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92 条记录 (耗时 0.017 秒)

    Adjustable weight ballasts for weighing down differently sized lighter-than-air balloons
    42.
    发明授权
    Adjustable weight ballasts for weighing down differently sized lighter-than-air balloons 失效
    可调节重量的镇流器用于称重不同大小的轻型气球

    公开(公告)号：US06666405B2

    公开(公告)日：2003-12-23

    申请号：US10100604

    申请日：2002-03-18

    申请人： Michael S. Isaacs

    发明人： Michael S. Isaacs

    IPC分类号： B64B170

    CPC分类号： B64B1/70

    摘要： An adjustable weight ballast for lighter-than-air balloon with a predetermined lift is disclosed, comprising at least two individual weights. There is a first means on each individual weight for selectively attaching two or more weights to each other to form a composite weight having a total weight at least equal to the predetermined lift of the balloon, and a second means for tethering the lighter-than-air balloon to this composite weight, in which manner a ballast for a balloon can have its weight incrementally adjusted to an amount just greater than the balloon's predetermined lift to thus securely tether the balloon to a surface on which the composite weight is supported without significantly exceeding the lift of the balloon.

    摘要翻译： 公开了一种具有预定升力的轻于气球的可调节重量的镇流器，其包括至少两个单独的重物。 在每个单独的重量上有一个第一装置，用于选择性地将两个或更多个重物彼此附接以形成总重量至少等于球囊的预定升程的复合重量，以及用于将较轻的重量系在一起的第二装置， 空气球到这种复合重量，其中气球的压载物可以使其重量逐渐地调整到刚好大于球囊的预定升力的量，从而将球囊牢固地束缚到其上支撑复合重物的表面，而不显着超过 气球的升力。

    ADJUSTABLE WEIGHT BALLASTS FOR WEIGHING DOWN DIFFERENTLY SIZED LIGHTER-THAN-AIR BALLOONS
    43.
    发明申请
    ADJUSTABLE WEIGHT BALLASTS FOR WEIGHING DOWN DIFFERENTLY SIZED LIGHTER-THAN-AIR BALLOONS 失效
    用于称重不同尺寸的轻型气球的可调重量重量

    公开(公告)号：US20030173457A1

    公开(公告)日：2003-09-18

    申请号：US10100604

    申请日：2002-03-18

    发明人： Michael S. Isaacs

    IPC分类号： B64B001/02 ,  B64B001/06

    CPC分类号： B64B1/70

    摘要： An adjustable weight ballast for lighter-than-air balloon with a predetermined lift is disclosed, comprising at least two individual weights. There is a first means on each individual weight for selectively attaching two or more weights to each other to form a composite weight having a total weight at least equal to the predetermined lift of the balloon, and a second means for tethering the lighter-than-air balloon to this composite weight, in which manner a ballast for a balloon can have its weight incrementally adjusted to an amount just greater than the balloon's predetermined lift to thus securely tether the balloon to a surface on which the composite weight is supported without significantly exceeding the lift of the balloon.

    摘要翻译： 公开了一种具有预定升力的轻于气球的可调节重量的镇流器，其包括至少两个单独的重物。 在每个单独的重量上有一个第一装置，用于选择性地将两个或更多个重物彼此附接以形成总重量至少等于球囊的预定升程的复合重量，以及用于将较轻的重量系在一起的第二装置， 空气球到这种复合重量，其中气球的压载物可以使其重量逐渐地调整到刚好大于球囊的预定升力的量，从而将球囊牢固地束缚到其上支撑复合重物的表面，而不显着超过 气球的升力。

    Method and system for setting hull parameter of airship and method of adjusting ascension rate of the same
    45.
    发明申请
    Method and system for setting hull parameter of airship and method of adjusting ascension rate of the same 有权
    设置飞艇船体参数的方法和系统及其提升方法

    公开(公告)号：US20030132343A1

    公开(公告)日：2003-07-17

    申请号：US10337998

    申请日：2003-01-08

    申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA

    发明人： Toyotoshi Kurose

    IPC分类号： B64B001/58

    CPC分类号： B64B1/44 ,  B64B1/70

    摘要： A method comprises: launching observation means configured to observe upper air environment immediately before launching an airship to acquire ambient air data on the actual conditions of the upper ambient air including altitude, pressure, wind direction, wind speed and temperature; determining an ascension profile for the airship by simulation using the ambient air data on the actual conditions of the ambient air; determining an initial quantity of Helium gas conforming to the actual conditions of the ambient air; and adjusting the quantity of Helium gas in the Helium room to the initial quantity of Helium gas to set an initial buoyancy. The method sets hull parameters for the hull of the airship to provide an ascension profile conforming to the actual conditions of the ambient air.

    摘要翻译： 一种方法包括：发射观测装置，被配置为在发射飞艇之前立即观察上部空气环境，以便根据包括高度，压力，风向，风速和温度在内的上部环境空气的实际状况获取环境空气数据; 通过使用关于环境空气的实际条件的环境空气数据进行模拟来确定飞艇的升高曲线; 确定符合环境空气实际条件的氦气初始量; 并将氦气室中的氦气量调节至初始量的氦气以设定初始浮力。 该方法为飞艇的船体设置船体参数，以提供符合环境空气实际条件的升降曲线。

    Unmanned lighter-than-air safe termination and recovery methods
    46.
    发明申请
    Unmanned lighter-than-air safe termination and recovery methods 有权
    无人驾驶轻便安全终点和恢复方法

    公开(公告)号：US20030109281A1

    公开(公告)日：2003-06-12

    申请号：US10129666

    申请日：2002-05-09

    发明人： Gerald M. Knoblach ,  Eric A. Frische

    IPC分类号： H04M001/00 ,  H04B001/38

    CPC分类号： G05D1/042 ,  B64B1/40 ,  B64B1/44 ,  B64B1/64 ,  B64B1/70 ,  G01S19/13 ,  H04B7/18504

    摘要： Innovative new methods in connection with lighter-than-air free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. Especially, termination of radio transmissions and flight related to regional, governmental and international border requirements, regulations and laws. The new methods comprise specific criteria, detection of the criteria and elements of operation for reducing or preventing illegal transmissions, for producing rapid descend to the ground, for environmentally acceptable landing and for facilitating recovery all with improved safety and enhanced compliance with known regulations.

    摘要翻译： 提供了与轻于空气的浮动平台相关的创新的新方法，便于合法的变送器操作，适当的平台飞行终止，环境可接受的着陆以及这些设备的恢复。 特别是终止与区域，政府和国际边界要求，条例和法律有关的无线电传输和飞行。 新方法包括具体标准，检测用于减少或防止非法传输的标准和操作要素，用于快速下降到地面，环境可接受的着陆和便于恢复，所有这些都是通过改进的安全性和加强对已知规定的遵守。

    Balancing device for air floaters
    47.
    发明授权
    Balancing device for air floaters 失效
    平衡空气浮子装置

    公开(公告)号：US5199667A

    公开(公告)日：1993-04-06

    申请号：US692370

    申请日：1991-04-26

    申请人： Yoshiro Fujii

    发明人： Yoshiro Fujii

    IPC分类号： B64B1/40 ,  B64B1/70

    CPC分类号： B64B1/40 ,  B64B1/70

    摘要： An air floater comprises a balloon body which seals a gas therein and balancing means detachably attached to the balloon body. The balloon body comprises a film composed of a central layer made of ethylene-vinyl alcohol copolymer-resin, an aluminum evaporated layer provided outside the central layer, and a heated adhesive layer provided inside the central layer. The balancing means comprises a plurality of magnetic cards which are attracted by an attraction portion composed of a magnetic body attached to the balloon body. The plurality of magnetic cards includes one card having a reference weight matched with the buoyant force of the balloon body, first weight balancing cards having weight heavier by stages than the reference weight, and second weight balancing cards having weight lighter by stages than the reference weight. The balancing means may comprise sublimate sealed in a bag body. The balancing means also may comprise a balancer cover composed of an adhesive surface portion having a rear surface to be adhered to the balloon body, a cover portion, a folding portion for integrally connecting both the adhesive surface portion and the cover portion, a balancer composed of one sheet and capable of separating into a reference balancer and a regulating balancer, and a both-sided adhesive sheet for rendering the reference balancer to adhere to the surface of the adhesive surface portion. The air floater is adapted for use as a miniature airship.

    摘要翻译： 空气浮子包括将气体密封的气囊体和可拆卸地附接到球囊体的平衡装置。 气囊体包括由乙烯 - 乙烯醇共聚物树脂制成的中心层，设置在中心层外侧的铝蒸镀层和设置在中心层内侧的加热粘合剂层构成的膜。 平衡装置包括被附接到气球体的磁体构成的吸引部分所吸引的多个磁卡。 多个磁卡包括具有与气球主体的浮力相匹配的参考重量的一个卡，具有比参考重量更重的重量的第一重量平衡卡和具有比参考重量更轻的重量的第二重量平衡卡 。 平衡装置可包括密封在袋体中的升华。 平衡装置还可以包括由粘合表面部分组成的平衡器盖，该粘合表面部分具有要粘附到气囊体的后表面，盖部分，用于将粘合表面部分和盖部分两者整体连接的折叠部分，平衡器 并且能够分离成参考平衡器和调节平衡器，以及用于使参考平衡器粘附到粘合剂表面部分的表面的双面粘合片。 空气浮筒适用于微型飞艇。