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HEAT-RELEASE ACTUATION FOR CONTROL OF MIXTURE-INHOMOGENEITY-DRIVEN COMBUSTION INSTABILITY

机译:用于控制混合物 - 不均匀性驱动的燃烧不稳定性的热释放致动

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A low-order heat-release model, which accounts for the impact of flame surface area and the equivalence ratio oscillations, was used in conjunction with system acoustics to design a hierarchy of control strategies designed to mitigate combustion instability. The model assumes premixed combustion which burns a mixture with a temporally dependent equivalence ratio at high Damkoehler number and low turbulence intensity (i.e., a wrinkled laminar flame). When the acoustic field is of the Helmholtz-resonator type, the instability is dominated by the ratio of the convective time lag between the primary fuel injection and the burning zone and the time constant of the resonant acoustics. The model was applied to a practical combustor, and the instability condition predicted agreed with the measurements. The model structure was then utilized to design several active control approaches which incorporated periodic fuel injection at an arbitrary location between the primary injector and the burning zone. We showed that by exploiting the instability mechanism, as captured by the model, one can add flexibility and robustness to the control design (e.g., where the injector is located, how much fuel is introduced, the settling time). Several control algorithms, including an integral controller located at the fuel supply, an integral-plus-proportional controller located at the burning zone, and a Posi-Cast controller located at an arbitrary location in between, are proposed. While we find that the secondary injector can be successful in suppressing the instability, irrespective of its location with respect to the flame zone, results show that the control effort and the robustness against uncertainty and changes in operating conditions depend on the delay associated with the combustion of the extra control fuel (i.e., the location of the injector and the control algorithm).
机译:甲低阶放热模型,其占火焰表面积的影响和当量比振荡,与系统结合声学被用于设计旨在减轻燃烧不稳定性的控制策略的分层结构。该模型假定预混合燃烧,其燃烧时在高Damkoehler数和低湍流强度(即,皱层流火焰)一个时间相关的当量比的混合物。当声场是亥姆霍兹谐振器型的,不稳定性是由主燃料喷射和燃烧区和共振声学时间常数之间的对流时间滞后之比支配。该模型适用于一实际燃烧器和不稳定性条件预测与测量值一致。然后该模型结构被利用来设计,其在主喷射器和燃烧区之间的任意位置引入周期性燃料喷射几个主动控制的方法。我们发现,通过利用不稳定性机制,如由模型捕获,可以增加灵活性和健壮性到控制设计(例如,其中所述喷射器的位置,多少燃料被引入,所述沉降时间)。几个控制算法,包括位于燃料供给积分控制器,定位在燃烧区中的积分加比例控制器,和位于两者之间的任意位置处的POSI-角色控制器,提出了建议。虽然我们发现,二次喷油器可以成功地相对于火焰区抑制不稳定,不论其位置,结果表明,控制力度,对不确定性和工作条件的变化鲁棒性取决于与燃烧相关的延迟额外的控制燃料(即,在喷射器的位置和控制算法)。

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