-
1.发明申请
公开(公告)号：WO2021069762A1
公开(公告)日：2021-04-15
申请号：PCT/ES2019/070678
申请日：2019-10-08
Applicant: VEGA CAMA, Sergio Rafael
Inventor： VEGA CAMA, Sergio Rafael
Abstract: Sistema de generación de energía eléctrica a partir de una fuerza de empuje aerostático, que comprende un conducto vertical (2); un aerostato (3) desplazable dentro del conducto vertical (2) con un movimiento alternativo, provisto de una cámara (4) que alberga un compartimento de gas (5) que confina en su interior un gas de sustentación menos denso que el aire, y un compartimento de aire (6) para la carga de aire, de modo que el llenado de la carga procura un movimiento descendente del aerostato (3) por efecto de la fuerza de gravedad, y el vaciado de la carga procura un movimiento ascendente del aerostato (3) por efecto de una fuerza de empuje aerostático; un conducto de recirculación (9) del aire desplazado durante el movimiento del aerostato (3); y medios de conversión energética (7) configurados para convertir la energía potencial resultante del movimiento de elevación del aerostato (3) en energía eléctrica.
-
公开(公告)号：WO2017105657A1
公开(公告)日：2017-06-22
申请号：PCT/US2016/060146
申请日：2016-11-02
Applicant: SKYCOM CORPORATION
Inventor： MICHAELIS IV, Max, G. , BENNETT, John, H. H.
CPC classification number: H02S20/32 , B64B1/12 , B64B1/30 , B64B1/58 , B64B1/62 , B64C2201/022 , B64C2201/122 , B64C2201/208 , H02S10/40 , H02S30/20
Abstract: Techniques are disclosed relating lighter-than-air aircraft. Such aircraft may be used for various purposes, such as providing network connectivity to areas that would otherwise lack such connectivity. For example, in some embodiments, a lighter-than-air aircraft according to this disclosure may include various types of antennas (directional or non-directional) for communicating with ground-based electronics or with other lighter-than-air aircraft.
Abstract translation: 所公开的技术涉及轻于空气的飞机。 这种飞机可以用于各种目的，例如提供网络连接到本来缺乏这种连接的地区。 例如，在一些实施例中，根据本公开内容的比空中轻的飞机可以包括用于与地面电子设备或与其他轻于空气的飞行器通信的各种类型的天线（定向或非定向的）。 p>
-
3.发明申请
公开(公告)号：WO2013131155A1
公开(公告)日：2013-09-12
申请号：PCT/BR2012/000128
申请日：2012-03-22
Applicant: FREIRE, Lincoln Fernandez
Inventor： FREIRE, Lincoln Fernandez
IPC: B64B1/62
CPC classification number: B64B1/62
Abstract: Sistema de controle de temperatura do gás de sustentação de dirigível (hélio, hidrogénio) que ajusta a sustentação da aeronave, automaticamente ou sob comando do piloto. Além de compensar os efeitos negativos devido à perda de peso do combustível consumido, permite ajustar os ângulos de arfagem e rolamento da aeronave, melhorando sua aeronavegabilidade, aumentando sobremaneira sua autonomia de vôo, assegura menor consumo de combustível e reduz a emissão de CO 2 na atmosfera.
Abstract translation: 用于控制飞艇（氦气，氢气）的提升气体的温度的系统自动或在飞行员的控制下调节飞艇升降机。 除了补偿消耗的燃料重量损失所带来的负面影响外，该系统还可以调整飞艇的俯仰角和俯仰角，提高其可操纵性，显着提高飞行自主性，将燃油消耗和二氧化碳排放量降低到 大气层。
-
公开(公告)号：WO2004100289A3
公开(公告)日：2005-11-10
申请号：PCT/US2004013895
申请日：2004-05-05
Applicant: ION AMERICA CORP , MCELROY JAMES FREDERICK , SRIDHAR K R
Inventor： MCELROY JAMES FREDERICK , SRIDHAR K R
CPC classification number: H01M8/186 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/101 , B64C2201/127 , B64C2201/148 , B64C2201/165 , B64D27/24 , B64D2041/005 , B64D2211/00 , H01M8/04007 , H01M8/2475 , H01M2250/20 , Y02E60/528 , Y02T50/44 , Y02T50/62 , Y02T50/69 , Y02T90/32 , Y02T90/36 , Y10S429/901
Abstract: A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air.
-
公开(公告)号：WO2021262325A2
公开(公告)日：2021-12-30
申请号：PCT/US2021/030929
申请日：2021-05-05
Applicant: ASTRALOFT, LLC
Inventor： WATTERS, David , WYE, Lauren , RENNICH, Patrick , WATTERS, Matthew , RICE, Christian, Vincent
IPC: B64B1/08 , B64B1/32 , B64B1/44 , B64B1/62 , B64C2201/022 , B64C2201/042 , B64C2201/101 , B64C2201/12 , B64C2201/122 , B64C2201/127 , B64C2201/141 , B64C2201/16 , B64C39/024 , B64D2211/00 , G05D1/046 , G05D1/104
Abstract: An airship comprising an envelope having a shape, a volume, and a frontal area. A lifting gas within the envelope. A propulsion system. A volume change mechanism arranged to change the shape of the envelope, wherein the change in shape of the envelope changes the volume of the envelope, the change in volume of the envelope causes a change in the buoyancy of the airship, and the change in shape of the envelope causes the frontal area of the envelope to change proportionally to the change in volume of the envelope.
-
Patent Agency Ranking
公开(公告)号：WO2020214552A1
公开(公告)日：2020-10-22
申请号：PCT/US2020/028048
申请日：2020-04-14
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： WALKER, James, Dakota , MOORES, Louise, Kathryn , JULLENS, Clinton
Abstract: An airship (100) includes a ballonet (110), a ballonet tracking system (125), and a vehicle management system (140). The ballonet is disposed within the airship and includes a ballonet surface (120). The ballonet tracking system includes one or more light emitters (137) disposed within the ballonet at one or more fixed locations and one or more light detectors (138) disposed within the ballonet at the one or more fixed locations. The ballonet tracking system measures a plurality of distances between one or more fixed locations and one or more locations on the ballonet surface. The ballonet tracking system also calculates differences between a predetermined set of expected distances and the plurality of measured distances. Based on the calculated differences, the ballonet tracking system calculates a volume of the ballonet. The vehicle management system is communicatively coupled to the ballonet tracking system and controls the operation of the airship using the calculated volume of the ballonet.
-
公开(公告)号：WO2017114370A1
公开(公告)日：2017-07-06
申请号：PCT/CN2016/112218
申请日：2016-12-26
Applicant: 龚炳新
Inventor： 龚炳新
IPC: B64B1/62
CPC classification number: B64B1/62
Abstract: 一种充氢离子气的飞行器，由多级伸缩气缸、密封容器、光源、电场和推进器构成。气缸由塑料制成，气缸通过阀门与密封容器连接；升空时，打开密封容器阀门，氢离子进入气缸，气缸膨胀，当气缸内氢离子密度小于外部空气密度时，飞行器获得升力；气缸内安装有光源，降落时，利用光源照射氢离子，使氢离子之间产生吸引力，气缸内压力降低，外部大气压力压迫气缸的活塞，气缸体积减少，氢离子密度增大，当气缸内氢离子密度大于气缸外部空气密度时，飞行器降落，在电场力作用下氢离子进入密封容器，关闭阀门，收起气缸。该飞行器通过控制推进器来控制飞行器的飞行速度与方向。该飞行器成本低、不易爆炸，适于用作个人飞行器。
-
公开(公告)号：WO2011005851A2
公开(公告)日：2011-01-13
申请号：PCT/US2010/041197
申请日：2010-07-07
Applicant: CAPPER, Harry, M.
Inventor： CAPPER, Harry, M.
Abstract: The invention is an aerostat assembly, specifically an aerostats assembly including a camera for aerial photography. The aerostat assembly includes a boom assembly joined to a buoyant aerostat balloon. The boom assembly includes a pivot assembly joined to the tether line and booms. Thrusters at the ends of the booms allow an operator to maneuver the assembly to desired positions as well as rotate the booms about the pivot assembly.
Abstract translation: 本发明是一种浮空器组件，特别是包括用于航空摄影的照相机的浮空器组件。 浮空器组件包括连接到浮力浮空器气球的吊杆组件。 悬臂组件包括连接到系绳和悬臂的枢轴组件。 吊杆末端的推进器可让操作员操纵组件到所需的位置，并围绕枢轴组件旋转吊杆。
-
公开(公告)号：WO2008054401A3
公开(公告)日：2009-04-09
申请号：PCT/US2006043706
申请日：2006-11-08
Applicant: BELL HELICOPTER TEXTRON INC , SMITH MICHAEL R , CHOWDHURY SOMEN , THO CHENG-HO
Inventor： SMITH MICHAEL R , CHOWDHURY SOMEN , THO CHENG-HO
IPC: B64B1/62
CPC classification number: B64D25/18 , B64C27/006 , B64D2201/00
Abstract: A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A first gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the first gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag. A second gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.
Abstract translation: 一种用于飞行器的碰撞衰减系统，该系统具有由飞机携带并且大体上邻近飞机外部充气的气囊。 气囊具有至少一个用于从气囊的内部释放气体的排气口。 第一气体源与气囊的内部流体连通，以便由第一气体源产生的气体使气囊充气。 提供排气阀以控制通过每个通气口的气体流动，每个排气阀可选择性地配置在打开状态之间，气体可以从气囊的内部通过相关联的排气口，并且气体可以在气体 保持在气囊的内部。 第二气源被提供用于在通过至少一个通气口排出气体之后至少部分地重新充气气囊。
-
公开(公告)号：WO2004100289A8
公开(公告)日：2005-11-10
申请号：PCT/US2004013895
申请日：2004-05-05
Applicant: ION AMERICA CORP , MCELROY JAMES FREDERICK , SRIDHAR K R
Inventor： MCELROY JAMES FREDERICK , SRIDHAR K R
CPC classification number: H01M8/186 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/101 , B64C2201/127 , B64C2201/148 , B64C2201/165 , B64D27/24 , B64D2041/005 , B64D2211/00 , H01M8/04007 , H01M8/2475 , H01M2250/20 , Y02E60/528 , Y02T50/44 , Y02T50/62 , Y02T50/69 , Y02T90/32 , Y02T90/36 , Y10S429/901
Abstract: A neutral buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air.
Abstract translation: 一个中性浮力的飞艇，如飞艇，包含一个提升体，允许飞艇在位于飞艇的空气和燃料电池中保持中性浮力。 一种在中性浮力飞艇中产生动力的方法，包括向固体氧化物燃料电池提供燃料和氧化剂以产生动力，并将热量从燃料电池提供到位于远处的提升体，其中提升体允许飞艇 在空气中保持中性浮力。
-
-
-
-
-
-
-
-
-
Search Results
57
records
(took 0.012 seconds)
