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Design and Control of a Proof-of-Concept Active Jet Engine Intake Using Shape Memory Alloy Actuators

机译:使用形状记忆合金作动器的概念验证型主动喷气发动机进气口的设计和控制

摘要

The design and control of a novel proof-of-concept active jet engine intake using Nickel-Titanium (Ni-Ti or Nitinol) shape memory alloy (SMA) wire actuators is used to demonstrate the potential of an adaptive intake to improve the fuel efficiency of a jet engine. The Nitinol SMA material is selected for this research due to the material's ability to generate large strains of up to 5 percent for repeated operations, a high power-to-weight ratio, electrical resistive actuation, and easy fabrication into a variety of shapes. The proof-of-concept engine intake employs an overlapping leaf design arranged in a concentric configuration. Each leaf is mounted on a supporting bar that rotates upon actuation by SMA wires electrical resistive heating. Feedback control is enabled through the use of a laser range sensor to detect the movement of a leaf and determine the radius of the intake area. Due to the hysteresis behavior inherent in SMAs, a nonlinear robust controller is used to direct the SMA wire actuation. The controller design utilizes the sliding-mode approach to compensate for the nonlinearities associated with the SMA actuator. Feedback control experiments conducted on a fabricated proof-of-concept model have demonstrated the capability to precisely control the intake area and achieve up to a 25 percent reduction in intake area. The experiments demonstrate the feasibility of engine intake area control using the proposed design.
机译:使用镍钛(Ni-Ti或镍钛诺)形状记忆合金(SMA)线促动器设计并控制新型概念性主动喷气发动机进气装置,以演示自适应进气装置改善燃油效率的潜力喷气发动机。选择Nitinol SMA材料是因为该材料具有产生高达5%的大应变以进行重复操作,高功率重量比,电阻驱动以及易于制造成各种形状的能力。概念验证的发动机进气口采用重叠的叶片设计,以同心的方式布置。每个叶片均安装在支撑杆上,该支撑杆在通过SMA线电阻加热驱动时旋转。通过使用激光距离传感器来检测叶子的运动并确定进气区域的半径,从而实现反馈控制。由于SMA固有的磁滞行为,因此使用了非线性鲁棒控制器来控制SMA导线的致动。控制器设计利用滑模方法来补偿与SMA执行器相关的非线性。在制造的概念验证模型上进行的反馈控制实验表明,可以精确控制进气面积并实现进气面积减少多达25%的能力。实验证明了使用提出的设计进行发动机进气区域控制的可行性。

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