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首页> 外文期刊>Journal of propulsion and power >Design of a Quiet Propeller for an Electric Mini Unmanned Air Vehicle
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Design of a Quiet Propeller for an Electric Mini Unmanned Air Vehicle

机译:电动微型无人机的静音螺旋桨设计

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摘要

Designing a quiet and efficient propeller is a demanding task because these two goals often lead to contradictory design trends. The task becomes even more complicated when additional constraints are introduced. This paper presents a multidisciplinary design optimization process for designing a quiet propeller under various constraints. The acoustic model of the propeller is presented in detail, including its validation. The new process is used to design a quiet propeller for an electric mini unmanned air vehicle. This design is subjected to power, structural, and side constraints. The design variables include blade geometry, blade cone angle, propeller radius, number of blades, and rotational speed. It is shown that the motor characteristics have an important influence on the optimization, and it is therefore important to take them into account during the design process. The influences of the various parameters on the design and propeller's characteristics are presented and discussed in detail.
机译:设计安静高效的螺旋桨是一项艰巨的任务,因为这两个目标通常会导致相互矛盾的设计趋势。当引入其他约束时,任务变得更加复杂。本文提出了一种多学科设计优化过程,用于在各种约束条件下设计安静的螺旋桨。详细介绍了螺旋桨的声学模型,包括其验证。新工艺用于为电动微型无人机设计安静的螺旋桨。该设计受到功率,结构和侧面约束。设计变量包括叶片几何形状,叶片锥角,螺旋桨半径,叶片数量和转速。结果表明,电机特性对优化有重要影响,因此在设计过程中将其考虑在内非常重要。详细介绍和讨论了各种参数对设计和螺旋桨特性的影响。

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