公开(公告)号：US20060038073A1

公开(公告)日：2006-02-23

申请号：US11049576

申请日：2005-02-02

申请人： John Shearing

发明人： John Shearing

IPC分类号： B64B1/02

CPC分类号： B64B1/06 ,  B64B1/16 ,  B64B1/58

摘要： A tubular container having a fabric shell formed and supported by suspension cables that are stretched between tower arrays that also serve to enclose the ends of the tube. This structure may be used as a building, a pressure vessel, a vacuum vessel, or as a container. If configured as a vacuum vessel and made with the super strong lightweight materials, then it is possible to create a lighter than air structure that will float in the atmosphere when evacuated of air.

摘要翻译： 一种管状容器，其具有形成并由悬挂电缆支撑的织物外壳，所述悬挂电缆在塔阵列之间被拉伸，所述塔阵列也用于封闭管的端部。 该结构可以用作建筑物，压力容器，真空容器或容器。 如果配置为真空容器并用超强的轻质材料制成，则可以产生比空气结构更轻的空气结构，该空气结构在排空空气时将浮在大气中。

公开(公告)号：US20140270795A1

公开(公告)日：2014-09-18

申请号：US13831004

申请日：2013-03-14

申请人： Edmund Joseph Kelly

发明人： Edmund Joseph Kelly

IPC分类号： B64B1/50 ,  H01L31/042 ,  H04B10/112 ,  G01S13/95

CPC分类号： B64B1/16 ,  B64B1/08 ,  B64B1/50 ,  B64B1/58 ,  B64F1/12 ,  G01S7/02 ,  G01S13/953 ,  H02S10/40 ,  H02S20/00 ,  H02S20/30 ,  H02S30/20 ,  H04B7/18502 ,  H04B7/18506 ,  H04B10/1129 ,  Y02A90/18

摘要： The present invention is realized by apparatus and methods for placing a large rigid buoyant platform in the low stratosphere of earth's atmosphere at an altitude of about 20 km, above clouds, moisture, dust, and wind. The platform can serve several uses, either individually or in any combination. These uses include uninterrupted radio and light communications, radar and optical observation including very powerful radars and solar power electricity generation. Long, strong and light tethers connect the buoyant structure to the ground which hold it in position against wind forces. The electricity output from a photovoltaic array is used to power platform uses and can also be coupled to high voltage transmission lines which transmit power from the platform to the earth's surface during daylight hours. Power can also be transmitted up to the platform during darkness to power facilities mounted on the platform ensuring continuous operation.

摘要翻译： 本发明通过将大型刚性浮力平台放置在大约20公里，云层，水分，灰尘和风的高度的地球大气层的低平流层中的装置和方法来实现。 该平台可以单独或以任何组合提供多种用途。 这些用途包括不间断的无线电和光通信，雷达和光学观测，包括非常强大的雷达和太阳能发电。 长而坚固的轻系绳将浮力结构连接到地面上，使其抵抗风力。 来自光伏阵列的电力输出用于为平台使用提供动力，并且还可耦合到在白天时间内将平台发射到地球表面的高压输电线路。 电力也可以在黑暗期间传输到平台上，以安装在平台上的设备，确保连续运行。

公开(公告)号：US08439294B2

公开(公告)日：2013-05-14

申请号：US12384802

申请日：2009-04-09

申请人： Sunstar Im

发明人： Sunstar Im

IPC分类号： B64B1/06

CPC分类号： B64B1/08 ,  B64B1/005 ,  B64B1/16 ,  B64B1/18 ,  B64B1/20 ,  B64B1/28 ,  B64B1/58 ,  B64B2201/00 ,  B64C2201/00 ,  B64G1/005

摘要： The structure provided multi-Levels of the center fuselage, two front wings, Extended mid-two wings and two rear wings with two vertical winglets.The fuselage has a cross section of half circle shaped fuselage.The first level comprises multi-fuel tanks, water tanks, Helium gas tanks, hydraulic, Pneumatic systems and plurality of the multi-landing gear bays and multi-cargo Compartments.The first level comprises a top cockpit and the plurality of the multi-passenger Cabins.The second level is comprises multi-central posts, multi-guy wires on the top center Beams, mid level, lower level center beams, leak proof sealed floor gates for the Multi-gas envelopes structure, under belly multi-pontoon air bags.The first level further comprises multi-jet power plants with multi-chute flaps.The second level may comprises, carbon fiber honey comb sandwich composite Multi-envelopes and multi-level soft gas envelopes.

摘要翻译： 该结构提供了中央机身的多层次，两个前翼，扩展中二翼和两个后翼与两个垂直的小翼。 机身有半圆形的机身横截面。 第一级包括多燃料箱，水箱，氦气罐，液压，气动系统和多个起落架舱和多货舱。 第一级包括顶部驾驶舱和多个多乘客舱。 第二层包括多中心柱，多中心柱，多中心杆，顶级中心梁，中级，下层中心梁，多气体信封结构的防漏密封地板门，腹部多浮桥气囊。 第一级还包括具有多溜槽襟翼的多喷射发电厂。 第二级可以包括碳纤维蜂蜜夹心复合多信封和多层软气体包络。

公开(公告)号：US09302758B2

公开(公告)日：2016-04-05

申请号：US13812495

申请日：2011-06-03

申请人： Hans Georg Kraus

发明人： Hans Georg Kraus

IPC分类号： B64C1/08 ,  B64B1/08 ,  B64B1/00 ,  B64B1/16 ,  B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/60 ,  B64B1/66 ,  B64F1/14 ,  B64F5/00

CPC分类号： B64B1/08 ,  B64B1/00 ,  B64B1/16 ,  B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/60 ,  B64B1/66 ,  B64F1/14 ,  B64F5/10 ,  Y02T50/82

摘要： A super-rigid hybrid airship having a modular structure with a central tube having a diameter of between 5 to 10% of the diameter of the airship, structural rings surrounding and preferably concentric with the central tube and connected to the tube by bolts; an external cover made from thin metal sheets, interspersed with composite resins and fibbers which is pressurized and pre-stressed by light gases and which is rigid, conductive, non-combustible and impermeable to gases; balloons filed with hydrogen and disposed in structural sections defined by neighboring structural rings; at least two interconnected cuffs inflated by atmospheric air serving as operational ballast and ensuring weight, pressure and volume balance of the airship. Preferably the airship has a blower system for dispersing air, arranged on the centerline of the top layer, wings arranged at each side of the fixed sections, and thrust means.

摘要翻译： 具有模块化结构的超刚性混合式飞艇，其中心管具有直径在飞艇直径的5至10％之间，结构环围绕并且优选地与中心管同心并且通过螺栓连接到管; 由薄金属片制成的外盖，散布有复合树脂和纤维，其被轻质气体加压和预应力，并且是刚性的，导电的，不可燃的和不可渗透的气体; 用氢气放置并设置在由相邻结构环限定的结构部分中的气球; 至少两个相互连接的袖口充气，作为操作压载物的大气，并确保飞艇的重量，压力和体积平衡。 优选地，飞艇具有用于分散空气的鼓风机系统，布置在顶层的中心线上，布置在固定部分的每一侧的翼和推力装置。

公开(公告)号：US08899514B2

公开(公告)日：2014-12-02

申请号：US14032806

申请日：2013-09-20

申请人： John Goelet

发明人： John Goelet

IPC分类号： B64B1/34 ,  B64B1/28 ,  B64B1/00 ,  B64B1/30 ,  B64B1/58 ,  B64B1/20 ,  B64B1/10 ,  B64B1/16 ,  B64B1/08 ,  B64B1/22

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： An airship is disclosed. The airship may include a plurality of frame members defining a support structure for a hull of the airship. The airship may further include a plurality of bladders disposed within the hull, and retaining a volume of a lighter-than-air gas. The airship may also include a plurality of valves operatively coupled to at least one of the bladders. The airship may additionally include a computer configured to operate the valves to vary aerostatic buoyancy of the airship to achieve a desired lift force.

摘要翻译： 飞艇被披露。 飞艇可以包括限定用于飞艇的船体的支撑结构的多个框架构件。 飞艇还可以包括设置在船体内的多个气囊，并且保持一定体积的轻于空气的气体。 飞艇还可以包括可操作地联接到至少一个气囊的多个阀。 飞艇还可以包括计算机，该计算机构造成操作阀以改变飞艇的空气静力浮力以实现期望的提升力。

公开(公告)号：US20140021293A1

公开(公告)日：2014-01-23

申请号：US14032806

申请日：2013-09-20

申请人： John GOELET

发明人： John GOELET

IPC分类号： B64B1/22

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： 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.

摘要翻译： 具有构造成容纳气体的船体的太阳能飞艇和具有推进装置的至少一个推进组件和构造成驱动推进装置的电动马达。 飞艇还可以包括电源系统，其包括可操作地耦合到电动机并被配置为向电动机供电的太阳能电池板。 电源系统还可以包括可操作地耦合到太阳能电池板并被配置为接收和存储由太阳能电池板供应的电能的电池，电池进一步可操作地耦合到电动机并且被配置为向电动机供电。 电池可以各自位于由飞艇的船体在选定为提供镇流器的位置中限定的飞艇的外部封套内。 太阳能飞艇还可以包括配置成容纳乘客或货物的货物系统。

公开(公告)号：US20130277496A1

公开(公告)日：2013-10-24

申请号：US13812495

申请日：2011-06-03

申请人： Hans Georg Kraus

发明人： Hans Georg Kraus

IPC分类号： B64B1/08 ,  B64F5/00

CPC分类号： B64B1/08 ,  B64B1/00 ,  B64B1/16 ,  B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/60 ,  B64B1/66 ,  B64F1/14 ,  B64F5/10 ,  Y02T50/82

摘要： A super-rigid hybrid airship having a modular structure with a central tube having a diameter of between 5 to 10% of the diameter of the airship, structural rings surrounding and preferably concentric with the central tube and connected to the tube by bolts; an external cover made from thin metal sheets, interspersed with composite resins and fibbers which is pressurized and pre-stressed by light gases and which is rigid, conductive, non-combustible and impermeable to gases; balloons filed with hydrogen and disposed in structural sections defined by neighboring structural rings; at least two interconnected cuffs inflated by atmospheric air serving as operational ballast and ensuring weight, pressure and volume balance of the airship. Preferably the airship has a blower system for dispersing air, arranged on the centerline of the top layer, wings arranged at each side of the fixed sections, and thrust means.

摘要翻译： 具有模块化结构的超刚性混合式飞艇，其中心管具有直径在飞艇直径的5至10％之间，结构环围绕并且优选地与中心管同心并且通过螺栓连接到管; 由薄金属片制成的外盖，散布有复合树脂和纤维，其被轻质气体加压和预应力，并且是刚性的，导电的，不可燃的和不可渗透的气体; 用氢气放置并设置在由相邻结构环限定的结构部分中的气球; 至少两个相互连接的袖口，由大气作为操作压载气体充气，并确保飞艇的重量，压力和体积平衡。 优选地，飞艇具有用于分散空气的鼓风机系统，布置在顶层的中心线上，布置在固定部分的每一侧的翼和推力装置。

公开(公告)号：US20140158817A1

公开(公告)日：2014-06-12

申请号：US13665379

申请日：2012-10-31

申请人： TP AEROSPACE, INC.

发明人： Paul Chambers

IPC分类号： B64B1/08 ,  B64B1/06 ,  B64B1/16

CPC分类号： B64B1/08 ,  B64B1/16 ,  B64B1/22 ,  B64B1/32 ,  B64B2201/00

摘要： A rigid airship comprising a hull comprising a rigid frame covered by a skin, the rigid frame comprising a plurality of high pressure inflated tubes.

摘要翻译： 一种刚性飞艇，包括一个包括被皮肤覆盖的刚性框架的船体，刚性框架包括多个高压膨胀管。

公开(公告)号：US20120018571A1

公开(公告)日：2012-01-26

申请号：US13182864

申请日：2011-07-14

申请人： John Goelet

发明人： John Goelet

IPC分类号： B64B1/00 ,  B64B1/06

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： 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.

摘要翻译： 具有构造成容纳气体的船体的太阳能飞艇和具有推进装置的至少一个推进组件和构造成驱动推进装置的电动马达。 飞艇还可以包括电源系统，其包括可操作地耦合到电动机并被配置为向电动机供电的太阳能电池板。 电源系统还可以包括可操作地耦合到太阳能电池板并且被配置为接收和存储由太阳能电池板供应的电能的电池，电池进一步可操作地耦合到电动机并且被配置为向电动机供电。 电池可以各自位于由飞艇的船体在选定为提供镇流器的位置中限定的飞艇的外部封套内。 太阳能飞艇还可以包括配置成容纳乘客或货物的货物系统。

公开(公告)号：US20100276546A1

公开(公告)日：2010-11-04

申请号：US12384802

申请日：2009-04-09

申请人： Sunstar Im

发明人： Sunstar Im

IPC分类号： B64B1/20 ,  B64G1/26 ,  B64B1/06

CPC分类号： B64B1/08 ,  B64B1/005 ,  B64B1/16 ,  B64B1/18 ,  B64B1/20 ,  B64B1/28 ,  B64B1/58 ,  B64B2201/00 ,  B64C2201/00 ,  B64G1/005

摘要： The structure provided multi-Levels of the center fuselage, two front wings, Extended mid-two wings and two rear wings with two vertical winglets.The fuselage has a cross section of half circle shaped fuselage.The first level comprises multi-fuel tanks, water tanks, Helium gas tanks, hydraulic, Pneumatic systems and plurality of the multi-landing gear bays and multi-cargo Compartments.The first level comprises a top cockpit and the plurality of the multi-passenger Cabins.The second level is comprises multi-central posts, multi-guy wires on the top center Beams, mid level, lower level center beams, leak proof sealed floor gates for the Multi-gas envelopes structure, under belly multi-pontoon air bags.The first level further comprises multi-jet power plants with multi-chute flaps.The second level may comprises, carbon fiber honey comb sandwich composite Multi-envelopes and multi-level soft gas envelopes.

摘要翻译： 该结构提供了中央机身的多层次，两个前翼，扩展中二翼和两个后翼与两个垂直的小翼。 机身有半圆形的机身横截面。 第一级包括多燃料箱，水箱，氦气罐，液压，气动系统和多个起落架舱和多货舱。 第一级包括顶部驾驶舱和多个多乘客舱。 第二级包括多中心柱，多中心柱，多中心杆，顶级中心梁，中级，下级中心梁，多气体信封结构的防漏密封地板门，腹部多浮桥气囊。 第一级还包括具有多溜槽襟翼的多喷射发电厂。 第二级可以包括碳纤维蜂蜜夹心复合多信封和多层软气体包络。