Abstract. Traditional tilt rotor ai

Abstract. Traditional tilt rotor aircraft rely on turning the whole engine nacelle, to accomplish thetransformation between vertical take-off and landing as well as flying. This scheme has a large rotationalinertia and requires a heavy and complex tilting mechanism. the engine jet flow in the process of verticaltake-off and landing directly spray down, and this flow could blow up the sand and stone, let engine suck itin or hurt people. So this paper designed a new rotated way based on variable shaft Angle gear transmission.The carrier aircraft design scheme referenced the data come from following software and website. The dataof airfoils come from the software profili and the website Airfoil Investigation Database. The pressuredistribution as well as air flow simulation and calculation is based on XFLR5. The mechanical, appearanceand overall design is based on CATIA. The gear contour design is based on CAXA CAD and the fullaircraft aerodynamic simulation is based on ANSYS/FLUENT. The engine with this design is fixed, so itonly needs rotate the tilting rotor shaft, and the mechanical structure is relatively simple, which make thisaircraft can play an important role in the future logistics and transportation system.

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结果 (英语) 1: [复制]

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Abstract. Traditional tilt rotor aircraft rely on turning the whole engine nacelle, to accomplish the transformation between vertical take-off and landing as well as flying. This scheme has a large rotational inertia and requires a heavy and complex tilting mechanism. the engine jet flow in the process of vertical take-off and landing directly spray down, and this flow could blow up the sand and stone, let engine suck it in or hurt people. So this paper designed a new rotated way based on variable shaft Angle gear transmission. The carrier aircraft design scheme referenced the data come from following software and website. The data of airfoils come from the software profili and the website Airfoil Investigation Database. The pressure distribution as well as air flow simulation and calculation is based on XFLR5. The mechanical, appearance and overall design is based on CATIA. The gear contour design is based on CAXA CAD and the fullaircraft aerodynamic simulation is based on ANSYS/FLUENT. The engine with this design is fixed, so it only needs rotate the tilting rotor shaft, and the mechanical structure is relatively simple, which make this aircraft can play an important role in the future logistics and transportation system.

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结果 (英语) 2:[复制]

复制成功！

正在翻译中..

结果 (英语) 3:[复制]

复制成功！

抽象的。传统的倾转旋翼飞机依靠转动整个机舱来完成 垂直起降与飞行的转换。这个方案有一个大的旋转 惯性，需要重型复杂的倾斜机构。垂直过程中的发动机射流 起降时直接喷射下来，这样的气流会把沙石吹起来，让发动机吸进去 伤害别人。为此，本文设计了一种基于变轴角齿轮传动的新型旋转方式。 舰载机设计方案参考了来自以下软件和网站的数据。数据 翼型的数据来自profili软件和网站翼型调查数据库。压力 基于XFLR5的气流组织及气流模拟计算。机械、外观 总体设计基于CATIA。基于CAXA的齿轮廓线设计和基于ANSYS/FLUENT的全机气动仿真。这种设计的发动机是固定的，所以 只需旋转可倾转子轴，机械结构相对简单 飞机可以在未来的物流和运输系统中发挥重要作用。

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