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Journal articles on the topic 'Fuel rich'

Author: Grafiati

Published: 3 June 2025

Last updated: 31 July 2025

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1

Yang, Guang, Xinghua Xie, Qiang Xie, and Xuerui Wang. "Study on combustion properties of magnesium-rich propellant based on analysis of kneading mixture." International Journal of Energy 2, no. 1 (2023): 5–8. http://dx.doi.org/10.54097/ije.v2i1.5139.

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In order to improve the combustion performance of the magnesium fuel, the heat value and combustion temperature of the mixture and the propellant were analyzed. The results show that: At the kneading machine speed of 1600 r/min, the magnesium and aluminum-rich fuel was prepared by adding propellant, with a calorific value of 2420 kg / t. The propellant has high calorific value, low combustion temperature, low non-combustible content, no by-products of combustion products, and low environmental pollution. Rich fuel shall meet the following requirements in use: First of all, the rich fuel should

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2

Valluri, Siva Kumar, Ian Monk, Mirko Schoenitz, and Edward L. Dreizin. "FUEL-RICH ALUMINUM-METAL FLUORIDE THERMITES." International Journal of Energetic Materials and Chemical Propulsion 16, no. 1 (2017): 81–101. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.2018021842.

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3

Cui, Yong Zhang, Guang Peng Li, Wei Guang Xu, and Jian Bin Zhu. "Experimental Investigation of NO_x and CO Emissions from Fuel Rich-Lean Flame of Natural Gas." Advanced Materials Research 347-353 (October 2011): 3821–25. http://dx.doi.org/10.4028/www.scientific.net/amr.347-353.3821.

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NOx and CO emissions of fuel rich-lean flame of natural gas water heaters were experimentally investigated. Fuel-rich and fuel-lean flame with different air factors were analyzed separately. Emission of fuel-rich flame is CO whereas emission of fuel-lean is NOx, and fuel rich-lean ratio is the most important factor for NOx and CO emission. If fuel-rich flame α1 is changed with constant fuel-lean flame α2, NOx emission decreases and CO emission increases evidently. If α2 is changed with constant α1, NOx decreases slightly and CO increases initially and then decreases. Depressing fuel-lean flame

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4

Jung, Woosuk, Seungkwan Baek, Youngil Kim, Taesoo Kwon, Juhyun Park, and Sejin Kwon. "Ignition of Fuel-rich Propellant Coated with Ignition Support Material in the Ramjet Combustor Condition." Journal of the Korean Society of Propulsion Engineers 21, no. 4 (2017): 79–88. http://dx.doi.org/10.6108/kspe.2017.21.4.079.

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5

Huang, Y. F., W. H. Kuan, S. L. Lo, and C. F. Lin. "Hydrogen-rich fuel gas from rice straw via microwave-induced pyrolysis." Bioresource Technology 101, no. 6 (2010): 1968–73. http://dx.doi.org/10.1016/j.biortech.2009.09.073.

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6

Bade Shrestha, S. O., I. Wierzba, and G. A. Karim. "A Thermodynamic Analysis of the Rich Flammability Limits of Fuel-Diluent Mixtures in Air." Journal of Energy Resources Technology 117, no. 3 (1995): 239–42. http://dx.doi.org/10.1115/1.2835347.

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A simple approach is described for the calculation of the rich flammability limits of fuel-diluent mixtures in air for a wide range of initial temperatures based only on the knowledge of the flammability limit of the pure fuel in air at atmospheric temperature and pressure conditions. Various fuel-diluent mixtures that include the fuels methane, ethylene, ethane, propane, butane, carbon monoxide, and hydrogen, and the diluents nitrogen, carbon dioxide, helium, and argon have been considered. Good agreement is shown to exist between predicted values of the rich flammability limits and the corre

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7

Bhosale, Priti, and Yogini Mulay. "Renewable Fuel Production." Ecology, Environment and Conservation 30, Suppl (2024): S436—S440. http://dx.doi.org/10.53550/eec.2024.v30i06s.064.

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The growing global energy demand and the environmental concerns associated with fossils fuels have sparked a shift towards renewable and sustainable energy sources, such as bioethanol. Bioethanol, a renewable liquid biofuel is a potential solution to address the challenges of energy security and climate changes. Conventionally first-generation biofuels can be produced through fermentation of starch-rich biomass i.e sugars to ethanol. The article provides a comprehensive overview of the bioethanol production process, encompassing pretreatment, enzymatic hydrolysis, fermentation by various micro

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8

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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9

Valluri, Siva K., Daniela Bushiri, Mirko Schoenitz, and Edward Dreizin. "Fuel-rich aluminum–nickel fluoride reactive composites." Combustion and Flame 210 (December 2019): 439–53. http://dx.doi.org/10.1016/j.combustflame.2019.09.012.

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10

Li, Xuhui, Kunquan Li, Chunlei Geng, Hamed El Mashad, Hua Li, and Wenqing Yin. "An economic analysis of rice straw microwave pyrolysis for hydrogen-rich fuel gas." RSC Advances 7, no. 84 (2017): 53396–400. http://dx.doi.org/10.1039/c7ra11034k.

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11

Specchia, Stefania. "Hydrocarbons valorisation to cleaner fuels: H2-rich gas production via fuel processors." Catalysis Today 176, no. 1 (2011): 191–96. http://dx.doi.org/10.1016/j.cattod.2011.01.018.

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12

Yang, Jiabao, Yan Gong, Juntao Wei, Qinghua Guo, Fuchen Wang, and Guangsuo Yu. "Chemiluminescence diagnosis of oxygen/fuel ratio in fuel-rich jet diffusion flames." Fuel Processing Technology 232 (July 2022): 107284. http://dx.doi.org/10.1016/j.fuproc.2022.107284.

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13

Lyubovsky, Maxim, Lance L. Smith, Marco Castaldi, et al. "Catalytic combustion over platinum group catalysts: fuel-lean versus fuel-rich operation." Catalysis Today 83, no. 1-4 (2003): 71–84. http://dx.doi.org/10.1016/s0920-5861(03)00217-7.

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14

Zhao, Xiang, Zhi-xun Xia, Bing Liu, Zhong Lv, and Li-kun Ma. "Numerical study on solid-fuel scramjet combustor with fuel-rich hot gas." Aerospace Science and Technology 77 (June 2018): 25–33. http://dx.doi.org/10.1016/j.ast.2017.12.024.

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15

Feitelberg, A. S., and M. A. Lacey. "The GE Rich-Quench-Lean Gas Turbine Combustor." Journal of Engineering for Gas Turbines and Power 120, no. 3 (1998): 502–8. http://dx.doi.org/10.1115/1.2818173.

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The General Electric Company has developed and successfully tested a full-scale, F-class (2550°F combustor exit temperature), rich-quench-lean (RQL) gas turbine combustor, designated RQL2, for low heating value (LHV) fuel and integrated gasification combined cycle applications. Although the primary objective of this effort was to develop an RQL combustor with lower conversion of fuel bound nitrogen to NOx than a conventional gas turbine combustor, the RQL2 design can be readily adapted to natural gas and liquid fuel combustion. RQL2 is the culmination of a 5 year research and development effor

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16

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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17

Ahn, Kyubok, Seonghyeon Seo, and Hwan-Seok Choi. "Fuel-Rich Combustion Characteristics of Biswirl Coaxial Injectors." Journal of Propulsion and Power 27, no. 4 (2011): 864–72. http://dx.doi.org/10.2514/1.b34121.

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18

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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19

Bhat, V. K., R. H. Brahmbhatt, P. G. Shrotri, and Haridwar Singh. "Performance of Fuel-Rich Propellants for Ramjet Applications." Defence Science Journal 46, no. 5 (1996): 331–36. http://dx.doi.org/10.14429/dsj.46.4300.

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20

Okuyama, Masaaki, Katsunori Hanamura, Ryozo Echigo, and Hideo Yoshida. "Flame Structure of Super Fuel-Rich Premixed Flame." Transactions of the Japan Society of Mechanical Engineers Series B 61, no. 587 (1995): 2724–30. http://dx.doi.org/10.1299/kikaib.61.2724.

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21

Lindgren, Eric R., David W. Pershing, D. A. Kirchgessner, and D. C. Drehmel. "Fuel rich sulfur capture in a combustion environment." Environmental Science & Technology 26, no. 7 (1992): 1427–33. http://dx.doi.org/10.1021/es00031a022.

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22

Goroshin, S., I. Fomenko, and J. H. S. Lee. "Burning velocities in fuel-rich aluminum dust clouds." Symposium (International) on Combustion 26, no. 2 (1996): 1961–67. http://dx.doi.org/10.1016/s0082-0784(96)80019-1.

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23

Kohse-Höinghaus, Katharina, Michael Kamphus, Guillermo González Alatorre, Burak Atakan, Alexander Schocker, and Andreas Brockhinke. "Concentration and temperature measurement in fuel-rich flames." Comptes Rendus de l'Académie des Sciences - Series IV - Physics 2, no. 7 (2001): 973–82. http://dx.doi.org/10.1016/s1296-2147(01)01242-2.

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24

Song, Eunhye, and Juhun Song. "Modeling of kerosene combustion under fuel-rich conditions." Advances in Mechanical Engineering 9, no. 7 (2017): 168781401771138. http://dx.doi.org/10.1177/1687814017711388.

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The turbo-pump and turbine are driven by liquid fuel fed into a gas generator, where the fuel is oxidized with a liquid oxidizing agent. For stable operation of the turbine, the combustion temperature of the gas generator must be maintained below 1000 K. The thermodynamic characteristics of kerosene oxidation in the gas generator must be understood to optimize the design and operation conditions of the liquid-fueled rocket engine system. Herein, the 3-species surrogate mixture model for kerosene was selected, and the detailed Dagaut’s kerosene oxidation mechanism consisting of 225 chemical spe

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25

Ashgriz, N., C. H. Chiang, and S. K. Aggarwal. "Flame structure in fuel rich mono-dispersed sprays." International Communications in Heat and Mass Transfer 15, no. 6 (1988): 765–72. http://dx.doi.org/10.1016/0735-1933(88)90019-x.

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26

Carney, Joel R, James M Lightstone, Thomas P McGrath, and Richard J Lee. "Fuel-Rich Explosive Energy Release: Oxidizer Concentration Dependence." Propellants, Explosives, Pyrotechnics 34, no. 4 (2009): 331–39. http://dx.doi.org/10.1002/prep.200800037.

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27

Yao, Yizhi, Mingbo Sun, Menglei Li, et al. "Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode." International Journal of Aerospace Engineering 2024 (February 6, 2024): 1–13. http://dx.doi.org/10.1155/2024/4340688.

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The ejector mode of the Rocket-Based Combined-Cycle (RBCC) engine is characterized by high fuel consumption. This study is aimed at investigating the influence of the rocket fuel-rich degree on the RBCC engine’s performance under the ejector mode combined with simultaneous mixing and combustion (SMC). Numerical simulations were conducted for various rocket mixing ratios (Φ=1.6~3.2) under subsonic (Maf=0.9) and supersonic (Maf=1.8) flight conditions. It was observed that a high fuel-rich degree in the rocket plume negatively impacts the eject performance under all conditions. However, it improv

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28

Apicella, B., A. Ciajolo, R. Barbella, et al. "Size Exclusion Chromatography of Particulate Produced in Fuel-Rich Combustion of Different Fuels." Energy & Fuels 17, no. 3 (2003): 565–70. http://dx.doi.org/10.1021/ef020149r.

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29

Li, Jiun-Ming, Chiang Juay Teo, Po-Hsiung Chang, Lei Li, Kim Seng Lim, and B. C. Khoo. "Excessively Fuel-Rich Conditions for Cold Starting of Liquid-Fuel Pulse Detonation Engines." Journal of Propulsion and Power 33, no. 1 (2017): 71–79. http://dx.doi.org/10.2514/1.b36088.

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30

Sentko, M. M., S. Schulz, C. Weis, et al. "Experimental investigation of synthesis gas production in fuel-rich oxy-fuel methane flames." Fuel 317 (June 2022): 123452. http://dx.doi.org/10.1016/j.fuel.2022.123452.

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31

ZHANG, Hui, Rui ONOGI, Ryo YOSHIIE, Yasuaki UEKI, and Ichiro NARUSE. "Electrochemical characteristics of solid oxide fuel cells supplied with CO-rich fuel gases." Journal of Thermal Science and Technology 19, no. 1 (2024): 23–00525. http://dx.doi.org/10.1299/jtst.23-00525.

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32

Wei, Xiaolin, Tongmo Xu, and Shien Hui. "Burning low volatile fuel in tangentially fired furnaces with fuel rich/lean burners." Energy Conversion and Management 45, no. 5 (2004): 725–35. http://dx.doi.org/10.1016/s0196-8904(03)00183-3.

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33

Lee, Wen Jhy, Burhanettin Cicek, and Selim M. Senkan. "Chemical structures of fuel-rich and fuel-lean flames of chloroform/methane mixtures." Environmental Science & Technology 27, no. 5 (1993): 949–60. http://dx.doi.org/10.1021/es00042a019.

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34

Lee, Seungmoon, Seung-Kwun Yoo, Jaehoon Lee, and Jin-Won Park. "Hydrogen-rich fuel gas production from refuse plastic fuel pyrolysis and steam gasification." Journal of Material Cycles and Waste Management 11, no. 3 (2009): 191–96. http://dx.doi.org/10.1007/s10163-008-0248-7.

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35

XIEQI, M., B. CICEK, and S. SENKAN. "Chemical structures of fuel-rich and fuel-lean flames of CCl4/CH4 mixtures☆." Combustion and Flame 94, no. 1-2 (1993): 131–45. http://dx.doi.org/10.1016/0010-2180(93)90026-y.

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36

Wang, Guodong, Jing Suming, Guoqing Liu, and Xingyong Gao. "Review on the Synthesis and Properties of the Energetic Compound Containing Boron." Current Organic Chemistry 24, no. 10 (2020): 1097–107. http://dx.doi.org/10.2174/1385272824999200516180719.

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Boron possesses the second greatest heating value of any element that can be adopted as an energetic material in the processing of propellants and explosives. It has become the first choice as a high energy fuel for solid fuel-rich propellants because of its advantages of high theoretical combustion heat. In the actual condition, the combustion efficiency of boron-containing fuel-rich propellants is low, and the potential energy of boron cannot be fully utilized. The compound containing-boron can be used as a new way to improve the combustion efficiency of fuel-rich propellants. In this paper,

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37

Lee, Chang Yeop, and Se Won Kim. "Experimental Study on Advanced Reburning for NOx Reduction by Pulsating Injection of Reburn Fuel." Applied Mechanics and Materials 704 (December 2014): 7–11. http://dx.doi.org/10.4028/www.scientific.net/amm.704.7.

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Reburning technology has been developed to adopt various commercial combustion systems. Fuel lean reburning is an advanced reburning method to reduce NOx economically without using burnout air, however it is not easy to get high NOx reduction efficiency. In the fuel lean reburning system, the localized fuel rich eddies are used to establish partial fuel rich regions so that the NOx can react with hydrocarbon radical restrictively. In this paper, a new advanced reburning method which supplies reburn fuel with oscillatory motion is introduced to increase NOx reduction rate effectively. To clarif

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38

Shaykin, A. P., and I. R. Galiev. "Influence Intensity Turbulence on the Width of the Zone Chemical Reactions and Speed Distribution of Methane-Hydrogen Flame." Siberian Journal of Physics 14, no. 4 (2019): 69–73. http://dx.doi.org/10.25205/2541-9447-2019-14-4-28-69-73.

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The prospects using methane-hydrogen fuel in power plants are shown. The effect of turbulence intensity on propagation velocity and width of the zone of chemical reactions methane-hydrogen flame in combustion chamber of variable volume is investigated. The article shows that effect of turbulence intensity on propagation velocity and flame width depends on fuel excess coefficient. During combustion of stoichiometric fuel-air mixtures, an increase in turbulence leads to a more noticeable increase in flame velocity than when burning poor and rich mixtures. It was experimentally found that increas

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39

Fyffe, John R., Mark A. Donohue, Maria C. Regalbuto, and Chris F. Edwards. "Mixed combustion–electrochemical energy conversion for high-efficiency, transportation-scale engines." International Journal of Engine Research 18, no. 7 (2016): 701–16. http://dx.doi.org/10.1177/1468087416665936.

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This article discusses an approach to exceeding current peak exergy efficiencies of approximately 50% for transportation-scale engines. A detailed model was developed for an internal combustion engine and a fuel cell, where the internal combustion engine is operated under fuel-rich conditions to produce a hydrogen-rich exhaust gas as a fuel for the fuel cell. The strategy of using combustion and electrochemical energy conversion processes has been shown to reduce reaction-related exergy losses while providing the balance of plant necessary to achieve efficient thermal management. Prior approac

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40

He, Na, Xifei Gao, Yanping Xin, et al. "Boron-based combustion modifiers on combustion performance of boron-based fuel-rich propellants." Journal of Physics: Conference Series 2891, no. 2 (2024): 022003. https://doi.org/10.1088/1742-6596/2891/2/022003.

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Abstract This paper investigates the effects of different boron-based combustion modifiers on the rheological, combustion and energy release characteristics of boron-based fuel-rich propellants. The results show that boron-based high-energy ionic salts (B1, B2, B3) and boron-based metallic fuels (Mg-Al-B), when combined with (AB+TAB)/HTPB mixed systems, exhibit superior rheological characteristics. The B2 and Mg-Al-B agglomerated particles demonstrate low apparent activation energy and high reaction rate constants, facilitating the rapid combustion of boron-based fuel-rich propellants. Further

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41

Azad, Abdul-Majeed, and Desikan Sundararajan. "A Phenomenological Study on the Synergistic Role of Precious Metals and the Support in the Steam Reforming of Logistic Fuels on Monometal Supported Catalysts." Advances in Materials Science and Engineering 2010 (2010): 1–15. http://dx.doi.org/10.1155/2010/681574.

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Clean power source utilizing vast logistic fuel reserves (jet fuels, diesel, and coal) would be the main driver in the 21st century for high efficiency. Fuel processors are required to convert these fuels into hydrogen-rich reformate for extended periods in the presence of sulfur, and deliver hydrogen with little or no sulfur to the fuel cell stack. However, the jet and other logistic fuels are invariably sulfur-laden. Sulfur poisons and deactivates the reforming catalyst and therefore, to facilitate continuous uninterrupted operation of logistic fuel processors, robust sulfur-tolerant catalys

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42

Rathi, Nikunj, and P. A. Ramakrishna. "Attaining Hypersonic Flight with Aluminum-Based Fuel-Rich Propellant." Journal of Propulsion and Power 33, no. 5 (2017): 1207–17. http://dx.doi.org/10.2514/1.b36463.

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43

Chen, D. M., S. P. Luh, T. K. Liu, G. K. Wu, and H. C. Perng. "COMBUSTION STUDY OF BORON-BASED FUEL-RICH SOLID PROPELLANT." International Journal of Energetic Materials and Chemical Propulsion 2, no. 1-6 (1991): 375–85. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v2.i1-6.220.

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44

Lee, Dongeun, and Changjin Lee. "Fuel-Rich Combustion Characteristic of a Combined Gas Generator." Journal of the Korean Society for Aeronautical & Space Sciences 43, no. 7 (2015): 593–600. http://dx.doi.org/10.5139/jksas.2015.43.7.593.

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45

Thomas, Solomon, T. L. Varghese, S. K. Gupta, T. S. Ram, and V. N. Krishnamurthy. "Natural Rubber Based Fuel Rich Propellant for Ramjet Rocket." Defence Science Journal 42, no. 3 (1992): 141–46. http://dx.doi.org/10.14429/dsj.42.4373.

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46

Okuyama, Masaaki, Ryozo Echigo, Hideo Yoshida, Motoi Koda, and Katsunori Hanamura. "Spectral Radiation Properties of Super Fuel-Rich Premixed Flame." Transactions of the Japan Society of Mechanical Engineers Series B 60, no. 577 (1994): 3145–52. http://dx.doi.org/10.1299/kikaib.60.3145.

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47

Hansen, Nils, James A. Miller, Tina Kasper, et al. "Benzene formation in premixed fuel-rich 1,3-butadiene flames." Proceedings of the Combustion Institute 32, no. 1 (2009): 623–30. http://dx.doi.org/10.1016/j.proci.2008.06.050.

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48

Lamprecht, A., B. Atakan, and K. Kohse-Höinghaus. "Fuel-rich flame chemistry in low-pressure cyclopentene flames." Proceedings of the Combustion Institute 28, no. 2 (2000): 1817–24. http://dx.doi.org/10.1016/s0082-0784(00)80584-6.

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49

Edwards, Meredith C., and Joy Doran-Peterson. "Pectin-rich biomass as feedstock for fuel ethanol production." Applied Microbiology and Biotechnology 95, no. 3 (2012): 565–75. http://dx.doi.org/10.1007/s00253-012-4173-2.

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50

Guteša Božo, M., MO Vigueras-Zuniga, M. Buffi, T. Seljak, and A. Valera-Medina. "Fuel rich ammonia-hydrogen injection for humidified gas turbines." Applied Energy 251 (October 2019): 113334. http://dx.doi.org/10.1016/j.apenergy.2019.113334.

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