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SHOCKLESS EXPLOSION COMBUSTION: AN INNOVATIVE WAY OF EFFICIENT CONSTANT VOLUME COMBUSTION IN GAS TURBINES

机译:快速爆炸燃烧:燃气轮机高效恒量燃烧的创新方式

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摘要

Constant volume combustion (CVC) in gas turbines is a promising way to achieve a step change in the efficiency of such systems. The most widely investigated technique to implement CVC in gas turbine systems is pulsed detonation combustion (PDC). Unfortunately, the PDC is associated with several disadvantages, such as sharp pressure transitions, entropy generation due to shock waves, and exergy losses due to kinetic energy. This work proposes a new way to implement CVC in a gas turbine combustion system: shockless explosion combustion (SEC). This technique utilizes acoustic waves inside the combustor to fill and purge the combustion tube. The combustion itself is controlled via the ignition delay time of the fuel/lair mixture. By adjusting the ignition delay in a way such that the entire fuel/air volume undergoes homogeneous auto-ignition, no shock waves occur. Accordingly, the losses associated with a detonation wave are not present in the proposed system. Instead, a smooth pressure rise is created due to the heat release of the homogeneous combustion. The current article explains the SEC process in detail, and presents the identified challenges. Solutions to these challenges and the numerical and experimental approach are presented subsequently alongside with first preliminary results of the numerical studies.
机译:燃气轮机中的恒定体积燃烧(CVC)是实现此类系统效率逐步变化的有前途的方法。在燃气轮机系统中实施CVC的最广泛研究的技术是脉冲爆震燃烧(PDC)。不幸的是,PDC具有几个缺点,例如急剧的压力转变,由于冲击波而产生的熵以及由于动能而产生的能量损失。这项工作提出了一种在燃气轮机燃烧系统中实施CVC的新方法:无冲击爆炸燃烧(SEC)。该技术利用燃烧器内部的声波来填充和吹扫燃烧管。燃烧本身是通过燃料/巢穴混合物的点火延迟时间来控制的。通过以某种方式调节点火延迟,使整个燃油/空气量进行均匀的自动点火,不会产生冲击波。因此,在所提出的系统中不存在与爆震波相关的损失。相反,由于均匀燃烧的热量释放而产生了平稳的压力上升。当前文章详细解释了SEC流程,并提出了已确定的挑战。随后提出了这些挑战的解决方案以及数值和实验方法,以及数值研究的初步结果。

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