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123 条记录 (耗时 0.043 秒)

    Inertia aerostat
    1.
    发明公开
    Inertia aerostat 审中-公开

    公开(公告)号：US20230322353A1

    公开(公告)日：2023-10-12

    申请号：US17972653

    申请日：2022-10-25

    申请人： Guangyuan XU

    发明人： Guangyuan XU

    IPC分类号： B64B1/38 ,  B64B1/24

    CPC分类号： B64B1/38 ,  B64B1/24

    摘要： An inertia aerostat having a vacuum compartment and an inertial floating device provided in the vacuum compartment, the inertial floating device comprises a drive shaft, drive devices, recycle and power generation devices and axially symmetric EMD rotation bodies, fixing devices are respectively provided at both ends of the drive shaft, the fixing devices are connected with the vacuum compartment, the drive devices are sleeved over the drive shaft, the axially symmetric EMD rotation bodies are connected with the drive devices via wheel ribs, the recycle and power generation devices are sleeved over the drive devices; by providing the vacuum compartment and the inertial floating device, inertial centrifugal forces generated by high speed rotation of the axially symmetric EMD rotation bodies in a gravitational field can be used as conversion media between kinetic energy and gravitational potential energy so free floating of the aerostat in the gravitational field can be realized.

    CAPTURE OF HYDROGEN BOILOFF
    2.
    发明申请
    CAPTURE OF HYDROGEN BOILOFF 有权

    公开(公告)号：US20230123465A1

    公开(公告)日：2023-04-20

    申请号：US17870717

    申请日：2022-07-21

    申请人： ZeroAvia, Inc.

    发明人： Gabriel DEVAULT ,  Bob Lee MACKEY

    IPC分类号： B64D37/04 ,  B64B1/24 ,  B64D41/00 ,  B64B1/62 ,  B60L58/30 ,  H01M8/04082 ,  H01M8/04089

    摘要： A hydrogen boiloff capture system. The hydrogen boiloff capture system having a cryogenic tank for storing liquid hydrogen. The hydrogen boiloff capture system also includes an intermediate tank fluidically coupled with the cryogenic tank. The intermediate tank is configured to receive hydrogen gas boiloff from the cryogenic tank. The intermediate tank is further configured to provide the hydrogen gas boiloff to a lighter-than-air craft to regulate buoyancy of the lighter-than-air craft. The intermediate tank is also configured to provide the hydrogen gas boiloff to a hydrogen fuel cell coupled to the lighter-than-air craft.

    HYBRID AIRSHIP AND RELATED ASSEMBLY AND/OR MAINTENANCE METHOD
    4.
    发明申请
    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.

    Device for reducing noise from jet-pylon interactions on jet engines
    7.
    发明授权
    Device for reducing noise from jet-pylon interactions on jet engines 有权
    用于减少喷气发动机上喷气塔相互作用的噪音的装置

    公开(公告)号：US08991749B2

    公开(公告)日：2015-03-31

    申请号：US13581050

    申请日：2011-02-25

    申请人： Alain Dravet ,  Jacques Michel Albert Julliard ,  Pierre Philippe Marie Loheac

    发明人： Alain Dravet ,  Jacques Michel Albert Julliard ,  Pierre Philippe Marie Loheac

    IPC分类号： B64B1/24 ,  B64C21/02 ,  B64C7/02 ,  B64D27/18 ,  F02K1/34

    CPC分类号： B64C21/02 ,  B64C7/02 ,  B64D27/18 ,  B64D33/06 ,  Y02T50/166

    摘要： An aircraft pylon for mounting a dual-flow or triple-flow jet engine, the pylon including an upper surface for connection to the aircraft, two side flanks, and a flange on the lower portion of the pylon. The pylon further includes at least one portion that extends downstream from the cold flow nozzle of the jet engine and lies in the cold flow and, on the portion thereof extending into the cold flow beyond the nozzle, at least one opening, positioned on one of the flanks of the pylon, by which an air stream is injected into or drawn from the gas flow that flows along the flanks of the pylon.

    摘要翻译： 一种用于安装双流或三流喷气发动机的飞机塔架，该塔架包括用于连接飞行器的上表面，两个侧翼和在塔架下部的凸缘。 塔架还包括至少一部分，其从喷气发动机的冷流喷嘴的下游延伸并且位于冷流中，并且在其延伸到超过喷嘴的冷流中的部分上，至少一个开口位于 塔的侧面，通过该侧翼将空气流注入或沿着沿着塔的侧面流动的气流引导。

    LENTICULAR AIRSHIP
    8.
    发明申请
    LENTICULAR AIRSHIP 有权
    航空公司

    公开(公告)号：US20110163200A1

    公开(公告)日：2011-07-07

    申请号：US12957989

    申请日：2010-12-01

    申请人： Pierre Balaskovic

    发明人： Pierre Balaskovic

    IPC分类号： B64B1/06 ,  B64B1/22 ,  B64B1/24 ,  B64B1/12

    CPC分类号： B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    摘要： An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    摘要翻译： 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

    Lighter-than-air vehicle for shading
    10.
    发明申请
    Lighter-than-air vehicle for shading 审中-公开
    用于阴影的轻型车辆

    公开(公告)号：US20090283630A1

    公开(公告)日：2009-11-19

    申请号：US12153259

    申请日：2008-05-15

    申请人： Ahmed Z. Al-Garni ,  Ayman H. Kassem

    发明人： Ahmed Z. Al-Garni ,  Ayman H. Kassem

    IPC分类号： B64B1/24 ,  B64B1/02 ,  B64D1/18

    CPC分类号： A45B23/00 ,  A45B2023/0093

    摘要： The lighter-than-air vehicle for shading is an airborne, movable system that provides sun shade for an open area. The vehicle is a substantially flat flying device having upper and lower surfaces, and which is filled with a lighter-than-air gas or gases, such as helium or hydrogen. The vehicle may be tethered to the ground through control wires, or may be fully autonomous and controlled by propeller fans. The required power may be provided by wire from ground, or through a portable power source, such as solar cells, mounted atop of vehicle. The vehicle has sun sensors that allow it to track the sun, and provides around the clock shaded area underneath its surface. The vehicle can also have pressure sensors and altitude sensors that may trigger an alarm in case of an emergency descent to the ground.

    摘要翻译： 用于阴影的轻型轻型车辆是一种机载的可移动系统，为开放区域提供遮阳。 车辆是具有上表面和下表面的基本上平坦的飞行装置，并且其填充有比空气较轻的气体或诸如氦气或氢气的气体。 车辆可以通过控制线连接到地面，或者可以完全自主并且由螺旋桨风扇控制。 所需的功率可以通过来自地面的电线或通过安装在车辆顶部上的便携式电源（例如太阳能电池）来提供。 车辆具有太阳传感器，可以让它跟踪太阳，并在其表面下方提供全天候的阴影区域。 车辆还可以具有压力传感器和高度传感器，以便在紧急下降到地面时触发报警。