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Influence of Operating Conditions and Residual Burned Gas Properties on Cyclic Operation of Constant-Volume Combustion

机译:操作条件和残余燃烧气体性能对恒储燃烧循环运算的影响

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The pressure-gain combustion concept is a solution envisioned to increase the thermodynamic efficiency of gas turbines. This article addresses the behaviour of piston-less constant-volume combustion in relevant conditions of engine application. For this purpose, a lab-scale combustion vessel (0.3 L) is run in cyclic operation (10 Hz) with an improved control over the boundary conditions. This facility features the spark-ignited, turbulent combustion of n-decane directly injected in preheated air (423 K, 0.4 MPa), with an overall equivalence ratio of 0.9. Solenoid valves are used to perform the air intake and burnt gas exhaust. A 0D analysis is developed and used to compute the gas thermodynamic evolution based on the experimental pressure traces. The effect of the main operating parameters on the combustion process is discussed: ignition delay, exhaust pressure and wall temperature. The vessel is operated without scavenging, hence the exhaust pressure drives the amount and the temperature of residual burnt gas (16-39% according to the 0D analysis). Highly diluted cycles (exhaust pressure 0.2 MPa) exhibit a higher combustion efficiency, but have a longer combustion duration (3 times more) than those of low dilution (exhaust pressure 0.07 MPa). For a higher wall temperature representative of engine combustor (1000 K), the heat losses are directly reduced, which affects the residual burnt gas properties. This also influences the residual gas temperature (870-1030 K) as well as dilution (10-26%).
机译:压力增益燃烧概念是设想增加燃气涡轮机的热力学效率的解决方案。本文讨论活塞少恒容燃烧的发动机应用的相关条件的行为。为了这个目的,一个实验室规模的燃烧容器(0.3L)与在边界条件的改进控制运行在循环操作(10赫兹)。该设施设有正癸烷的火花点火,湍流燃烧在预热空气(423 K,0.4兆帕)直接注射,以0.9的总当量比。电磁阀被用于执行进气和燃烧废气排放。甲0D分析开发和用于计算基于实验压力迹线的气体热力学演化。讨论对燃烧过程的主要操作参数的影响:点火延迟,排气压力和壁温。该容器不清除操作,因此,排气压力驱动量和残余燃烧气体的温度(根据0D分析16-39%)。高度稀释的周期(排气压力为0.2MPa)表现出更高的燃烧效率,但具有比低稀释度(排气压力0.07兆帕)的较长的燃烧持续期(3倍以上)。对于更高的代表发动机燃烧器(1000 K)的壁温度,热损失直接还原,从而影响到残余燃烧气体性质。这也影响残留气体温度(870-1030 K)以及稀释(10-26%)。

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