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Investigation on new low cost electronically controlled fuel metering systems for small gas turbine engines.

机译:对用于小型燃气轮机的新型低成本电子控制燃油计量系统的研究。

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摘要

This work introduces two new lost cost, electronically controlled fuel metering systems for small gas turbine engines, particularly applicable in remotely piloted vehicles. The first one incorporates a diaphragm operated flat-seat bypass valve to maintain a constant differential pressure across the metering valve, which is actuated by a digital linear actuator. In the second one, both the metering and the bypass valves are controlled by two independently operated digital linear actuators.; The mathematical models for the first fuel metering system, were created and used for computer simulation. Next, after preparing the experimental test set-up, the manufactured prototype was tested and the models for both the steady state and the dynamic response were validated. Three design optimization criteria, fuel flow linearity, low sensitivity to the design parameters changes and fast dynamic response were examined to improve the performance of the proposed fuel metering system. Finally, a multi-objective optimization technique was developed and implemented to obtain the best design parameters of the system.; For the second fuel metering system, first the mathematical models for both the steady state and dynamic response were developed. Next, due to the flexibility offered by this system, different control strategies for controlling the digital linear actuators during the normal operation mode of the actuators and also during the back-up operation modes were introduced and investigated. Finally, to investigate the impact of different control strategies on the dynamic response of the engine, a dynamic model for the engine was also developed and used.; At the end, four available fuel metering systems, including the two new ones, were compared regarding their deviation from the fuel flow linearity, dynamic response and the cost.
机译:这项工作引入了两个新的损失成本,用于小型燃气轮机的电子控制燃油计量系统,特别适用于远程驾驶车辆。第一个集成了一个隔膜操作的平座旁通阀,以维持整个计量阀的恒定压差,该压差由数字线性执行器驱动。在第二个中,计量阀和旁通阀均由两个独立操作的数字线性致动器控制。创建了第一个燃油计量系统的数学模型,并将其用于计算机仿真。接下来,在准备好实验测试装置之后,测试了制造的原型,并验证了稳态和动态响应的模型。对三个设计优化标准,燃油流量线性度,对设计参数变化的低敏感性以及快速的动态响应进行了研究,以改善建议的燃油计量系统的性能。最后,开发并实现了一种多目标优化技术,以获取系统的最佳设计参数。对于第二个燃油计量系统,首先开发了稳态和动态响应的数学模型。接下来,由于该系统提供的灵活性,引入并研究了在致动器的正常操作模式期间以及在备用操作模式期间用于控制数字线性致动器的不同控制策略。最后,为了研究不同控制策略对发动机动态响应的影响,还开发并使用了发动机动态模型。最后,比较了四个可用的燃油计量系统,包括两个新的燃油计量系统,它们偏离了燃油流量线性度,动态响应和成本。

著录项

  • 作者

    Mohtasebi, Seyer Saeid.;

  • 作者单位

    Concordia University (Canada).;

  • 授予单位 Concordia University (Canada).;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 193 p.
  • 总页数 193
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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