CN102530232A - 一种可控氢气飞行器 - Google Patents

一种可控氢气飞行器 Download PDF

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Publication number
CN102530232A
CN102530232A CN2011103740127A CN201110374012A CN102530232A CN 102530232 A CN102530232 A CN 102530232A CN 2011103740127 A CN2011103740127 A CN 2011103740127A CN 201110374012 A CN201110374012 A CN 201110374012A CN 102530232 A CN102530232 A CN 102530232A
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hydrogen
storehouse
balloon
flight vehicle
helium
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CN2011103740127A
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白雪海
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Priority to CN2011103740127A priority Critical patent/CN102530232A/zh
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Abstract

本发明的氢气飞行器为双层球囊的气球或飞艇，内层装氢气，外层装氦气(1)，内层氢气球囊又分扩冲仓(2)和压缩仓(3)。

Description

一种可控氢气飞行器
一，技术背景
氢气飞行器是一种环保节能的理想飞行器，但是由于氢气易燃易爆的特性，至今没有进入实用阶段，放出去的氢气球也不能收回来。本发明解决了上述问题。 
二，技术摘要 
本发明的氢气飞行器为双层球囊的气球或飞艇，内层装氢气，外层装氦气(1)，内层氢气球囊又分扩冲仓(2)和压缩仓(3)。 
三，技术说明 
本发明的氢气飞行器由氦气仓(1)，氢气扩充仓(2)，氢气压缩仓(3)，压气泵和气管(4)气压传感器(5)，卫星定位仪(6)，单片机或其他计算机控制系统(7)，缆绳和吊篮(8)，螺旋桨(9)等组成，氢气扩充仓和氢气压缩仓位于氦气仓内，由压气泵和气管连接，气压传感器分别安装在氦气仓和氢气扩充仓氢气压缩仓内，与单片机连接，螺旋桨安装在吊篮外侧。 
四，技术含义 
单片机通过气压传感器监测氦气仓和氢气扩充仓压缩仓，同时通过卫星定位知道空间位置。当氦气泄漏或氢气泄漏的时候发出警报。氢气进入压缩仓时，飞行器上行运动；氢气进入扩充仓时，飞行器下行运动；螺旋桨工作时，飞行器前行运动。 
五，权利要求 
一种可控氢气飞行器，由双层球囊构成，外层球囊装有氦气，内层球囊装有氢气，氢气囊分隔成两个仓，一个扩充仓，一个压缩仓 
六，技术意义 
本发明解决了氢气球易燃易爆的问题，同时可控飞行，适用于空间探测休闲娱乐等方面。
附图说明 
图一是氢气飞行器剖面图 

Claims (1)

1.一种可控氢气飞行器，由双层球囊构成，外层球囊装有氦气，内层球囊装有氢气，氢气囊分隔成两个仓，一个扩充仓，一个压缩仓。 
CN2011103740127A 2011-11-12 2011-11-12 一种可控氢气飞行器 Pending CN102530232A (zh)

Priority Applications (1)

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CN2011103740127A CN102530232A (zh) 2011-11-12 2011-11-12 一种可控氢气飞行器

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CN2011103740127A CN102530232A (zh) 2011-11-12 2011-11-12 一种可控氢气飞行器

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CN102530232A true CN102530232A (zh) 2012-07-04

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2578814C1 (ru) * 2015-03-02 2016-03-27 Юлия Алексеевна Щепочкина Воздухоплавательный аппарат
CN113060271A (zh) * 2021-03-03 2021-07-02 浙江热土航空发展有限公司 一种具有新型气囊布局的氢能源飞艇及使用方法
CN115709794A (zh) * 2022-11-25 2023-02-24 中国特种飞行器研究所 一种可回收氢飞艇及其使用方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1322657A (zh) * 2000-05-10 2001-11-21 何志刚 飞艇和气球卸载后的自增重方法
CN1359827A (zh) * 2000-12-22 2002-07-24 张涛 能安全使用氢气、并能控制其升降的硬壳气球、飞艇
US20090114768A1 (en) * 2007-04-24 2009-05-07 Michael Todd Voorhees Aerostatic Buoyancy Control System
CN101607590A (zh) * 2008-06-19 2009-12-23 许世永 改进型射频遥控气球

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1322657A (zh) * 2000-05-10 2001-11-21 何志刚 飞艇和气球卸载后的自增重方法
CN1359827A (zh) * 2000-12-22 2002-07-24 张涛 能安全使用氢气、并能控制其升降的硬壳气球、飞艇
US20090114768A1 (en) * 2007-04-24 2009-05-07 Michael Todd Voorhees Aerostatic Buoyancy Control System
CN101607590A (zh) * 2008-06-19 2009-12-23 许世永 改进型射频遥控气球

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2578814C1 (ru) * 2015-03-02 2016-03-27 Юлия Алексеевна Щепочкина Воздухоплавательный аппарат
CN113060271A (zh) * 2021-03-03 2021-07-02 浙江热土航空发展有限公司 一种具有新型气囊布局的氢能源飞艇及使用方法
CN115709794A (zh) * 2022-11-25 2023-02-24 中国特种飞行器研究所 一种可回收氢飞艇及其使用方法

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Application publication date: 20120704