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1. 发明授权

US11987357B2 Gaseous matter capture system and method 有权
公开(公告)号：US11987357B2
公开(公告)日：2024-05-21
申请号：US17811629
申请日：2022-07-11
申请人： HIGH HOPES LABS LTD.
发明人： Eran Oren
IPC分类号： B64C39/02 , B01D53/04 , B01D53/22 , B01D53/62 , B01D53/84 , B01D53/86 , B64B1/50 , B64F3/00 , B64U10/30 , B64U101/00 , G01W1/08
CPC分类号： B64C39/024 , B01D53/04 , B01D53/22 , B01D53/62 , B01D53/84 , B01D53/86 , B64B1/50 , B64C39/022 , B64F3/00 , G01W1/08 , B01D2253/108 , B01D2253/204 , B01D2257/504 , B01D2258/06 , B64U10/30 , B64U2101/00
摘要： A gaseous matter capture system and method comprising an aerial unit configured to capture gaseous matter directly from the atmosphere and further comprising storage means configured to transfer said gaseous matter for further processing in a non-aerial unit for the purposes of climate change mitigation and further use of captured gases.

2. 发明授权

US09853360B2 Inflatable radar signal device 有权
公开(公告)号：US09853360B2
公开(公告)日：2017-12-26
申请号：US14744829
申请日：2015-06-19
申请人： LOCKHEED MARTIN CORPORATION
发明人： Russell M. Sylvia , Robert P. Gordon, Jr. , Martin C. Lewis , Mark E. Whalen
IPC分类号： G08B5/00 , B63C9/18 , H01Q15/14 , G01S19/14 , B63C11/26 , B63B22/22 , B63C9/15 , B64B1/50
CPC分类号： H01Q15/14 , B63B22/22 , B63C9/155 , B63C11/26 , B64B1/50 , G01S19/14 , G08B5/002
摘要： An inflatable RADAR signal device that is capable of rising above the surface of the water when deployed and that reflects RADAR emissions. The signal device is a self-contained, small, independent system that can withstand being present in a maritime environment, including being submerged in the water and/or being located on a vessel in the water, for an extended amount of time. The device includes a housing that houses one or more deflated balloons that are constructed of a material that, when inflated, rise above the level of the water and that reflect RADAR emissions. The device includes at least one gas cylinder for inflating the balloon(s), and a mechanism to trigger release of the balloon(s) from the housing including a mechanism to trigger release of the gas from the gas cylinder(s) to inflate the balloon(s).

3. 发明申请

US20170361914A1 HIGH ALTITUDE GRAVITY ENERGY STORAGE 审中-公开
公开(公告)号：US20170361914A1
公开(公告)日：2017-12-21
申请号：US15611782
申请日：2017-06-01
申请人： Edmund Joseph Kelly , Roger Arnold
发明人： Edmund Joseph Kelly , Roger Arnold
IPC分类号： B64B1/50 , H02S10/20 , H02S30/20 , H02S10/00 , B64B1/08
CPC分类号： B64B1/50 , B64B1/08 , H02S10/00 , H02S10/20 , H02S30/20 , Y02E10/50
摘要： The present invention is realized by apparatus and methods for harvesting, storing, and generating energy by permanently placing a large rigid buoyant platform high in the earth's atmosphere, above clouds, moisture, dust, and wind. Long, strong and light tethers can connect the buoyant structure to the ground which can hold it in position against wind forces. Weights suspended from the buoyant platform with cables are raised and lowered by electric winches to store and release gravitational potential energy. High voltage transmission lines electrically connect the platform to the earth's surface. Electrical energy from the high voltage transmission lines or from photovoltaic arrays on the platform can be stored as gravitational potential energy and subsequently released as electricity from generators driven from the stored gravitational potential energy and used on the platform or transmitted via the high voltage transmission lines.

4. 发明授权

US09449475B2 Emergency location device 有权
标题翻译：紧急定位装置
公开(公告)号：US09449475B2
公开(公告)日：2016-09-20
申请号：US14286249
申请日：2014-05-23
申请人： Peter Aguilar
发明人： Peter Aguilar
IPC分类号： G08B5/00 , B64B1/50
CPC分类号： G08B5/002 , B64B1/50
摘要： An emergency location device with a deployable rescue balloon is presented. The balloon is housed in tube body in its stowed state with a frangible foil holding it in place at the proximal edge of the tube body. The device includes a ball valve attached to the opposite end of the balloon and further coupled to a charger valve. The charger valve includes a piercing needle configured to pierce a helium pressure tank thereby deploying and inflating the rescue balloon. The helium tank, the charger valve, and the ball valve are all enclosed in the lumen of the tube body. The balloon is attached to the inside of the tube body via a lanyard, which unravels when the balloon is deployed. A threaded cap coupled to the distal end of the tube body, which is also used to deploy the balloon, secures the helium pressure tank in the tube body.
摘要翻译：提出了具有可部署的救援气球的紧急定位装置。气囊以其收起状态容纳在管体中，其中易碎的箔将其保持在管体近端的适当位置。该装置包括附接到球囊的相对端的球阀，并进一步联接到充气阀。充电阀包括穿刺针，其被构造成刺穿氦压力罐，从而展开和充气救援气球。氦罐，充电阀和球阀均封闭在管体的内腔中。气球通过挂绳连接到管体内部，当气囊展开时，该挂绳松开。联接到管主体的远端的螺纹盖，其也用于展开气囊，将氦压力罐固定在管体中。

5. 发明申请

US20160214716A1 BREAKING APART A PLATFORM UPON PENDING COLLISION 审中-公开
标题翻译：打破一个平台在垂死的碰撞
公开(公告)号：US20160214716A1
公开(公告)日：2016-07-28
申请号：US14757425
申请日：2015-12-23
申请人： SPACE DATA CORPORATION
发明人： Gerald Mark KNOBLACH , Eric A. FRISCHE
IPC分类号： B64D1/02 , B64B1/50 , B64B1/70 , B64B1/42
CPC分类号： B64D1/02 , B64B1/40 , B64B1/42 , B64B1/50 , B64B1/70 , G08G5/045
摘要： A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.
摘要翻译：公开了一种用于分离和释放响应于高冲突概率的浮动平台的有效载荷的组成部分的方法和系统。该方法包括：确定飞行中飞行器是否在至少与浮动平台相关联的安全区域内，其中所述浮动平台包括可释放地耦合的组件; 以及响应于确定所述飞行中飞行器至少在所述安全区域内的确定而启动释放机构，其中所述释放机构被配置为使所述组件部件脱离连接。

6. 发明申请

US20150274277A1 LIGHTER-THAN-AIR CRAFT FOR ENERGY-PRODUCING TURBINES 审中-公开
标题翻译：用于能源生产涡轮的轻型空气压缩机
公开(公告)号：US20150274277A1
公开(公告)日：2015-10-01
申请号：US14679883
申请日：2015-04-06
申请人： Altaeros Energies, Inc.
发明人： Benjamin W. Glass
IPC分类号： B64B1/06 , B64B1/50
CPC分类号： B64B1/06 , B64B1/50 , F03D1/02 , F03D9/32 , F03D13/20 , F05B2240/133 , F05B2240/917 , F05B2240/922 , Y02E10/728
摘要： A wind-based power generating system provides a wind energy converter for converting wind energy into another form of energy using a lighter-than-air craft configured to produce a positive net lift. The net lift includes both a net aerodynamic lift and a net buoyant lift. A tethering mechanism is configured to restrain the lighter-than-air craft with respect to the ground. The lighter-than-air craft defines an interior volume for containing a lighter-than-air gas, and the lighter-than-air craft has a fore section and an aft section. The tethering system has at least one attachment point on the fore section of the lighter-than-air craft and at least one attachment point on the aft section of the lighter-than-air craft. The lighter-than-air craft provides a stable aerodynamic moment with respect to a yaw axis about a center-of-mass of the lighter-than-air craft. The craft can be formed in a variety of aerodynamic profiles/shapes.
摘要翻译：风力发电系统提供了一种风能转换器，用于将风能转换成另一种形式的能量，其中使用被构造成产生正净升降机的轻于空气的工艺。净升降机包括净空气动力升降机和净浮力升降机。束缚机构构造成相对于地面限制轻型飞行器。轻型空中飞行器具有用于容纳比空气中轻的气体的内部空间，而轻型飞行器具有前部和后部。系绳系统在轻型飞行器的前部上具有至少一个连接点，以及轻型飞行器的后部上的至少一个附接点。轻型飞行器相对于偏航轴提供了围绕轻型飞行器的中心质量的稳定的空气动力学力矩。该工艺可以形成各种空气动力学特性/形状。

7. 发明申请

US20150161857A1 EMERGENCY LOCATION DEVICE 审中-公开
标题翻译：紧急位置装置
公开(公告)号：US20150161857A1
公开(公告)日：2015-06-11
申请号：US14286249
申请日：2014-05-23
申请人： Peter AGUILAR
发明人： Peter AGUILAR
IPC分类号： G08B5/00
CPC分类号： G08B5/002 , B64B1/50
摘要： An emergency location device with a deployable rescue balloon is presented. The rescue balloon is housed in tube body in its stowed state with a frangible foil holding it in place at the proximal edge of the tube body. The location device includes a ball valve attached to the opposite end of the rescue balloon and further coupled to a charger valve. The charger valve includes a piercing needle configured to pierce a helium pressure tank thereby deploying and inflating the rescue balloon. The helium tank, the charger valve, the ball valve are all enclosed in the lumen of the tube body. The rescue balloon is attached to the inside of the tube body via a lanyard, which unravels when the balloon is deployed. A threaded cap coupled to the distal end of the tube body, which is also used to deploy the rescue balloon, secures the helium pressure tank in the tube body.
摘要翻译：提出了具有可部署的救援气球的紧急定位装置。救护气球以其收容状态容纳在管体中，其易碎的箔将其保持在管体的近端处的适当位置。定位装置包括附接到救援气球的相对端的球阀，并进一步联接到充气阀。充电阀包括穿刺针，其被构造成刺穿氦压力罐，从而展开和充气救援气球。氦罐，充电阀，球阀都封闭在管体的内腔中。救护气球通过挂绳连接在管体的内部，挂绳在气囊展开时解开。联接到管主体的远端的螺纹盖，其也用于展开救援气球，将氦压力罐固定在管体中。

8. 发明申请

US20140077030A1 Self Transportable Aerostat System 有权
标题翻译：自动运输气动系统
公开(公告)号：US20140077030A1
公开(公告)日：2014-03-20
申请号：US13735728
申请日：2013-01-07
申请人： TCOM, LP
发明人： Edward Cunningham , Han Dinh Phan
IPC分类号： B64B1/66 , B64B1/58
CPC分类号： B64F1/14 , B64B1/50 , B64B1/58 , B64B1/66 , B64D47/08 , B64F1/12
摘要： A self transportable aerostat system comprising: a first motorized mooring truck; a mooring tower removably attached to a base assembly of the first mooring truck, generally vertically arranged in relation to the bed of the first mooring truck; a proximal and distal boom deck removably attached to the base assembly; a flying sheave for redirecting a tether carried by the base assembly and attachable to an aerostat; a second motorized mooring truck attachable to the outer edge of the distal boom; and, an aerostat truck having an electrical connection for connecting to the first mooring truck and having an aerostat storage compartment for storing the aerostat is a retracted configuration.
摘要翻译：一种可自行运送的空气净化系统，包括：第一电动系泊车; 系泊塔可移除地附接到第一系泊车的基座组件，其大致垂直地布置成相对于第一系泊车的床; 可拆卸地附接到基座组件的近侧和远侧臂架甲板; 用于重新定向由基座组件承载的系绳并可附接到空气净化器的飞轮; 第二电动系泊车可附接到远端吊杆的外缘; 并且具有用于连接到第一系泊卡车的电气连接并且具有用于存储空气净化器的空气净化器储藏室的空气净化器卡车是缩回构型。

9. 发明申请

US20140054412A1 BALLOON-BORNE PLATFORM STABILIZATION 有权
标题翻译：气球平台稳定
公开(公告)号：US20140054412A1
公开(公告)日：2014-02-27
申请号：US14004169
申请日：2012-03-11
申请人： Avishay Guetta , Ragael Amber , Yuval Guetta
发明人： Avishay Guetta , Ragael Amber , Yuval Guetta
IPC分类号： B64B1/50
CPC分类号： B64B1/50 , B64B1/52
摘要： An aerial balloon system comprising a payload platform suspended from an inflated balloon by means of a balloon cable, and an anchoring cable attaching the platform to an anchor point beneath it. The balloon cable and anchoring cable are attached to the payload platform by means of a connecting element pivotally attached to the platform. The platform may include a servo controlled pitch stabilizing system using the input from a pitch sensor mounted on the platform to control an angular actuator to change the angle which the platform makes with the pivoted connection element. Additionally, the platform may include a servo controlled orientation stabilizing system using the input from an orientation sensor mounted thereon to control the departure of the orientation of the platform from a predetermined orientation. This may be readily accomplished using a variable pitch rotor, the pitch being controlled by the orientation sensor signal.
摘要翻译：一种空中气球系统，其包括通过气囊缆索从充气气囊悬挂的有效载荷平台，以及将平台附接到其下方的锚点的锚定缆索。气球电缆和锚固电缆通过可枢转地附接到平台的连接元件附接到有效负载平台。平台可以包括使用安装在平台上的俯仰传感器的输入的伺服控制桨距稳定系统来控制角度致动器以改变平台与枢转连接元件形成的角度。另外，平台可以包括伺服控制的定向稳定系统，其使用来自安装在其上的定向传感器的输入来控制平台的定向从预定取向的偏离。这可以使用可变桨距转子容易地实现，该间距由定向传感器信号控制。

10. 发明申请

US20130344417A9 HIGH ALTITUDE PLATFORM 有权
标题翻译：高海拔平台
公开(公告)号：US20130344417A9
公开(公告)日：2013-12-26
申请号：US13810615
申请日：2011-06-14
申请人： Peter Davidson , Hugh Edmund Murray Hunt , Christopher John Burgoyne
发明人： Peter Davidson , Hugh Edmund Murray Hunt , Christopher John Burgoyne
IPC分类号： H01M8/22 , H02K7/18
CPC分类号： H04B10/25752 , B64B1/50 , B64C39/022 , D07B1/14 , D07B5/005 , F02C6/00 , H01M8/04201 , H01M8/22 , H01M2250/20 , H02K7/1807 , H04B7/18504 , Y02T90/32
摘要： An apparatus for generating electrical energy at altitude, comprising a tether connecting a substantially ground level location, part to a platform at an elevated location, the tether comprising a conduit coupled to an electrical generator at the platform, the conduit arranged to allow the flow of a fuel fluid from the substantially ground level location to the elevated location, and the electrical generator being operable to convert energy in the fuel fluid to electrical energy at the elevated location.
摘要翻译：一种用于在海拔高度产生电能的装置，包括连接基本上地平面位置的部分，部分至高架位置处的平台，所述系绳包括连接到所述平台处的发电机的导管，所述导管被布置成允许燃料流体从基本上接地的位置到升高的位置，并且所述发电机可操作以将所述燃料流体中的能量转换到所述升高的位置处的电能。

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