基于改进QPSO-SVR的航空发动机排气温度预测
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TH17; V231.1

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(国家自然科学基金委员会与中国民用航空局联合资助项目(U1633101) ;中央高效基本科研业务费中国民航大学专项资助项目(3122013H001)


Aeroengine Exhaust Gas Temperature Prediction Based on IQPSO-SVR
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    摘要:

    为了减少航空发动机排气温度的随机性对飞机安全飞行的影响,提出了改进量子粒子群优化支持向量回归机(improved quantum behaved particle swarm optimization support vector regression,简称IQPSO-SVR)的航空发动机排气温度预测模型,以A319飞机的V2500发动机为例,选取状态监控所监测的性能数数据作为训练样本和测试样本,其中航空发动机的高压转子转速、低压转子转速、燃油流量、高压压气机出口温度以及时间t作为模型的输入,以航空发动机排温度作为模型的输出,在不同组训练样本的条件下,对改进量子粒子群优化过的支持向量回归基模型进行测试,并与量子粒子群优化支持向量回归机(quantum behaved particle swarm optimization support vector regression,简称QPSO-SVR)、支持回归机 (support vector regression,简称SVR)进行对比。研究结果表明,改进量子粒子群优化支持向量回归机在航空发动机排气温度预测中相较其他两方法准确性更高,同时,在添加噪声的情况下,IQPSO-SVR也具有较好的预测能力。

    Abstract:

    In order to reduce the impact of aircraft engine exhaust gas temperature on aircraft safety flight, the IQPSO-SVR(improved quantum-behaved particle swarm optimization support vector regression) model was proposed to predict the aero-engine exhaust gas temperature, Take the V2500 engine of A319 aircraft as an example, the performance parameter data from condition monitoring are selected as both the training and test samples, The high pressure-rotor speed, low-pressure rotor speed, fuel flow and high pressure compressor outlet temperature of the aero engine are taken as the inputs of the model, The aero-engine exhaust gas temperature is used as the output of the model, The IQPSO-SVR model is tested under the condition of different training samples, and compared with QPSO-SVR(quantum behaved particle swarm optimization support vector regression) and SVR (support vectorregression), experimental results show that the quantum adaptive particle swarm optimization SVR is more accurate than the other two methods in the prediction of aero-engine exhaust gas temperature and the QAPSO-SVR has better prediction ability innoise reduction.

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  • 在线发布日期: 2019-05-13
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