Results 11 to 20 of about 2,006 (138)
Thermal Release Characteristics of Aeroengine Combustor Outlet Modulated by Gliding Arc Plasma [PDF]
A gliding arc plasma (GAP) combustion dome is used to construct a diagnostic platform for the swirl combustor of aeroengines. Thermocouple measurements, particle image velocimetry, and spontaneous emission imaging are employed to measure the outlet ...
Lei Zhang +5 more
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Experimental Prediction of Lean Blowout Limits for 3kW Micro Gas Turbine Combustor fuelled with LPG [PDF]
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
doaj +1 more source
Multi-Fidelity Combustor Design and Experimental Test for a Micro Gas Turbine System
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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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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Experimental study on the rotating detonation engine based on a gas mixture
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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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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Computer simulation for trimming exit temperature profile from low emission combustor [PDF]
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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Experimental and Simulation Study on the Emissions of a Multi-Point Lean Direct Injection Combustor [PDF]
Spurred by the world’s attention to pollution emissions from commercial aero-engines, the International Civil Aviation Organization (ICAO) has made more stringent emission regulations for civil aircraft engines, especially the NOx emission.This paper ...
P. Zhu +5 more
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Aerothermal Performance and Soot Emissions of Reacting Flow in a Micro-Gas Turbine Combustor
Micro-gas turbines are used for power generation and propulsion in unmanned aerial vehicles. Despite the growing demand for electric engines in a world striving for a net zero carbon footprint, combustion gas turbines will continue to play a critical ...
Heyu Wang, Kai Hong Luo
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Study on Microwave-Assisted Ignition Using a Novel Aero-Engine Combustor
Microwave plasma can improve the performance of ignition and combustion, as well as reduce pollutant emissions. By designing a novel microwave feeding device, the combustor can be used as a cavity resonator to generate microwave plasma and improve the ...
Yunwei Zhang +4 more
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