首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences >THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER’S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON
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THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER’S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON

机译:特殊强调地面共振现象的新型直升机建造方案的支持过程,模拟研究设计和结构

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During design work on the new constructionof a light unmanned helicopter an attempt wasmade to map the actual design of the helicopterand built the helicopter mode using the finiteelement method. Calculations made using thismethod were intended as a support forconstruction work. In addition, this model couldbe used as a simulator for the real resonancetests and the first attempts to disassemble therotor. Such an approach to the design andtesting of the real structure allowed us toexamine in detail the dangers that may occurwhen tested on a real object. The main reasonsfor using the model were to determine thenatural frequency of the structure, reproductionattempts resonance (excitation harmonic force)simulations of the rotor to detach from zero tonominal speed and landing simulations ofasymmetric structures on the ground.
机译:在新建筑的设计工作中 一架轻型无人直升机试图 绘制直升机的实际设计图 并使用有限元建立了直升机模式 元素方法。使用此进行的计算 该方法旨在支持 施工作业。此外,此模型可以 用作真实共振的模拟器 测试和首次尝试拆卸 转子。这种设计方法和 对真实结构的测试使我们能够 详细检查可能发生的危险 在真实物体上测试时。主要原因 使用该模型是为了确定 结构的固有频率,繁殖 尝试共振(激发谐波力) 转子从零分离到的模拟 标称速度和着陆模拟 地面上的不对称结构。

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