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公开(公告)号：US11487189B2
公开(公告)日：2022-11-01
申请号：US16630426
申请日：2017-07-12
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: A high-place observation device for stably performing a fixed-point observation of a target object from a high place is provided. The high-place observation device provides a long pole which is formed to extend and contract freely and which stands on the installation surface, a rotorcraft for positioning the pole to a desirable height position by extending and contracting the pole by a floating force in a connected state, a winding mechanism which fixes and maintains the height position of the pole to the height position set by the rotorcraft, and a camera attached to the rotorcraft.
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公开(公告)号：US20230014788A1
公开(公告)日：2023-01-19
申请号：US17935829
申请日：2022-09-27
Applicant: AERONEXT INC.
Inventor： Yoichi SUZUKI
Abstract: A high-place observation device for stably performing a fixed-point observation of a target object from a high place is provided. The high-place observation device provides [Solution] Provides a long pole which is formed to extend and contract freely and which stands on the installation surface, a rotorcraft for positioning the pole to a desirable height position by extending and contracting the pole by a floating force in a connected state, a winding mechanism which fixes and maintains the height position of the pole to the height position set by the rotorcraft, and a camera attached to the rotorcraft.
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公开(公告)号：US09139279B2
公开(公告)日：2015-09-22
申请号：US13623757
申请日：2012-09-20
Applicant: Stephen B. Heppe
Inventor： Stephen B. Heppe
Abstract: In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.
Abstract translation: 在一个例子中，长期耐力飞艇系统包括有效载运飞艇和与有效载客飞艇机械连接以形成第一组合飞艇的第一物流飞艇，有效载客飞艇和具有至少两倍的设计能力的物流飞艇， 至少有以下至少一个：发电能力，推进能力，耐力能力和升力能力，其中第一组合飞艇是自由飞行的，比空中轻，并且被配置为在没有物理连接的情况下保持高达30天以上 到地面。 还提供了长期耐力飞艇作业的说明性方法。
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公开(公告)号：US11352134B2
公开(公告)日：2022-06-07
申请号：US15863018
申请日：2018-01-05
Applicant: Raytheon Company
Inventor： Gregory W. Heinen
IPC: B64C39/02 , H01Q1/34 , B64B1/44 , B64B1/70 , B64B1/34 , H01Q1/22 , H01Q1/08 , G01S7/40 , H01Q1/28 , B64B1/54
Abstract: A flight vehicle includes a drone with a pair of shaped protrusions mechanically coupled to the drone. One of the shapes is a hollow lift-producing shape, such as being a balloon filed with a lighter-than-air gas, and the other of the shapes is below the drone. The shape below the drone may be a hollow shape that does not produce lift, for example being a balloon filled with air. The shapes may be similar in size and shape, so as to provide similar drag characteristics. The shapes may be opposite ends of a support, such as a stick, rod, or other (relatively) slender structure. The vehicle includes a payload, such as radar calibration equipment or an antenna. The drone may be used to counteract wind forces on the flight vehicle, and/or to otherwise position the flight vehicle.
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公开(公告)号：US6050874A
公开(公告)日：2000-04-18
申请号：US806499
申请日：1997-02-27
Applicant: Mary Kae Ries
Inventor： Mary Kae Ries
CPC classification number: A63H27/10 , A63H2027/1041 , A63H2027/1075
Abstract: A coupling strip for connecting a plurality of balloons in adjacent sequential position to one another in fascial and inexpensive manner consisting of an elongate flexible strip, made from plastic, cloth or other lightweight flexible material and in which the length thereof is determined by the number of sequential adjacent balloons one wishes to couple together for decorative or for any other purpose of notice and in which the width thereof is sufficient only to carry an aperture between the edges, the coupling strip consisting of a sequence of such apertures, spaced from one another substantially throughout the length of the coupling strip, for receiving the neck of a balloon. The apertures may be spaced at any desired distance from one another so as to facilitate insertion of a balloon neck in either a budding relation to an adjacent balloon or at any desired distance therefrom throughout the length of the coupling strip.
Abstract translation: 一种连接条，用于以紧凑且便宜的方式将多个气囊彼此相连的位置连接起来，该细长的柔性条由塑料，布或其它轻质柔性材料制成，其长度由 顺序的相邻气球希望联接在一起用于装饰或用于任何其他目的，并且其宽度仅足以在边缘之间承载孔，该连接条由一系列这样的孔组成，彼此间隔开大致 在连接条的整个长度上，用于接收气球的颈部。 孔可以彼此间隔任何期望的距离，以便于将球囊颈部以与芽壁相邻的气囊插入，或者在连接条的整个长度处以任何期望的距离插入。
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Patent Agency Ranking
公开(公告)号：US3432122A
公开(公告)日：1969-03-11
申请号：US3432122D
申请日：1967-06-19
Applicant: GOODYEAR AEROSPACE CORP
Inventor： FLICKINGER MAYNARD L , ROSS ROBERT S
CPC classification number: B64B1/40
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7.发明授权公开(公告)号：US11774832B2
公开(公告)日：2023-10-03
申请号：US17935829
申请日：2022-09-27
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
CPC classification number: G03B17/561 , B64B1/44 , B64B1/54 , B64C27/00 , B64D47/08 , B64F3/00 , G03B15/006
Abstract: A high-place observation device for stably performing a fixed-point observation of a target object from a high place is provided. The high-place observation device provides [Solution] Provides a long pole which is formed to extend and contract freely and which stands on the installation surface, a rotorcraft for positioning the pole to a desirable height position by extending and contracting the pole by a floating force in a connected state, a winding mechanism which fixes and maintains the height position of the pole to the height position set by the rotorcraft, and a camera attached to the rotorcraft.
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公开(公告)号：US5820243A
公开(公告)日：1998-10-13
申请号：US816151
申请日：1997-03-12
Applicant: Chih-Chen Chang
Inventor： Chih-Chen Chang
CPC classification number: F21V21/16 , B64B1/54 , F21S4/10 , F21V21/00 , F21V3/023 , A63H2027/1058 , A63H2027/1075 , Y10S362/806
Abstract: The present invention provides an air suspended luminary that includes balloons and luminaries. By means of floating balloons, the present invention is to suspend an end of a string of luminaries on the bottom of the balloon, the another end of the string of luminary is fixed on the ground to control the suspending height. Said balloon can connect with the string of luminaries through a hollow transparent connecting object. The present invention can be combined with many balloons and strings of the luminaries to create varied shapes and used in varied field especially in an expense of open field.
Abstract translation: 本发明提供一种包括气球和发光体的空气悬浮照明。 通过浮动气球，本发明是将气球的底部上的一串照明器的一端悬挂在一起，将灯串的另一端固定在地面上以控制悬挂高度。 所述气球可以通过中空的透明连接物体与灯串连接。 本发明可以与许多气球和灯串组合以产生不同的形状，并且在各种领域中使用，特别是以开放场的费用。
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公开(公告)号：US4361295A
公开(公告)日：1982-11-30
申请号：US112220
申请日：1980-01-15
Applicant: Joachim Wenzel
Inventor： Joachim Wenzel
CPC classification number: F24J2/5271 , B64B1/40 , F24J2/5241 , F24J2/5264 , Y02E10/47 , Y10S136/292
Abstract: Solar power station with semiconductor solar cells for generating electric power, wherein the semiconductor solar cells are provided on a member such as a balloon or a kite which carries the solar cells into the air. The function of the balloon or kite can also be fulfilled by a glider or airship. The solar power station can be operated by allowing the system to ascend at sunrise and descend at sunset or when the wind is going to be too strong in order to avoid any demage.
Abstract translation: 具有用于产生电力的半导体太阳能电池的太阳能发电站，其中将半导体太阳能电池设置在将太阳能电池携带到空气中的诸如气球或风筝的构件上。 气球或风筝的功能也可以通过滑翔机或飞艇来实现。 太阳能发电站可以通过允许系统在日出时上升，在日落时下降，或者当风力太强时，以避免任何降水。
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公开(公告)号：US20220127017A1
公开(公告)日：2022-04-28
申请号：US17437916
申请日：2020-03-10
Applicant: Szabolcs TAKÁCS
Inventor： Szabolcs TAKÁCS
Abstract: The subject of the present invention relates to a floating platform (10) for launching a space rocket (100) from high altitude comprising a support structure (20) for suspending the space rocket (100) and which support structure (20) can be releasably connected to the space rocket (100), one or more hydrogen or helium filled balloons (30) fixed to the support structure (20), one or more rigid-walled tanks (12) and a compressor module (40) connected to the one or more balloons (30) and rigid-walled tanks (12) for delivering at least a portion of the hydrogen or helium stored in the balloons (30) into the one or more rigid-walled tanks (12), said one or more balloons (30) are dimensioned to lift the floating platform (10) and the space rocket (100) connected thereto, characterized in that the floating platform (10) comprises a hydrogen or helium-filled, preferably cigar-shaped rigid-walled balloon (35) which is releasably connected to the support structure (20) and secured to the top of the space rocket (100) and which is suitable for connecting the space rocket (100) to the support structure (20). The invention further relates to a method for launching a rigid-walled balloon (35) into space.
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