一种新型旋转式扑翼飞行器的原理结构分析 |
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引用本文: | 高永宁,高晓燕.一种新型旋转式扑翼飞行器的原理结构分析[J].直升机技术,2007(4):31-39. |
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作者姓名: | 高永宁 高晓燕 |
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作者单位: | 福建省泉州市林业局,福建省泉州市林业局 泉州,362000,泉州,362000 |
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摘 要: | 本文介绍了一种仿效鸟类飞行方式的新型旋转式扑翼飞行器的原理结构分析。该飞行器兼备固定翼飞机和直升机的功能,具有垂直升降和空中悬停的能力;同时具有扑翼前飞后飞,左飞右飞的能力。其扑翼采用旋转式扑翼,与传统平面式扑翼相比较,效率较高,升力较平稳。研制扑翼飞行器关键要解决二个问题:第一是如何让扑翼飞行器垂直离地升空;第二是如何操纵。对此二个问题,提出一套新的解决方案。
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关 键 词: | 旋转式扑翼飞行器 结构分析 操纵系统 动力传动装置 |
A New Rotary Wing Aircraft Flutter of Structural Analysis |
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Authors: | GAO Yong-ning GAO Xiao-yan |
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Abstract: | Follow the example of a new way of birds flying rotary wing aircraft around the principle structure.The new rotary-wing aircraft flutter fixed-wing aircraft and helicopters are the functions of a vertical take-off and landing and hover in the air;at the same time,able to fly forward;Behind the fly;Left fly;The right to fly.Its use Flapping-Wing rotary wing flutter,flutter with the traditional wing of the plane,more efficient,more stable lift.Flapping-Wing Aircraft Development key to solve two problems:the first is how to make Flapping-wing aircraft took off vertically;The second is how to manipulate.We have two problems,put a new set of solutions. |
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Keywords: | rotary wing aircraft structural analysis handing system propulsion control |
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