Results 1 to 10 of about 49,628 (234)
Experimental Prediction of Lean Blowout Limits for 3kW Micro Gas Turbine Combustor fuelled with LPG [PDF]
INCAS Bulletin, 2021 The Lean Blowout Limit of the combustor is one of the important performance parameters for a gas turbine combustor design. This study aims to predict the total pressure loss and Lean Blowout (LBO) limits of an in-house designed swirl stabilized 3kW can ...
V. KIRUBAKARAN, David BHATT
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Energy Reports, 2023 Research on micro/meso combustor-based small-scale power plants is developing rapidly. This rapid development is motivated by a higher energy density than lithium-ion batteries.
Herman Saputro +5 more
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Multi-Fidelity Combustor Design and Experimental Test for a Micro Gas Turbine System
Energies, 2022 A multi-fidelity micro combustor design approach is developed for a small-scale combined heat and power CHP system. The approach is characterised by the coupling of the developed preliminary design model using the combined method of 3D high-fidelity ...
Yize Liu +6 more
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Machines, 2022 Heavy fuel combustion problems with startup and operation may significantly reduce the microturbine efficiency in small APUs (Auxiliary Power Units). The use of commercial automotive-derived turbochargers solves the design problems of compressors and ...
Luca Piancastelli +2 more
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Catalytic Combustor for Small Gas Turbines: Combustor Development [PDF]
Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications, 1989 As described previously in ASME papers, an effort has been underway to apply catalytic combustion for small gas turbines. To improve combustion efficiency at the engine operating conditions, two catalytic combustors have been developed. Both combustors showed high combustion efficiency and low NOx emissions in combustor rig tests. In engine tests, Type
J. Kitajima, S. Kajita
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Experimental study on the rotating detonation engine based on a gas mixture
Frontiers in Energy Research, 2023 A direct connection test of a rotating detonation engine was conducted. The outer and inner diameters of the annular combustors were 206 and 166 mm, respectively.
Sainan Xue +5 more
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Computer simulation for trimming exit temperature profile from low emission combustor [PDF]
Компьютерные исследования и моделирование, 2014 It is discussed peculiarities of forming gas temperature fields in gas turbine engine low emission combustors. It is shown the influence of burn-up rate on combustor outlet temperature and proposed recommendation for design the dilution system for the ...
K. S. Pugach
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Entropy, 2021 Computational Fluid Dynamics is a fundamental tool to simulate the flow field and the multi-physics nature of the phenomena involved in gas turbine combustors, supporting their design since the very preliminary phases.
Davide Bertini +2 more
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Alternate-Fueled Combustor-Sector Performance—Part A: Combustor Performance and Part B: Combustor Emissions [PDF]
ISRN Mechanical Engineering, 2012 Alternate aviation fuels for military or commercial use are required to satisfy MIL-DTL-83133F or ASTM D 7566 standards, respectively, and are classified as “drop-in’’ fuel replacements. To satisfy legacy issues, blends to 50% alternate fuel with petroleum fuels are acceptable.
D. T. Shouse +7 more
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Energies, 2021 Aiming at the problem of the narrow combustion stability boundary, a conical swirler was designed and constructed based on the concept of fuel distribution.
Yixiang Yuan +5 more
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