首页> 外文OA文献 >A Demonstration of a Retrofit Architecture for Intelligent Control and Diagnostics of a Turbofan Engine
【2h】

A Demonstration of a Retrofit Architecture for Intelligent Control and Diagnostics of a Turbofan Engine

机译:涡轮风扇发动机智能控制和诊断的改造架构演示

摘要

A retrofit architecture for intelligent turbofan engine control and diagnostics that changes the fan speed command to maintain thrust is proposed and its demonstration in a piloted flight simulator is described. The objective of the implementation is to increase the level of autonomy of the propulsion system, thereby reducing pilot workload in the presence of anomalies and engine degradation due to wear. The main functions of the architecture are to diagnose the cause of changes in the engine s operation, warning the pilot if necessary, and to adjust the outer loop control reference signal in response to the changes. This requires that the retrofit control architecture contain the capability to determine the changed relationship between fan speed and thrust, and the intelligence to recognize the cause of the change in order to correct it or warn the pilot. The proposed retrofit architecture is able to determine the fan speed setting through recognition of the degradation level of the engine, and it is able to identify specific faults and warn the pilot. In the flight simulator it was demonstrated that when degradation is introduced into an engine with standard fan speed control, the pilot needs to take corrective action to maintain heading. Utilizing the intelligent retrofit control architecture, the engine thrust is automatically adjusted to its expected value, eliminating yaw without pilot intervention.
机译:提出了一种智能涡轮风扇发动机控制和诊断的改造架构,该架构可改变风扇速度命令以保持推力,并描述了其在无人驾驶飞行模拟器中的演示。实施的目的是提高推进系统的自主性水平,从而减少异常情况下的飞行员工作量以及由于磨损导致的发动机退化。该体系结构的主要功能是诊断发动机运行变化的原因,必要时警告飞行员,并根据变化来调整外环控制参考信号。这就要求改造控制体系结构必须具有确定风扇速度和推力之间变化的关系的能力,以及识别变化原因的智能,以便对其进行纠正或警告飞行员。提出的改造体系结构能够通过识别发动机的退化程度来确定风扇速度设置,并且能够识别出特定故障并警告飞行员。在飞行模拟器中,证明了在将降级引入具有标准风扇速度控制的发动机中时,飞行员需要采取纠正措施以保持航向。利用智能改造控制架构,发动机推力会自动调整到期望值,无需驾驶员干预即可消除偏航。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号