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1. 发明公开

CN103118938A 太阳能动力飞艇的系统和方法失效
公开(公告)号：CN103118938A
公开(公告)日：2013-05-22
申请号：CN201180045162.1
申请日：2011-07-15
申请人： LTA有限公司
发明人： J.戈伊雷特
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
CPC分类号： B64B1/06 , B64B1/005 , B64B1/08 , B64B1/10 , B64B1/16 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/58 , B64D9/00
摘要：一种太阳能飞艇，具有配置用于容纳气体的船体和至少一个推进组件，所述至少一个推进组件具有推进装置和配置用于驱动推进装置的电动机。所述太阳能飞艇也可包括动力供应系统，该动力供应系统包括可操作地联接于电动机并且配置用于为电动机供应动力的太阳能板。所述动力供应系统也可包括可操作地联接于太阳能板并且配置用于接收和储存由太阳能板供应的电能的电池，所述电池进一步可操作地联接于电动机且配置用于为电动机供应动力。所述电池的每一个在飞艇的外部气囊中被定位在选为设置压舱物的位置，所述外部气囊由飞艇的船体限定。所述太阳能飞艇也可包括配置用于容纳乘客或货物的船货系统。

2. 发明公开

CN106976544A 一种飞艇吊舱结构无效
公开(公告)号：CN106976544A
公开(公告)日：2017-07-25
申请号：CN201710124655.3
申请日：2017-03-03
申请人：南京航空航天大学
发明人：单杭英 , 孙中涛 , 杨忠清
IPC分类号： B64B1/22 , B64B1/28 , B64B1/30
摘要：本发明涉及一种飞艇吊舱结构，包括横向承力框、地板组件、小翼、外立面和舱顶；所述横向承力框的上部与气囊外伸结构件相连，下部工字型截面的高度与地板组件齐平，横向承力框与地板组件组成吊舱的传力骨架；所述小翼设置在吊舱两侧，作为吊舱的外挂结构，发动机安装架、发动机整流罩、螺旋桨保护环和发动机系统均安装在小翼上；所述外立面设置在横向承力框和地板组件外围，用于对横向承力框和地板组件组成的传力骨架起支撑、固定作用；所述舱顶的顶部轮廓与气囊的弧面一致。本发明安全、舒适，增加横向承力框的宽度和高度，即可产生宽敞的内部空间；可用于经营航空项目的旅游观光、重大节日的航拍以及紧急情况下航空运输军、民用物资等。

3. 发明授权

CN103118938B 太阳能动力飞艇的系统和方法失效
公开(公告)号：CN103118938B
公开(公告)日：2016-05-25
申请号：CN201180045162.1
申请日：2011-07-15
申请人： LTA有限公司
发明人： J.戈伊雷特
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
CPC分类号： B64B1/06 , B64B1/005 , B64B1/08 , B64B1/10 , B64B1/16 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/58 , B64D9/00
摘要：一种太阳能飞艇，具有配置用于容纳气体的船体和至少一个推进组件，所述至少一个推进组件具有推进装置和配置用于驱动推进装置的电动机。所述太阳能飞艇也可包括动力供应系统，该动力供应系统包括可操作地联接于电动机并且配置用于为电动机供应动力的太阳能板。所述动力供应系统也可包括可操作地联接于太阳能板并且配置用于接收和储存由太阳能板供应的电能的电池，所述电池进一步可操作地联接于电动机且配置用于为电动机供应动力。所述电池的每一个在飞艇的外部气囊中被定位在选为设置压舱物的位置，所述外部气囊由飞艇的船体限定。所述太阳能飞艇也可包括配置用于容纳乘客或货物的船货系统。

4. 发明专利

CA2803682A1 SYSTEM AND METHOD FOR SOLAR-POWERED AIRSHIP 未知
公开(公告)号：CA2803682A1
公开(公告)日：2012-01-26
申请号：CA2803682
申请日：2011-07-15
申请人： LTA CORP
发明人： GOELET JOHN
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
摘要： A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.

5. 发明专利

AU2011279902A1 System and method for solar-powered airship 未知
公开(公告)号：AU2011279902A1
公开(公告)日：2013-01-10
申请号：AU2011279902
申请日：2011-07-15
申请人： LTA CORP
发明人： GOELET JOHN
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
摘要： A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.

6. 发明专利

DE10011319C2 未知
公开(公告)号：DE10011319C2
公开(公告)日：2002-01-24
申请号：DE10011319
申请日：2000-03-10
申请人： CARGOLIFTER AG
发明人： SMITH TIM
IPC分类号： B64B1/20 , B64B1/28 , B64B1/34 , B64B1/00 , B64B1/36 , B64B1/38

7. 发明专利

JP2006001435A Multipurpose airship 审中-公开
标题翻译：多用途航空
公开(公告)号：JP2006001435A
公开(公告)日：2006-01-05
申请号：JP2004180560
申请日：2004-06-18
申请人： Mutsuro Bunto , 睦郎豊東
发明人： BUNTO MUTSURO
IPC分类号： B64B1/00 , B64B1/02 , B64B1/22 , B64B1/28 , B64B1/34 , B64D1/16 , B64D1/18
CPC分类号： B64B1/22 , B64B1/02 , B64B1/28 , B64B1/34 , B64D1/18
摘要： PROBLEM TO BE SOLVED: To provide a multipurpose airship which can be multipurposely used and takes an inexpensive administrative and maintenance expense.
SOLUTION: A balloon 5 which is made of either material of soft, semi-soft or hard material, in appropriate shape such as sphere or spindle shape, and generates a levitation force by filling a gas lighter than air is detachably mounted to the top, and is equipped with a two steps variable angle rotor 4 capable of adjusting an angle so as to generate both the levitation force and propulsive force, a stabilizing wing 2 where a propulsion unit 3 composed of a propeller or a jet engine is variable from the horizontal to vertical for the propulsive direction and detachably mounted to the end part, and a cabin 1 for a crew. A working apparatus such as a spraying device 10 of agricultural chemical can be mounted to the cabin 1.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：提供可以多用途的多用途飞艇，并且需要廉价的行政和维护费用。解决方案：气球5由柔软，半软或硬质材料制成，适当形状如球体或心轴形，并通过填充比空气更轻的气体产生悬浮力可拆卸地安装到顶部，并且配备有能够调节角度以产生悬浮力和推进力的两级可变角转子4;稳定翼2，其中由推进器或喷气发动机组成的推进单元3是可变的从推动方向从水平方向垂直，并可拆卸地安装到端部，以及用于船员的舱室1。工作装置如农用化学品的喷洒装置10可安装在舱室1.版权所有（C）2006，JPO＆NCIPI

8. 发明专利

AU2011279902B2 System and method for solar-powered airship 未知
公开(公告)号：AU2011279902B2
公开(公告)日：2015-07-23
申请号：AU2011279902
申请日：2011-07-15
申请人： LTA CORP
发明人： GOELET JOHN
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
摘要： A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.

9. 发明专利

DE19744581A1 Engine powered spherical aerostat 未知
公开(公告)号：DE19744581A1
公开(公告)日：1999-04-15
申请号：DE19744581
申请日：1997-10-04
申请人： BOCK JUERGEN DIPL PHYS
IPC分类号： B64B1/06 , B64B1/22 , B64B1/28 , B64B1/60
摘要： The lower half of the sphere is constructed as a shell-form gondola, and two diametrically opposed power plants are installed on the shell construction on the outside of the hull. The power plants are stabilized by suitable struts connected to reinforced sections of the shell construction. Change in the airship direction can be brought about by controlled differential thrust of the power plants. An Independent claim is included for a gondola which has a cabin, promenade deck, cockpit and cargo hold arranged in tiers in an annular fashion.

10. 发明专利

EA201390137A1 СИСТЕМА И СПОСОБ ДЛЯ ДИРИЖАБЛЯ НА СОЛНЕЧНОЙ ЭНЕРГИИ 未知
公开(公告)号：EA201390137A1
公开(公告)日：2013-10-30
申请号：EA201390137
申请日：2011-07-15
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
摘要： Дирижабльнасолнечнойэнергиис корпусом, выполненнымс возможностьюсодержанияв себегаза, ипоменьшеймереоднимдвигательнымузломс двигательнымустройствоми электрическимидвигателями, выполненнымис возможностьюприведениядвигательногоустройства. Дирижабльможеттакжевключатьв себясистемуподачиэнергии, включающуюв себяпанелисолнечныхбатарей, функциональносоединенныес электрическимдвигателями выполненныес возможностьюподачиэнергиик электрическимдвигателям. Системаподачиэнергиитакжеможетвключатьв себяаккумуляторы, функциональносоединенныес панелямисолнечныхбатарейи выполненныес возможностьюполученияи храненияэлектрическойэнергии, подаваемойпанелямисолнечныхбатарей, причемаккумуляторыдополнительнофункциональносоединеныс электрическимидвигателямии выполненыс возможностьюподачиэнергиик электрическимдвигателем. Каждыйизаккумуляторовможетбытьрасположенв наружнойоболочкедирижабля, образованнойкорпусомдирижабляв положении, выбранномдляобеспечениябалласта. Дирижабльнасолнечнойэнергиитакжеможетвключатьв себягрузовуюсистему, выполненнуюс возможностьюсодержанияпассажировилифрахта.

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