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1/10th Scale Model Tests of a Centre-line Tiltrotor: Conversion between rotary and fixed wing modes

机译:1/10尺度模型测试中心线Tiltrotor:旋转和固定机翼模式之间的转换

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In the centre-line tiltrotor configuration considered here, the rotors are mounted on the aircraft centre-line to allow the wings to be optimised without the constraints of carrying wing tip mounted rotors. Both approaches (wing tip mounted and centre-line mounted) provide the major advantage of speed and range over other edgewise operating rotorcraft. As described elsewhere, the centre-line configuration offers the additional important benefits of a more compact, agile design with improved field of view. The challenge is optimising the aerodynamics and control of the proprotors and airframe for rotary and winged flight over the complete flight envelope, and in particular the conversion process between helicopter and airplane modes. A 1/10~(th) scale model of a centre-line tiltrotor is being used. The airframe will develop to have the same general layout as that proposed for the full scale aircraft but targeted for a 10 kg take-off weight and to be operated safely within the flight envelopes of conventional fixed and rotary wing radio-controlled models. The test programme has four stages of investigation: hover rig, helicopter mode, airplane mode, and conversion. For the hover rig, the airframe is reduced to just landing skids so that it is flown as a meshing rotor helicopter. For the helicopter, airplane and conversion testing, the full fuselage and fixed wing surfaces are used, with a conventional wheeled, fixed undercarriage. The conversion testing starts with the rotors tilted to different fixed. For the full mode the pilot is free to fly all the flight modes, using conversion as appropriate. Flight test results to date are discussed.
机译:在这里考虑的中心线Tiltrotor配置中,转子安装在飞机中心线上,以允许翼在没有承载翼尖安装转子的约束的情况下进行优化。两种方法(机翼尖端安装和中心线安装)提供速度和范围的主要优点和其他边缘操作旋翼机。如其他地方所述,中心线配置提供了更紧凑,敏捷设计的额外重要优势,并改善了改进的视野。挑战是在完全飞行包络上优化对旋转和飞行飞行的扶手和机身的空气动力学和控制,特别是直升机和飞机模式之间的转换过程。使用中心线倾斜仪的1/10〜(Th)比例模型。机身将开发成具有相同的普通布局,如满量程飞行器所提出的,但是针对10kg起飞重量,并且在传统固定和旋转无线电控制模型的飞行信封内安全地操作。测试程序有四个调查阶段:悬停钻机,直升机模式,飞机模式和转换。对于悬停钻井平台,机身将减少到仅降落的滑块,使其成为啮合转子直升机。对于直升机,飞机和转换测试,使用完整的机身和固定翼面,具有传统的轮式固定底盘。转换测试从转子倾斜到不同固定的转换测试。对于全模式,飞行员可以自由地飞行所有飞行模式,适当使用转换。讨论了迄今为止的飞行测试结果。

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