不同工况下旋流稳定常压LDI燃烧器压力信号的非线性动态分析

A. Torregrosa, Alberto Broatch Jacobi, Jorge García-Tíscar, Marc Rodríguez Pastor
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摘要

精益直喷(LDI)燃烧器是一项很有前途的技术,旨在减少新一代航空发动机的氮氧化物排放。然而,该技术的主要缺点之一是在某些操作条件下出现燃烧不稳定。为了研究这些问题,在CMT-Motores - tsamrmicos研究所建立了一个密闭的、大气的、涡流稳定的LDI燃烧器。在这种配置下,由喷射压力控制的空气质量流量、温度和燃油质量流量可以独立修改,以达到不同的燃烧状态。本文对等效比(0.3≤Φ≤0.8)、空气温度(50、100、150℃)和燃料质量流量(200、250、300、335、370 mg/s)进行了参数化研究,通过对燃烧室内压力信号的评估,评估了它们对系统动力学的影响。这些信号是用两个压阻式传感器获得的,它们以相同的轴向距离安装在燃烧室壁上,但位于燃烧室的两侧。对于一些感兴趣的变量组合,可以检测到大振幅的非稳态振荡。等效比的变化对压力信号的动态特性有深刻的影响,在接近精益极限(Φ = 0.3)或最丰富的测试条件(Φ = 0.8)时获得更稳定的配置。中程等效比值(0.4≤Φ≤0.7)显示出最不稳定的行为,具有随时间保持几乎恒定的大压力振荡(准周期状态)或经历其振幅突然变化的信号(间歇状态)。由于湍流旋流稳定喷雾火焰燃烧器可能会经历复杂的流动-火焰相互作用,从而导致这些燃烧状态的非线性行为,因此一些信号处理技术,如三维相空间重建或递归图,已经应用于实验数据,以便更好地了解这些高动态特征。
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Nonlinear Dynamic Analysis of the Pressure Signals on a Swirl-Stabilized Atmospheric LDI Burner Across Different Operating Conditions
Lean Direct Injection (LDI) burners are a promising technology aimed at reducing NOx emissions in new generation aeroengines. However, one of the main drawbacks of this technology is the appearance of combustion instabilities at certain operating conditions. In order to investigate these issues, a confined, atmospheric, swirl-stabilized LDI burner has been set up at the Institute CMT-Motores Térmicos. In this configuration, air mass flow, temperature, and fuel mass flow rate, which is controlled by the injection pressure, can be independently modified to reach different combustion states. In this paper, a parametric study of the equivalence ratio (0.3 ≤ Φ ≤ 0.8), air temperature (50, 100, 150 °C) and fuel mass flow rate (200, 250, 300, 335, 370 mg/s) has been performed to assess their influence on the dynamics of the system through the evaluation of the pressure signals inside the chamber. These signals have been acquired with two piezoresistive sensors flush-mounted to the combustor wall at the same axial distance but in opposite sides of the chamber. Large-amplitude unsteady oscillations are detected for some combinations of the variables of interest. Equivalence ratio variations are shown to affect deeply the dynamic features of the pressure signal, obtaining more stable configurations either close to the lean limit (Φ = 0.3) or at the richest condition tested (Φ = 0.8). Mid-range equivalence ratio values (0.4 ≤ Φ ≤ 0.7) are shown to display the most unstable behavior, featuring large pressure oscillations that remain nearly constant over time (quasi-periodic states) or signals that experience sudden variations in their amplitude (intermittent states). Since turbulent swirl-stabilized spray flame combustors may experience complex flow-flame interactions that could lead to nonlinear behavior of these combustion regimes, several signal processing techniques such as three-dimensional phase space reconstruction or recurrence plots have been applied to the experimental data in order to obtain better insight into these highly dynamic features.
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