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

机译:中线倾转器的1/10比例模型测试: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:在此处考虑的中线倾斜旋翼配置中,旋翼安装在飞机的中心线上,以使机翼得到优化,而不受携带机翼末端安装的旋翼的约束。两种方法(机翼末端安装和中心线安装)均提供了速度和航程的优势,超过了其他沿边运行的旋翼飞机。如其他地方所述,中心线配置还提供了其他更重要的优点,即具有更紧凑,更敏捷的设计以及更佳的视野。挑战在于优化螺旋桨和机身的空气动力学性能,以及在整个飞行包线内进行旋翼飞行和机翼飞行的控制,尤其是直升机和飞机模式之间的转换过程。正在使用中心线倾斜转子的1/10〜比例模型。机身的总体布局将与全尺寸飞机的总体布局相同,但目标是起飞重量为10千克,并且可以在常规固定翼和旋转翼无线电控制模型的飞行范围内安全运行。测试程序分为四个调查阶段:悬停钻机,直升机模式,飞机模式和转换。对于悬停钻机,机身被缩小为仅是着陆滑道,因此它可以作为啮合旋翼直升机飞行。对于直升机,飞机和转换测试,使用完整的机身和固定机翼表面,并使用常规的带轮固定式起落架。转换测试从转子倾斜到不同的固定位置开始。对于全模式,飞行员可以自由进行所有飞行模式的飞行,并进行适当的转换。讨论了迄今为止的飞行测试结果。

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