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公开(公告)号：US12091150B2
公开(公告)日：2024-09-17
申请号：US17920982
申请日：2021-04-21
Applicant: Jan Willem Van Egmond
Inventor： Jan Willem Van Egmond
CPC classification number: B64C1/08 , B64B1/08 , E04B1/3211 , F17C1/00 , F17C2201/0128 , F17C2201/054 , F17C2201/056 , F17C2203/012 , F17C2223/0123 , F17C2223/033
Abstract: A low-density structured material with good mechanical stability that can be used for three-dimensional structures, and methods to make and use same. In embodiments, the low-density structured material includes a first surface of interconnected polyhedrons, a plurality of tetrahedral arrangements whose base is the polyhedrons of the first surface, a second surface that is a web attached to the tetrahedral vertices of the tetrahedral arrangements, and panel materials overlying the web. The low-density structured material can be utilized in a variety of different structures.
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公开(公告)号：US20240228062A1
公开(公告)日：2024-07-11
申请号：US18488128
申请日：2023-10-17
Applicant: H2 Clipper, Inc.
Inventor： Rinaldo S. Brutoco , Robert H. Shelton , Michael R. Everman
Abstract: A system, method and apparatus are proposed to assist in assembling the frame, attaching the skin, and performing other tasks in manufacturing an airship and constructing other structures that are otherwise challenging, inefficient, or unsuitable for humans to perform, and/or that traditionally require significant investments in capital intensive manufacturing facilities. Several embodiments are proposed in which these and other recurring manufacturing tasks can be performed safely and efficiently with the assistance of autonomous, semi-autonomous, and/or human-directed robots, acting independently and in robot swarms.
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3.发明公开公开(公告)号：US20240116621A1
公开(公告)日：2024-04-11
申请号：US18486615
申请日：2023-10-13
Applicant: H2 Clipper, Inc.
Inventor： Rinaldo S. Brutoco , Robert H. Shelton , Shawn Merritt
CPC classification number: B64B1/08 , B64B1/14 , B64C39/024
Abstract: A lighter-than-air airship has an exoskeleton constructed of spokes and hubs to create a set of connected hexagrams comprised of isosceles triangles wherein the spokes flex and vary in length to produce the slope of said airship's surface. In one embodiment, the exoskeleton connects to a nose cone that includes a cockpit cabin for controlling the airship's operation from a single location that can be physically separated from the exoskeleton in response to catastrophic events and for autonomous and/or remotely piloted operation. An improved means is also provided for landing and unloading cargo, and through use of unmanned aerial vehicles in another embodiment, the airship is configured for remote pickup, transport, delivery and return of payloads such as packages. In yet another embodiment, the airship provides a communications platform for beam form transmission and satellite signal relay, including in combination with the foregoing disclosed attributes.
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公开(公告)号：US20230211866A1
公开(公告)日：2023-07-06
申请号：US17597684
申请日：2020-07-17
Applicant: Flying Whales
Inventor： Clément Barthe , Emmanuel Crespin , Jean-Marie Gourlin
Abstract: A method for erecting the structure of an aerostat in successive horizontal sections, starting from the top horizontal section, comprising an iteration of the following steps, starting from a current state of completion of the aerostat structure, lifting the current state of the structure, at first lifting points, by means of lifting means arranged in a current transverse position; placing a support device in line with second lifting points for lifting the current state of the structure; transferring the current state of the structure from the lifting means to the support device; moving the lifting means to another transverse position; completely assembling the horizontal section immediately below the current state of the structure on the structure.
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公开(公告)号：US20230150693A1
公开(公告)日：2023-05-18
申请号：US18056399
申请日：2022-11-17
Applicant: H2 Clipper, Inc.
Inventor： Rinaldo S. Brutoco , Robert H. Shelton , Michael R. Everman
Abstract: A system, method and apparatus are proposed to assist in assembling the frame, attaching the skin, and performing other tasks in manufacturing an airship and constructing other structures that are otherwise challenging, inefficient, or unsuitable for humans to perform, and/or that traditionally require significant investments in capital intensive manufacturing facilities. Several embodiments are proposed in which these and other recurring manufacturing tasks can be performed safely and efficiently with the assistance of autonomous, semi-autonomous, and/or human-directed robots, acting independently and in robot swarms.
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Patent Agency Ranking
6.发明申请公开(公告)号：US20170368782A1
公开(公告)日：2017-12-28
申请号：US15527976
申请日：2015-11-18
Applicant: AIRBUS GROUP SAS
Inventor： Albert ABISROR , Didier MESNAGE
IPC: B32B1/00 , B32B7/08 , B32B7/12 , B32B9/02 , B32B5/02 , B32B27/06 , B32B27/12 , B32B37/12 , B32B9/04 , B32B5/18 , B32B38/00 , B64B1/08 , B64B1/40 , B64G1/22 , B64C3/30
CPC classification number: B32B1/00 , B29C66/1122 , B29C66/30341 , B29C66/304 , B29C66/432 , B29C66/4326 , B29C66/45 , B29C66/49 , B29C66/729 , B29D22/02 , B29K2713/00 , B29L2009/00 , B29L2022/02 , B29L2031/3097 , B32B5/028 , B32B5/18 , B32B7/08 , B32B7/12 , B32B9/02 , B32B9/045 , B32B27/065 , B32B27/12 , B32B37/12 , B32B2038/008 , B32B2250/40 , B32B2262/02 , B32B2262/0269 , B32B2262/106 , B32B2266/02 , B32B2266/0221 , B32B2305/022 , B32B2305/18 , B32B2307/50 , B32B2307/7166 , B32B2457/12 , B32B2605/18 , B64B1/08 , B64B1/14 , B64B1/40 , B64C3/30 , B64G1/22 , B64G1/222 , B64G1/62 , B64G1/66 , B64G2001/224
Abstract: A multilayer sealed skin, in particular for an inflatable structure and that includes a first polymer film, a reinforcing fabric disposed on the first polymer film and a second polymer film disposed on the reinforcing fabric and adhered by means of an adhesive to the first polymer film through cavities in the reinforcing fabric. The skin can be applied to the production of an inflatable structural element such as an inflatable beam for which the skin forms an outer wall of the structural element and for which the first film of the skin forms an inner face of the outer wall of the structural element, and the second film forms an outer face of the wall.
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公开(公告)号：US09004397B2
公开(公告)日：2015-04-14
申请号：US13817891
申请日：2011-08-19
Applicant: Bojan Pecnik
Inventor： Bojan Pecnik
CPC classification number: B64B1/08 , B64B1/06 , B64B1/30 , B64B1/58 , B64C2201/022 , B64C2201/122 , B64C2201/127
Abstract: An autonomous stratospheric unmanned airship with an operating altitude from 5-22 km and with a multi-month operational cycle. Spheroid rigid geodesic frame of constant volume formed by a multitude of struts, with an outer envelope enclosing the frame defining the eigenfrequency spectrum of the airship above 20 Hz, with vibrational amplitudes between 0.1 and 1 cm. Independently controllable electrical propulsion units, attached to the frame in the horizontal plane passing through the center of mass, can change the direction and value of the thrust vector. Buoyancy is controlled with a system integrated inside the geodesic frame including buoyant fluid pressurized tanks, valves for the release of the buoyant fluid through the buoyant fluid conduit into the buoyant gas cell which fills the geodesic frame. Valves at the subsystem support platform enable ambient atmosphere to fill the internal volume of the frame not occupied by the buoyant gas cell.
Abstract translation: 自主的平流层无人飞艇，运行高度为5-22公里，并具有多个月的运行周期。 具有恒定体积的球体刚性测地框架由多个支柱形成，外围包围框架，其限定了20Hz以上的飞艇的本征频谱，震动振幅在0.1和1cm之间。 独立可控的电动推进装置可以改变推力矢量的方向和值。 浮力由集成在测地框架内的系统控制，包括浮力流体加压罐，用于通过浮力流体导管将浮力流体释放到填充测地框架的浮力气室中的阀。 在子系统支撑平台上的阀门能够使环境气氛填充未被浮力气体池占据的框架的内部体积。
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公开(公告)号：US20110233325A1
公开(公告)日：2011-09-29
申请号：US13075155
申请日：2011-03-29
Applicant: Dale Clifford Kramer
Inventor： Dale Clifford Kramer
IPC: B64B1/00
Abstract: A system for controlling the lift of an airship for carrying a cargo and a supply of fuel has a self supporting hull made of a flexible gas impermeable material. Air which is located in the hull is at an internal pressure which is greater than the atmospheric pressure of the air on the outside of the hull, and a bag filled with helium is located within the hull and is surrounded by the air in the hull. A heating means is provided to heat both the air and the helium. The bag located within the hull and surrounded by the air in the hull has enough helium in it at ambient temperature to lift all but the cargo and fuel in the airship, and the air and helium, when heated, provides increased buoyancy due to the increase of expansion of both heated gases to lift the airship with its fuel and cargo.
Abstract translation: 用于控制用于运送货物的飞艇的升力和供应燃料的系统具有由柔性气体不可渗透材料制成的自支撑船体。 位于船体中的空气处于大于船体外部空气的大气压的内部压力，并且填充有氦气的袋位于船体内并被船体中的空气包围。 提供加热装置以加热空气和氦气。 位于船体内并被环境中的空气包围的袋子在环境温度下具有足够的氦气，以提升飞艇上的所有货物和燃料，而加热时的空气和氦气由于增加而提供增加的浮力 扩张两种加热的气体，以便用其燃料和货物提升飞艇。
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公开(公告)号：US20090134268A1
公开(公告)日：2009-05-28
申请号：US11945047
申请日：2007-11-26
Applicant: Richard L. Kulesha
Inventor： Richard L. Kulesha
CPC classification number: B64B1/06 , B64B1/08 , B64C2201/022
Abstract: An aerial load lifting system features a non-rigid or blimp-type dirigible providing a lighter-than-air envelope that is placed within a structural shell. The system is designed so that the envelope provides essentially neutral buoyancy for the structure, leaving only the cargo weight to be lifted by the rotors. The structural shell supports the engine, fuel tank, rotors, and transmission system that power the lift and vectoring of the aircraft, in addition to supporting the cargo load. The structural shell transfers the weight of the load directly to the location of the rotors, thus avoiding stress on the envelope.
Abstract translation: 一种空中负载提升系统具有非刚性或微型飞行器，提供放置在结构外壳内的轻于空气的封套。 该系统的设计使得外壳为结构提供基本上中性的浮力，只留下货物由转子提升。 结构外壳还支持发动机，燃油箱，转子和传动系统，以支持飞机的起重和矢量化，以及支撑货物载荷。 结构外壳将负载的重量直接转移到转子的位置，从而避免了信封上的压力。
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公开(公告)号：US6148609A
公开(公告)日：2000-11-21
申请号：US321796
申请日：1999-05-27
Applicant: Anthony Italo Provitola
Inventor： Anthony Italo Provitola
CPC classification number: B64G1/401 , B64B1/08 , B64B1/58 , B64C29/005 , B64C39/001 , B64G1/402 , F02K9/42 , B64G1/002
Abstract: A turbo-rocket thruster is disclosed in which the turbine compressor is used to intake and compress a gaseous fuel for combustion with a stored oxidizer injected into the compressed gaseous fuel stream. The compressor stage is driven by the turbine stage, which is driven by burning gaseous fuel passing across the turbine blades. The burned gases are then expanded through an exhaust nozzle and thereby ejected to produce reaction thrust.
Abstract translation: 公开了一种涡轮火箭推进器，其中涡轮压缩机用于吸入和压缩用于燃烧的气体燃料，其中储存的氧化剂被注入到压缩气体燃料流中。 压缩机级由涡轮机级驱动，涡轮级通过燃烧通过涡轮叶片的气体燃料驱动。 然后将燃烧的气体通过排气喷嘴膨胀，从而喷射以产生反作用力。
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