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COMPOUND-SPLIT DRIVETRAINS FOR ROTORCRAFT

机译:旋翼机的复合动力传动装置

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The investigation presented in this paper is part of the international research project VARI-SPEED with the aim to invent a speed-variable drivetrain for different rotorcraft configurations to reduce the required propulsion power, which enables a modern and ecologically efficient aviation. The research is focused on drivetrain technologies for rotorcraft to enable a variable rotor speed. In the first part known variable transmission drivetrain technologies were listed. Evaluation parameters for usage of transmissions in rotorcraft were defined and rated with a utility analysis. The listed drivetrain technologies were evaluated according to their ability to fulfil the requirements of the evaluation parameters. It could be shown that continuously variable transmission power split gearboxes have the highest potential to be used in rotorcraft. Mechanical discrete variable transmission gearboxes may also have a potential to be used in rotorcraft but the shifting process could be a problem. In the next step the three power split gearbox configurations - Input Split, Output Split and Compound Split - were analysed according to their power split behaviour at different transmission ratios. The more power is transferred via the mechanical path the higher the efficiency is and the lower the additional mass is. In the investigation a spread of two was assumed. This results in a maximum power flow via the variator path of 66 % for the Output Split, of 40 % for the Input Split and of 17 % for the Compound Split. To take safety aspects and specification regulations into account, a FMEA for the Compound Split was carried out. It could be shown, that with additional measures there won't be an additional risk in the drivetrain for a rotorcraft using a Compound Split. The findings of this research show the direction of further investigation on transmission variable gearboxes for rotorcraft. Knowing that Compound Split offers the highest potential different types can be developed and evaluated for usage.
机译:本文提出的研究是国际研究项目VARI-SPEED的一部分,该项目旨在发明一种适用于不同旋翼飞机配置的变速传动系统,以降低所需的推进力,从而实现现代且生态高效的航空。该研究专注于旋翼飞机的动力传动系统技术,以实现可变的旋翼速度。在第一部分中,列出了已知的可变变速器传动系统技术。定义了旋翼飞机变速器使用的评估参数,并通过效用分析对其进行了评估。根据其满足评估参数要求的能力对列出的传动系统技术进行了评估。可以证明,无级变速器动力分配齿轮箱具有在旋翼航空器中使用的最大潜力。机械离散变速传动齿轮箱也可能会在旋翼航空器中使用,但换档过程可能会成为一个问题。在下一步中,根据它们在不同传动比下的动力分配性能,分析了三种动力分配齿轮箱配置-输入分配,输出分配和复合分配。通过机械路径传递的功率越多,效率越高,附加质量越低。在调查中,假设传播为两个。这导致通过变速箱路径的最大功率流量对于输出分配器为66%,对于输入分配器为40%,对于化合物分配器为17%。为了考虑安全方面和规范规定,对复合料分离装置进行了FMEA。可以证明,采用附加措施后,使用复合裂隙的旋翼飞机的动力总成不会有额外的风险。这项研究的结果表明了进一步研究旋翼航空器变速箱变速箱的方向。知道Compound Split具有最高的潜力,可以开发和评估不同类型的用途。

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