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81. 发明授权

US09428257B2 Extended endurance air vehicle 有权
标题翻译：延长耐力飞行器
公开(公告)号：US09428257B2
公开(公告)日：2016-08-30
申请号：US14485685
申请日：2014-09-13
申请人： William Edmund Nelson
发明人： William Edmund Nelson
IPC分类号： B64B1/02 , B64B1/10 , B64B1/12 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/32 , B64B1/34 , B64B1/58
CPC分类号： B64B1/02 , B64B1/10 , B64B1/12 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/32 , B64B1/34 , B64B1/58 , B64B2201/00 , B64D27/24 , B64D2211/00 , G05D1/0011
摘要： An air vehicle comprises a vehicle body and a propulsion assembly. The vehicle body has the shape of a wing airfoil to generate lift when air flows over the vehicle body. The vehicle body has a body longitudinal axis and substantially planar port and starboard sides of composite material, and includes first and second hulls that are secured together side-by-side, the hulls having longitudinal axes that are substantially parallel to the body longitudinal axis and two substantially planar side walls at least one of which is of composite material. Each hull defines a separate fluid chamber that is filled with a fluid that is at least partially buoyant. The propulsion assembly is secured to the vehicle body port and starboard sides. The propulsion assembly includes port front and rear engines and starboard front and rear engines, wherein at least two of the engines have independently controlled thrust vectors.
摘要翻译：一种机动车辆包括车体和推进组件。车体具有翼型的形状，以在空气流过车体时产生升力。车身具有主体纵向轴线和复合材料的基本上平面的端口和右舷侧面，并且包括并排固定在一起的第一和第二船体，船体具有基本上平行于主体纵向轴线的纵向轴线，并且两个基本平坦的侧壁，其至少一个是复合材料。每个船体限定了一个单独的流体室，其中填充有至少部分浮力的流体。推进组件被固定到车体端口和右舷。推进组件包括前端和后部发动机和右舷前发动机，其中至少两个发动机具有独立控制的推力矢量。

82. 发明授权

US09102391B2 Hydrogen lighter-than-air craft structure 有权
标题翻译：氢气轻于空气工艺结构
公开(公告)号：US09102391B2
公开(公告)日：2015-08-11
申请号：US13855923
申请日：2013-04-03
申请人： Rinaldo Brutoco
发明人： Rinaldo Brutoco
IPC分类号： B64B1/08 , B64B1/18 , B64B1/12 , B64B1/20 , B64B1/32 , B64B1/62 , B64B1/66 , B64B1/58
CPC分类号： B64B1/08 , B64B1/12 , B64B1/18 , B64B1/20 , B64B1/32 , B64B1/58 , B64B1/62 , B64B1/66
摘要： A system for efficiently transporting hydrogen from where it can be economically made to where it is most needed including an airship having an exoskeleton made up of equal length spokes and equal sized hubs with six spokes terminating at each hub forming a set of hexagons. This set of connected hexagons forms the 3-dimensional shape of the ship by allowing various spokes to flex to different radii. A skin is attached external to the exoskeleton.
摘要翻译：一种用于将氢气从经济上有效地运送到最需要的地方的系统，包括具有由相同长度的辐条构成的外骨骼的飞艇和具有六个辐条的飞轮，所述六个辐条在每个轮毂处终止形成一组六边形。这组连接的六边形通过允许各种轮辐弯曲到不同的半径形成船的三维形状。皮肤附着在外骨骼的外部。

83. 发明授权

US06966523B2 Airship and method of operation 失效
标题翻译：飞艇及作战方法
公开(公告)号：US06966523B2
公开(公告)日：2005-11-22
申请号：US10718634
申请日：2003-11-24
申请人： Hokan S. Colting
发明人： Hokan S. Colting
IPC分类号： B64B1/02 , B64B1/32 , B64B1/34 , B64C21/02 , B64C39/02
CPC分类号： B64B1/34 , B64B1/02 , B64B1/32 , B64C21/02 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/044 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/146 , B64C2201/165 , Y02T50/166
摘要： An airship has a generally spherical shape and has an internal envelope for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7% full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.
摘要翻译：飞艇具有大致球形并且具有用于容纳诸如氦气或氢气的提升气体的内部信封。飞艇有一个推进和控制系统，允许飞行到所需的游荡地点，并在该地点保持一段时间。在一个实施例中，当内部信封充满提升气体的时间少至7％时，飞艇可以达到中性浮力，并且可以具有大约6万英尺的服务天花板。飞艇具有可以包括通信设备或监视的设备模块设备，或两者兼而有之。飞艇可以从地面站遥控。飞艇具有太阳能电池阵列，推进和控制系统的电动机由阵列获得的功率驱动。飞艇还具有可用于驱动电动机的辅助动力单元。飞艇可以有一个推动螺旋桨，有助于驾驶飞艇，还可以使球形飞艇进一步向后流动的距离。在一个实施例中，飞艇可以在高度加油以允许延长的游荡。

84. 发明申请

US20050173591A1 AIRSHIP AND METHOD OF OPERATION 失效
标题翻译：航空和操作方法
公开(公告)号：US20050173591A1
公开(公告)日：2005-08-11
申请号：US10718634
申请日：2003-11-24
申请人： Hokan Colting
发明人： Hokan Colting
IPC分类号： B64B1/02 , B64B1/32 , B64B1/34 , B64C21/02 , B64C39/02
CPC分类号： B64B1/34 , B64B1/02 , B64B1/32 , B64C21/02 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/044 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/146 , B64C2201/165 , Y02T50/166
摘要： An airship has a generally spherical shape and has an internal envelope for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7% full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.
摘要翻译：飞艇具有大致球形并且具有用于容纳诸如氦气或氢气的提升气体的内部信封。飞艇有一个推进和控制系统，允许飞行到所需的游荡地点，并在该地点保持一段时间。在一个实施例中，当内部信封充满提升气体的时间少至7％时，飞艇可以达到中性浮力，并且可以具有大约6万英尺的服务天花板。飞艇具有可以包括通信设备或监视的设备模块设备，或两者兼而有之。飞艇可以从地面站遥控。飞艇具有太阳能电池阵列，推进和控制系统的电动机由阵列获得的功率驱动。飞艇还具有可用于驱动电动机的辅助动力单元。飞艇可以有一个推动螺旋桨，有助于驾驶飞艇，还可以使球形飞艇进一步向后流动。在一个实施例中，飞艇可以在高度加油以允许延长的游荡。

85. 发明公开

US20230339629A1 HYBRID AIRSHIP FOR PACKAGE DELIVERY 审中-公开
公开(公告)号：US20230339629A1
公开(公告)日：2023-10-26
申请号：US18305321
申请日：2023-04-21
申请人： Nathan Ian Cobb
发明人： Nathan Ian Cobb
IPC分类号： B64U10/30 , B64B1/66 , B64B1/32
CPC分类号： B64U10/30 , B64B1/66 , B64B1/32 , B64U2101/60
摘要： An unmanned hybrid airship for delivering packages, featuring: a forward payload bay counterbalanced by a moveable counterweight; and a gripping mechanism for engaging unconventional mooring structures such as balcony rails and window sills. Other embodiments are described.

86. 发明申请

US20200283170A1 HYBRID AIRSHIP AND RELATED ASSEMBLY AND/OR MAINTENANCE METHOD 审中-公开
公开(公告)号：US20200283170A1
公开(公告)日：2020-09-10
申请号：US16763624
申请日：2017-11-13
申请人： TOTAL SA , FLYING WHALES
发明人： Hervé KUHLMANN
IPC分类号： B64F5/40 , B64B1/22 , B64B1/32 , B64B1/24 , B64D9/00 , B64D37/04
摘要： The present invention concerns hybrid airship comprising at least one buoyancy enclosure containing a gas lighter than air, a gondola attached below the buoyancy enclosure, the gondola extending along a longitudinal axis, at least one propeller configured to propel the hybrid airship, the at least one propeller being attached to the buoyancy enclosure, at least one generator, configured to provide power to the propeller, the generator being connected to the gondola. The hybrid airship comprises an arm protruding from the gondola and connecting the generator to the gondola.

87. 发明授权

US10308340B2 System, method and apparatus for widespread commercialization of hydrogen as a carbon-free fuel source 有权
公开(公告)号：US10308340B2
公开(公告)日：2019-06-04
申请号：US15351759
申请日：2016-11-15
申请人： Rinaldo Brutoco
发明人： Rinaldo Brutoco
IPC分类号： B64B1/62 , H02S20/00 , C25B1/04 , B64B1/12 , H01M10/46 , H02J7/35 , H02S20/30 , B64B1/06 , B64B1/20 , B64B1/28 , B64B1/32 , B64B1/64 , B64B1/66 , B64D27/24 , B64D41/00
摘要： A system for transporting hydrogen from where it can be economically made to where it is most needed using airships. Green technologies can be used to generate electricity near to the primary energy sources. This electricity can then be used to produce hydrogen directly from water. Hydrogen can be delivered using an airship in which the hydrogen gas can also be used for generating lift, providing propulsion energy and serving ancillary needs. The ship can be equipped with solar cells that generate electricity that can be used to make hydrogen from water, and can be used to power the ship's propulsion system.

88. 发明申请

US20190152576A1 AIRCRAFT 审中-公开
公开(公告)号：US20190152576A1
公开(公告)日：2019-05-23
申请号：US16302771
申请日：2017-05-31
申请人： Hybrid-Airplane Technologies GmbH
发明人： Csaba SINGER
IPC分类号： B64B1/58 , B64B1/20 , B64B1/08 , B64B1/18 , B64B1/32
摘要： The invention relates to an aircraft having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) comprises a plurality of rod or tube-shaped sections (24-30) which define a circular, oval or polygonal main clamping plane for the shell (10).

89. 发明授权

US09802690B2 Cargo airship 有权
公开(公告)号：US09802690B2
公开(公告)日：2017-10-31
申请号：US14531481
申请日：2014-11-03
申请人： LTA Corporation
发明人： John Goelet , Loginn Kapitan , Ron Hochstetler
IPC分类号： B64B1/08 , B64B1/22 , B64D1/22 , B64D9/00 , B64B1/10 , B64B1/20 , B64B1/32 , B64B1/34 , B64B1/58 , B64B1/70 , B64D1/02
CPC分类号： B64B1/08 , B64B1/10 , B64B1/20 , B64B1/22 , B64B1/32 , B64B1/34 , B64B1/58 , B64B1/70 , B64D1/02 , B64D1/22 , B64D9/003 , Y02T50/46
摘要： A cargo airship is disclosed. The cargo airship may include a hull configured to contain a gas and at least one propulsion assembly coupled to the airship and including a propulsion device. The cargo airship may further include a payload bay comprising an external cargo area located outside of the hull. The cargo airship may also include a cargo handling system including at least one hoisting mechanism configured to lift cargo into the external cargo area while the airship is hovering.

90. 发明授权

US4061293A Balloon with manually operable helicopter blades 失效
标题翻译：气球与手动可操作的直升机叶片
公开(公告)号：US4061293A
公开(公告)日：1977-12-06
申请号：US775709
申请日：1977-03-09
申请人： Kenneth K. Lo
发明人： Kenneth K. Lo
IPC分类号： B64B1/32 , B64C31/04
CPC分类号： B64B1/32 , B64C31/04
摘要： A balloon filled with buoyant gas provides the major part of the required lift. A pair of spaced rings are supported by a rigging having a plurality of lines supported by the upper half of the balloon at approximately the vertical center of the balloon. Each of a pair of helicopter blade units is rotatably mounted on a corresponding one of the rings. A frame is supported by the rigging beneath the balloon and has a passenger's bicycle type seat mounted thereon, a pedal-operated sprocket wheel rotatably mounted thereon and a plurality of landing wheels rotatably mounted thereon. The sprocket wheel is coupled to the helicopter blade units in a manner whereby a passenger seated in the seat and pedalling the sprocket wheel in any position between central and forward positions contrarotates the torque-balancing blade units for providing additional lift and forward propulsion force. A rudder is movably mounted on the frame and is controlled in direction by the passenger for directing the aircraft in flight.
摘要翻译：填充浮力气体的气球提供所需电梯的主要部分。一对隔开的环由在气球的大致垂直中心处具有由球囊的上半部支撑的多条线的索具支撑。一对直升机刀片单元中的每一个可旋转地安装在相应的一个环上。框架由气球下方的索具支撑，并且具有安装在其上的乘客自行车型座椅，可旋转地安装在其上的踏板操作链轮和可旋转地安装在其上的多个着陆轮。链轮以这样的方式联接到直升机叶片单元，使得坐在座椅中并且在链轮之间的中间和向前位置之间的任何位置的乘客反转转矩平衡叶片单元以提供额外的提升和向前推进力。方向舵可移动地安装在框架上，并由乘客在方向上控制，以将飞机引导飞行。

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