CN112498674A - 充气式全电力旋翼民用直升飞机 - Google Patents

充气式全电力旋翼民用直升飞机 Download PDF

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CN112498674A
CN112498674A CN202011435374.8A CN202011435374A CN112498674A CN 112498674 A CN112498674 A CN 112498674A CN 202011435374 A CN202011435374 A CN 202011435374A CN 112498674 A CN112498674 A CN 112498674A
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别道平
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Abstract

充气式全电力旋翼民用直升飞机，有旋翼固定和旋翼倾转两种机型，包括旋翼、机体、储气仓、机舱、设备仓、机架、旋翼支架、垂直尾翼、电动机、刀片电池、太阳能薄膜电池、逆变器、轮胎、停机坪，其特征是：利用热气球原理，所述储气仓充装氦气，氦气的作用力与反作用力既可增加飞机载重量助力飞机起飞，又可起降落伞作用降低飞机的下降速度，确保飞机起飞、降落的安全稳定性。本发明的有益效果是：填补了世界没有充气式旋翼民用直升飞机的空白，开辟了全球无污染的充气式旋翼民用直升飞机产业，分流了地面汽车数量，为社会提供了没有交通拥堵、快捷迅达的绿色交通工具。结构简单。

Description

充气式全电力旋翼民用直升飞机
所属领域：
本发明涉及充气式全电力旋翼民用直升飞机，有旋翼固定和旋翼倾转两种机型，属于充气式全电力旋翼民用直升飞机领域。
背景技术：
目前，国内只有旋翼无人飞机，且因旋翼金属疲劳的难题，一般载重只有几公斤最多不超过25公斤，应用领域只是农业植保或者短途快递，更多的甚至是干脆没有载重量的儿童玩具。国外虽然有旋翼倾转直升飞机，但纯粹是军品，且自带的燃油不仅严重限制了载重量，还污染空气，这是一方面。另一方面，交通拥堵、停车困难等大城市病已经严重影响到社会的正常运转和人们的日常生活，可以不夸张地说，呼吸新鲜的空气和出行不堵车，有停车位虚位以待，已经成了现代都市人梦寐以求的奢望。
本发明的目的，结束全球没有充气式民用旋翼直升飞机的历史，在消除直升飞机以燃油驱动污染空气的基础上，实现私人小汽车向空中发展，解决城市街道交通拥堵和停车难的世界性难题，为社会提供没有交通拥堵的舒适愉快的绿色交通工具。
为达到上述目的，本发明所采取的技术方案是，充气式全电力民用旋翼直升飞机，有旋翼固定和旋翼倾转两种机型，包括旋翼、机体、机架、旋翼支架、储气仓、机舱、设备仓、电动机、刀片电池、太阳能薄膜电池、逆变器、轮胎、垂直尾翼、停机坪，其特征是：所述旋翼固定机型所述机体为“圆柱形”，所述储气仓充装氦气，氦气的作用力与反作用力既增加飞机载重量助力飞机起飞，又起降落伞作用降低飞机的下降速度，确保飞机起飞、降落的安全稳定性。
本发明在上述技术方案的基础上，还可以做如下改进。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述旋翼固定机型没有所述垂直尾翼，飞行方向由所述旋翼旋转速度差控制。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述旋翼倾转机型在在空中所述旋翼可倾转，推动飞机巡航，飞行方向靠所述垂直尾翼控制，降落时所述旋翼回归原位并降低旋转速度，实现飞机平稳降落。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述机体分上中下三层，最上层为所述储气仓，中层为所述客舱、下层为所述设备仓。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述机架上安装所述旋翼支架，所述旋翼支架安装所述电动机，所述电动机与所述旋翼连接驱动所述旋翼运转。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述电动机由所述刀片电池驱动，所述刀片电池和所述逆变器均安装在所述设备仓。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述机体粘贴所述太阳能薄膜电池发电，通过所述逆变器不间断为所述刀片电池补充电能。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述轮胎对降落起缓冲作用和实施在所述停机坪内移动。
本发明所述充气式全电力民用旋翼直升飞机，进一步：所述停机坪为加长的高速公路服务区和随处可见城乡所述房屋屋顶。
本发明的有益效果是：填补了世界没有充气式旋翼直升飞机的空白，开辟了全球无污染的充气式旋翼民用直升飞机产业，分流了地面汽车数量，为社会提供了没有交通拥堵的快捷迅达的绿色交通工具。结构简单。
附图说明：
下面结合附图和实施例对本发明作进一步说明：
图1是本发明的主视结构示意图
图2是本发明的分视结构示意图
附图中，列示的各标号所代表的充气式全电力旋翼民用直升飞机各部件的名称如下：
1旋翼、2机体、3机架、4旋翼支架、5储气仓、6、机舱、7设备仓、8电动机、9刀片电池、10太阳能薄膜电池、11逆变器、12 轮胎、13停机坪、60垂直尾翼。
具体实施方式
以下结合附图对本发明的原理和特征进行描述，所举实例只用于解释本发明，并非用于限制本发明的范围。
实施例一、如图1所示，本发明充气式全电力民用旋翼直升飞机，有旋翼固定和旋翼倾转两种机型，包括旋翼1、机体2、机架3、旋翼支架4、储气仓5、机舱6、设备仓7、电动机8、刀片电池9、太阳能薄膜电池10、逆变器11、轮胎12、停机坪13、垂直尾翼60，其特征是：利用热气球原理，所述旋翼1固定机型所述机体2为“圆柱形”，所述储气仓5充装氦气，氦气的作用力与反作用力既增加飞机载重量助力飞机起飞，又起降落伞作用，降低飞机的下降速度，确保飞机起飞、降落的安全稳定性；所述机体2分上中下三层，最上层为5储气仓，中层为所述客舱6、下层为所述设备仓7；所述机架3 上安装旋翼支架4，旋翼支架4安装所述电动机8，所述电动机8与所述旋翼1连接，驱动所述旋翼1运转；所述电动机8由所述刀片电池9驱动，所述刀片电池9和所述逆变器11安装在所述设备仓7；所述机体2粘贴所述太阳能薄膜电池10发电，通过所述逆变器11不间断为所述刀片电池9补充电能；所述轮胎12对飞机降落起缓冲作用并实现飞机在所述停机坪13内移动；所述停机坪13为加长的高速公路服务区和城乡随处可见的所述房屋屋顶。
实施例2、与实施例1相同，如图1所示，不同的是，所述旋翼1 固定机型没有所述垂直尾翼60，飞行方向由所述旋翼1旋转速度差控制；所述旋翼1倾转机型在空中所述旋翼1可倾转，推动飞机巡航，飞行方向靠所述垂直尾翼60控制，降落时所述旋翼1回归原位并降低旋转速度，实现飞机平稳降落。
以上所述仅为本发明的最佳实施例，并不用以限制本发明，凡在本发明精神和原则之内，所作的任何修改、等同替换、改进等，均应包含在本发明的保护范围之内。

Claims (9)

1.充气式全电力旋翼民用直升飞机，有旋翼固定和旋翼倾转两种机型，包括旋翼、机体、机架、旋翼支架、储气仓、机舱、设备仓、电动机、刀片电池、太阳能薄膜电池、逆变器、轮胎、垂直尾翼、停机坪，其特征是：所述旋翼固定机型所述机体为“圆柱形”，所述储气仓充装氦气，氦气的作用力与反作用力既可增加飞机载重量和助力飞机起飞，又可起降落伞作用降低飞机的下降速度，确保飞机起飞、降落的安全稳定性。
2.根据权利要求1所述充气式全电力民用旋翼直升飞机，其特征是：所述旋翼固定机型所述机体没有所述垂直尾翼，飞行方向由所述旋翼旋转速度差控制。
3.根据权利要求2所述充气式全电力民用旋翼直升飞机，其特征是：所述旋翼倾转机型在在空中所述旋翼倾转，推动飞机巡航，飞行方向靠所述垂直尾翼控制，降落时所述旋翼回归原位并降低旋转速度，实现飞机平稳降落。
4.根据权利要求3所述充气式全电力民用旋翼直升飞机，其特征是：所述机体分上中下三层，最上层为所述储气仓，中层为所述客舱、下层为所述设备仓。
5.根据权利要求4所述充气式全电力民用旋翼直升飞机，其特征是：所述机架上安装所述旋翼支架，所述旋翼支架安装所述电动机，所述电动机与所述旋翼连接，驱动所述旋翼运转。
6.根据权利要求5所述充气式全电力民用旋翼直升飞机，其特征是：所述电动机由所述刀片电池驱动，所述刀片电池和所述逆变器安装在所述设备仓。
7.根据权利要求6所述充气式全电力民用旋翼直升飞机，其特征是：所述机体粘贴所述太阳能薄膜电池发电，通过所述逆变器不间断为所述刀片电池补充电能。
8.根据权利要求7所述充气式全电力民用旋翼直升飞机，其特征是：所述轮胎对飞机降落起缓冲作用和实施在所述停机坪内移动。
9.根据权利要求7所述充气式全电力民用旋翼直升飞机，其特征是：所述停机坪为加长的高速公路服务区和城乡随处可见的所述房屋屋顶。
CN202011435374.8A 2020-12-11 2020-12-11 充气式全电力旋翼民用直升飞机 Pending CN112498674A (zh)

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CN101157383A (zh) * 2007-11-02 2008-04-09 黄刚 一种新型飞艇
CN205931212U (zh) * 2016-06-04 2017-02-08 郑州中德美游乐设备有限公司 用氦气球克服一部分重力的多旋翼载人飞行器
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