hydrocarbon fuel is oxidized under fuel-rich conditions. The distinction between what constitutes the largest P AH molecule and the smallest soot particle is arbitrary; the formation processes of both can be placed under the heading of molecular weight growth. Evidence exists for the carcinogenicity of many P AH molecules. Soot is used as a component of dyes and as an additive to rubbers as
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Varella, Roberto Aliandro. "Analysis of plasma assisted combustion under rich-fuel conditions." Instituto Tecnológico de Aeronáutica, 2015. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3234.

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The recently increasing interest in plasma assisted combustion is motivated by new possibilities for ignition and flame stabilization, in addition to pollutant emission reduction and control. The plasma generates a chemical active environment producing radicals, excited species and ions thus increasing the combustion process reaction rate. In this work the effect of plasma assisted combustion phenomena in a premixed flame of natural gas-air is investigated by using pollutant emission gas analysis, optical emission spectroscopy and high speed imaging. The plasma is created by using a gliding-ar
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Weber, Matthew F. "Characterization of Combustion Dynamics in a Liquid Model Gas Turbine Combustor Under Fuel-Rich Conditions." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1562060065192189.

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Dannecker, Karin Margaret. "EFFECT OF COAL COMPOSITION ON FUEL-NITROGEN MECHANISMS DURING FUEL RICH COMBUSTION (STAGED, POLLUTANTS)." Thesis, The University of Arizona, 1985. http://hdl.handle.net/10150/275302.

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Bose, Arun Chand. "Pulverized coal combustion: Fuel nitrogen mechanisms in the rich post-flame." Diss., The University of Arizona, 1989. http://hdl.handle.net/10150/184635.

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Chemical kinetic mechanisms governing the fate of coal nitrogen in the fuel-rich stage of a pulverized-coal staged combustion process were investigated. Emphasis was on determination of the effects of coal rank, temperature and stoichiometric ratios on the speciation and rates of destruction of nitrogenous species and correlation of coal data by a unif1ed mechanism. The relative importance of homogeneous and heterogeneous mechanisms during post-flame interconversion reactions of the fuel nitrogen pool was quantified. Experiments with doped propane gas and a high- and low-grade coals, burned un
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Skoglund, Nils. "Ash chemistry and fuel design focusing on combustion of phosphorus-rich biomass." Doctoral thesis, Umeå universitet, Institutionen för tillämpad fysik och elektronik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-88505.

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Biomass is increasingly used as a feedstock in global energy production. This may present operational challenges in energy conversion processes which are related to the inorganic content of these biomasses. As a larger variety of biomass is used the need for a basic understanding of ash transformation reactions becomes increasingly important. This is not only to reduce operational problems but also to facilitate the use of ash as a nutrient source for new biomass production. Ash transformation reactions were examined in the present work using the Lewis acid-base concept. The model presented in
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Pastore, Andrea. "Syngas production from heavy liquid fuel reforming in inert porous media." Thesis, University of Cambridge, 2010. https://www.repository.cam.ac.uk/handle/1810/237704.

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In the effort to introduce fuel cell technology in the field of decentralized and mobile power generators, a hydrocarbon reformer to syngas seems to be the way for the market uptake. In this thesis, a potential technology is developed and investigated, in order to convert commercial liquid fuel (diesel, kerosene and biodiesel) to syngas. The fundamental concept is to oxidise the fuel in a oxygen depleted environment, obtaining hydrogen and carbon monoxide as main products of the reaction. In order to extend the flammability limit of hydrocarbon/air mixtures, the rich combustion experiments hav
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Eftekharzadeh, Nooshin 1965. "Simplified kinetic models describing the fate of coal nitrogen under fuel-rich combustion conditions." Thesis, The University of Arizona, 1994. http://hdl.handle.net/10150/278453.

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Twenty three sets of experimental data describing CO, CO₂, H₂, O₂, NO, NH₃, and HCN concentration profiles for fuel-rich pulverized coal combustion in plug flow configurations were correlated by a simple kinetic mechanism. A comprehensive mechanism covering the entire fuel-rich zone was formulated by combining models describing short and long time scale combustion. Short time scale phenomena (up to 0.6 seconds) including coal devolatilization were handled by developing global semi-empirical models based on fundamental concepts. Kinetic parameters for the proposed mechanism were estimated by us
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Lopez, David M. "Controlling fuel and diluent gas flow for a diesel engine operating in the fuel rich low-temperature-combustion mode." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/40455.

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Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.<br>Includes bibliographical references (p. 37).<br>The flow of a diluent gas supplied to a motoring engine was controlled at a diluent to air mass flow ratios of 10%, 30%, 50%, and 70%. This arrangement was a significant set up for running the engine in the Low-Temperature Combustion mode. The engine used was a 436 cc Yanmar Diesel engine, driven at constant 2200 rpm by a 10 hp AC powered dynamometer. Intake air flow was measured by a model FMA-903-V Air Velocity Transducer by Omega Engineering, Inc.,
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Boutazakhti, Mohamed. "The effect of jet mixing on the combustion efficiency of a hot, fuel-rich cross-flow." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape4/PQDD_0015/MQ54105.pdf.

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Books on the topic "Fuel rich combustion"

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Brabbs, Theodore A. Fuel-rich catalytic combustion of a high density fuel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Brabbs, Theodore A. Fuel-rich catalytic combustion of a high density fuel. Lewis Research Center, 1993.

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Brabbs, Theodore A. Fuel-rich catalytic combustion of a high density fuel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Hodgson, J. W. Investigation and demonstration of a rich combustor cold-start device for alcohol-fueled engines. National Renewable Energy Laboratory, 1998.

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Radial-bias-combustion and central-fuel-rich swirl pulverized coal burners for wall-fired boilers. Nova Science Publishers, 2009.

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Boutazakhti, Mohamed. The effect of jet mixing on the combustion efficiency of a hot, fuel-rich cross-flow. National Library of Canada, 2000.

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Hall, Robert J. Turbulent radiation effects in HSCT combustor rich zone: Prepared under contract NAS3-26618. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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A, Merritt Sylvia, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Fuel-rich catalytic combustion of a high density fuel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Fuel-rich catalytic combustion of jet-A fuel: Equivalence ratios 5.0 to 8.0. National Aeronautics and Space Administration, 1989.

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M, Gracia-Salcedo Carmen, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Fuel-rich catalytic combustion of jet-A fuel: Equivalence ratios 5.0 to 8.0. National Aeronautics and Space Administration, 1989.

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Book chapters on the topic "Fuel rich combustion"

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Uemichi, Akane, Ippei Kanetsuki, and Shigehiko Kaneko. "Combustion Oscillation Characteristics of Hydrogen-Rich Fuel." In Fluid-Structure-Sound Interactions and Control. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-7542-1_56.

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Pettersson, A., A.-L. Elledt, A. Moöler, B.-M. Steenari, and L.-E. Åmand. "The Impact of Zeolites During Co-Combustion of Municipal Sewage Sludge with Alkali and Chlorine Rich Fuels." In Proceedings of the 20th International Conference on Fluidized Bed Combustion. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-02682-9_140.

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Pang, WeiQiang, Luigi T. De Luca, XueZhong Fan, Oleg G. Glotov, and FengQi Zhao. "Combustion Properties." In Boron-Based Fuel-Rich Propellant. CRC Press, 2019. http://dx.doi.org/10.1201/9780429030680-6.

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"Fuel-Rich Chemistry and Soot Precursors." In Applied Combustion Diagnostics. CRC Press, 2002. http://dx.doi.org/10.1201/9781498719414-20.

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Pang, WeiQiang, Luigi T. De Luca, XueZhong Fan, Oleg G. Glotov, and FengQi Zhao. "Combustion Performance of Model Propellant with Boron and Boron-Containing Compounds." In Boron-Based Fuel-Rich Propellant. CRC Press, 2019. http://dx.doi.org/10.1201/9780429030680-7.

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Borisov, A. A. "IMPULSE PRODUCTION BY INJECTING FUEL-RICH COMBUSTION PRODUCTS IN AIR." In Combustion Processes in Propulsion. Elsevier, 2006. http://dx.doi.org/10.1016/b978-012369394-5/50035-4.

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Schofield, Keith. "The importance of the temperature, interaction time, and heterogeneous collision frequency constraints: fuel-rich or -lean differences." In Combustion Emissions. Elsevier, 2020. http://dx.doi.org/10.1016/b978-0-12-819126-2.00004-2.

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"Pollution Control." In Environmental Toxicology, edited by Sigmund F. Zakrzewski. Oxford University Press, 2002. http://dx.doi.org/10.1093/oso/9780195148114.003.0017.

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Coal is now used mainly as fuel for the production of electricity. Worldwide about 28% of commercial energy production depends on coal. In the United States it is about 31% and in some coal rich but oil poor countries such as China, Germany, Poland and the Czech Republic the figures are 73%, 56%, 95% and 86%, respectively (1). Because of the ample supply of available coal, dependence on coal as an energy source will probably remain high for some time to come. However, coal is the most polluting of all fuels; its main pollutants are sulfur dioxide and suspended particulate matter (SPM). Depending on its origin, coal contains between 1 and 2.5% or more sulfur. This sulfur comes in three forms: pyrite (FeS2), organic bound sulfur, and a very small amount of sulfates (2). Upon combustion, about 15% of the total sulfur is retained in the ashes. The rest is emitted with flue gases, mostly as SO2 but also, to a lesser extent, as SO3. This mixture is frequently referred to as SOx (2). The three basic approaches to the control of SOx emission are prepurification of coal before combustion, removal of sulfur during combustion, and purification of flue gases. The first approach, referred to as a benefication process, is based on a difference in specific gravity between coal (sp gr = 1.2–1.5) and pyrite (sp gr = 5). Although the technical arrangements may vary, in essence the procedure involves floating the crushed coal in a liquid of specific gravity between that of pure coal and that of pyrite. Coal is removed from the surface while pyrite and other minerals settle to the bottom. Coal benefication can reduce sulfur content by about 40% (2). Although gravity separation is presently the only procedure in use, research was initiated on microbial purification of coal. A research project conducted by the Institute of Gas Technology, with funding from the U.S. Department of Energy, was aimed at the development of genetically engineered bacteria capable of removing organic sulfur from coal. Inorganic sulfur can be removed by the naturally occurring bacteria Thiobacillus ferrooxidans, Thiobacillus thiooxidans, and Sulfolobus acidocaldarius (3).
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Basava, Venkata Appa Rao, Aditya Kolakoti, and Prasada Rao Kancherla. "IDI Engine With Alternate Fuels." In Handbook of Research on Advancements in Manufacturing, Materials, and Mechanical Engineering. IGI Global, 2021. http://dx.doi.org/10.4018/978-1-7998-4939-1.ch002.

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A plethora of experiments were conducted on IDI engine with various biodiesels (e.g., methyl esters of mahua, jatropha, rice bran, pongamia, palm, beef tallow, and waste cooking oils). Review of the results of these endeavors with various additives and blends with or without super charging of the engine are presented in this chapter. All these attempts have been concentrated to arrive at the best yield from a single cylinder engine. The recorded pressure changes during combustion, the derived heat release rates, and exhaust emissions are presented in the form of plots at various loads and at a constant speed. Engine cylinder vibrations (reflect combustion excitation) in the form of FFT and time waves were recorded at radial points and vertical on the cylinder body to assess the combustion propensity in all cases of studies. The results with relative benefits are enumerated.
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Emdadul Hoque, Md, and Fazlur Rashid. "Gasification Process Using Downdraft Fixed-Bed Gasifier for Different Feedstock." In Gasification [Working Title]. IntechOpen, 2021. http://dx.doi.org/10.5772/intechopen.96227.

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The use of conventional fuels is decreasing globally due to its limited reserves and negative impact on the environment. The associated cost of conventional fuels is increasing owing to the higher demand for conventional fuels. Hence, utilization methods of biomass to generate energy are of growing interest. Among different biomass feedstocks, rice husks, waste plastics, and sawdust are significantly available in the global environment. The annual generation amount of rice husk is approximately 120 million tons worldwide, with an annual energy generation potential of 109 GJ with a heating value of 15 MJ/kg. The gasification process is assumed to be the most effective biomass conversion method that can generate synthetic gas to operate IC engines, fuel cells, and boilers. Synthetic gas production from biomass using a gasification process is a significant source of future energy. Downdraft fixed-bed gasifiers are considered as a feasible option of biomass conversion in the gasification process. By optimizing the operating conditions of downdraft fixed-bed gasifier, such as reaction zone temperature, combustion zone temperature, intake air temperature, airflow rate, the humidity of intake air, a significant amount of synthetic gas can be produced from rice husks, waste plastic material, and sawdust.
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Conference papers on the topic "Fuel rich combustion"

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Lee, Dongeun, and Changjin Lee. "Fuel-rich Combustion Characteristics of Hybrid Rocket Engine." In 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3828.

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Rizk, N. K., and H. C. Mongia. "Ultra-Low NOx Rich-Lean Combustion." In ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1990. http://dx.doi.org/10.1115/90-gt-087.

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An investigation has been carried out of the influence of the geometry and operating parameters of the rich/quench/lean (RQL) combustion concept on the NOx emissions. The RQL combustor is a three stage, variable geometry system in which fuel is burned in a carefully controlled fuel rich and fuel lean environment. The data utilized in this investigation were obtained under a wide range of operation that simulates the maximum continuous power mode, and for fuels that represent the future distillate types. An expression based on residence time, reaction rates, and mixing rates in each of the comb
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BRABBS, THEODORE, R. ROLLBUHLER, and ERWIN LEZBERG. "Fuel-rich catalytic combustion - A fuel processor for high-speed propulsion." In 26th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2319.

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Poyyapakkam, Madhavan, John Wood, Steven Mayers, Andrea Ciani, Felix Guethe, and Khawar Syed. "Hydrogen Combustion Within a Gas Turbine Reheat Combustor." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-69165.

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This paper describes a novel lean premixed reheat burner technology suitable for Hydrogen-rich fuels. The inlet temperature for such a combustor is very high and reaction of the fuel/oxidant mixture is initiated through auto-ignition, the delay time for which reduces significantly for Hydrogen-rich fuels in comparison to natural gases. Therefore the residence time available for premixing within the burner is reduced. The new reheat burner concept has been optimized to allow rapid fuel/oxidant mixing, to have a high flashback margin and to limit the pressure drop penalty. The performance of the
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FOELSCHE, R., J. KEEN, W. SOLOMON, P. BUCKLEY, and E. CORPORAN. "Non-equilibrium combustion model for fuel rich gas generators." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2041.

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Bachovchin, Dennis M., and William F. Domeracki. "Rich-Quench-Lean Combustion for Multiple Fuels." In ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-gt-448.

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Westinghouse has developed a rich-quench-lean gas turbine combustor for use on multiple gaseous fuels. The design is based on variants of the Multi-Annular Swirl Burner (MASB) that was invented as a low-NOx topping combustor for the second generation PFBC process, utilizing high temperature vitiated air and high temperature NH3-rich fuel gas, both derived from coal. This Westinghouse RQL combustor is also capable of low-NOx performance using either natural gas or propane in vitiated air, as well as compressor air operation using syngas (coal- or biomass-derived fuel gas for IGCC), propane, or
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Slavinskaya, Nadezhda, Oskar Haidn, and Johan Steelant. "Kinetic Modeling for High Pressure, Fuel - Rich Methane / Oxygen Combustion." In 45th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-775.

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SCHADOW, K., E. GUTMARK, T. PARR, D. PARR, and K. WILSON. "Enhancement of fine-scale mixing for fuel-rich plume combustion." In 25th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-376.

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Weber, M., J. Song, and J. G. Lee. "Characterization of Dynamics of Unstable Fuel-Rich Flame." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-60121.

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Abstract The flame dynamics during unstable combustion occurring in a model gas turbine combustor under fuel-rich conditions analogous to idle and sub-idle conditions in an aero-engine is characterized by simultaneous measurement of flame emissions and dynamic pressure fluctuation as well as high-speed imaging. Pressure fluctuation during unstable combustion causes linearly increasing velocity fluctuation at the combustor inlet. The fluctuation level of CH*-band emission which is mainly from soot linearly increases with respect to the combustor inlet velocity fluctuation up to ∼40% of mean vel
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Herdin, G. R., F. Gruber, D. Plohberger, and M. Wagner. "Experience With Gas Engines Optimized for H2-Rich Fuels." In ASME 2003 Internal Combustion Engine Division Spring Technical Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/ices2003-0596.

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The gas engine is a very efficient possibility of a technological approach for the conversion of chemically bound energy into mechanical or electrical power. Degrees of efficiency achieved thus far through the electrification of natural gas amount to up to 45% depending on the engine size and further potentials are already being opened up. Gas engines therefore do not need to fear a comparison with diesel engines in terms of efficiency. The modern gas engines have considerable advantages regarding emissions. The state of the art for the NOx emissions of natural gas engines can presently be giv
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Reports on the topic "Fuel rich combustion"

1

Santoro, Robert J., and Virginia C. Klema. (DURIP) - Species and Temperature Measurements in Fuel Rich Combustion Regions. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada218568.

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