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公开(公告)号：US20100276546A1
公开(公告)日：2010-11-04
申请号：US12384802
申请日：2009-04-09
Applicant: Sunstar Im
Inventor： Sunstar Im
CPC classification number: B64B1/08 , B64B1/005 , B64B1/16 , B64B1/18 , B64B1/20 , B64B1/28 , B64B1/58 , B64B2201/00 , B64C2201/00 , B64G1/005
Abstract: The structure provided multi-Levels of the center fuselage, two front wings, Extended mid-two wings and two rear wings with two vertical winglets.The fuselage has a cross section of half circle shaped fuselage.The first level comprises multi-fuel tanks, water tanks, Helium gas tanks, hydraulic, Pneumatic systems and plurality of the multi-landing gear bays and multi-cargo Compartments.The first level comprises a top cockpit and the plurality of the multi-passenger Cabins.The second level is comprises multi-central posts, multi-guy wires on the top center Beams, mid level, lower level center beams, leak proof sealed floor gates for the Multi-gas envelopes structure, under belly multi-pontoon air bags.The first level further comprises multi-jet power plants with multi-chute flaps.The second level may comprises, carbon fiber honey comb sandwich composite Multi-envelopes and multi-level soft gas envelopes.
Abstract translation: 该结构提供了中央机身的多层次，两个前翼，扩展中二翼和两个后翼与两个垂直的小翼。 机身有半圆形的机身横截面。 第一级包括多燃料箱，水箱，氦气罐，液压，气动系统和多个起落架舱和多货舱。 第一级包括顶部驾驶舱和多个多乘客舱。 第二级包括多中心柱，多中心柱，多中心杆，顶级中心梁，中级，下级中心梁，多气体信封结构的防漏密封地板门，腹部多浮桥气囊。 第一级还包括具有多溜槽襟翼的多喷射发电厂。 第二级可以包括碳纤维蜂蜜夹心复合多信封和多层软气体包络。
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公开(公告)号：US20100163669A1
公开(公告)日：2010-07-01
申请号：US12317733
申请日：2008-12-29
Applicant: Sunstar Im
Inventor： Sunstar Im
IPC: B64C1/00 , B64C3/00 , B64D11/00 , B64C35/00 , B64D11/06 , B64C9/00 , B64C3/14 , B64C1/14 , B64C25/04 , B64D45/00
CPC classification number: B64C1/0009 , B64C3/10 , B64C2001/0027
Abstract: An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear small wings, vertical winglets, and four levels. The fuselage has a cross-section of substantially a half circle fuselage shape. Being is wide enough to provide lifting force, and includes four levels separated by multi partition structure. The front wings are disposed horizontally in front portions of the fuselage. The rear small wings are disposed horizontally in rear portions of the fuselage. The vertical winglets are disposed at the wingtips of the rear small wings. The first level disposed at a bottom of the four levels includes a fuel tank storages and a plurality of landing gear bays. The second level disposed at a middle of the four levels includes cargo bay. The third level may comprise a top cockpit and a plurality of passenger cabins. The fuselage provides major portion of lifting force and the wings provides steering force, and lifting force. The fourth level may comprises a plurality of passenger cabins.
Abstract translation: 提供飞机结构。 飞机的飞机结构包括机身，前翼，后小翼，垂直小翼和四级。 机身具有大致半圆形的机身形状的横截面。 足够宽，提供提升力，包括由多分隔结构隔开的四级。 前翼水平放置在机身的前部。 后部小翼水平放置在机身的后部。 垂直小翼设置在后小翼的翼尖处。 设置在四级底部的第一级包括燃料箱储存器和多个起落架舱。 四级中间的第二级包括货舱。 第三级可以包括顶部驾驶舱和多个乘客舱。 机身提供主要部分的提升力，机翼提供转向力和提升力。 第四级可以包括多个乘客舱。
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公开(公告)号：US08459596B2
公开(公告)日：2013-06-11
申请号：US12592655
申请日：2009-12-01
Applicant: Sunstar Im
Inventor： Sunstar Im
Abstract: A sky/space elevator vehicle for going from the surface of a planet or moon up into space and back again. The vehicle has a single fuselage comprising multiple floor sections including a top and bottom cone. The movement of the vehicle is controlled by helium filled envelops as well as a combined jet and rocket propulsion system.
Abstract translation: 一个天空/太空电梯车辆，从行星或月球的表面进入太空，然后返回。 车辆具有单个机身，其包括多个底板部分，包括顶部和底部锥体。 车辆的运动由氦气填充的信封以及组合的喷气和火箭推进系统控制。
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公开(公告)号：US20110127382A1
公开(公告)日：2011-06-02
申请号：US12592655
申请日：2009-12-01
Applicant: Sunstar Im
Inventor： Sunstar Im
IPC: B64G1/00
Abstract: Sky/Space elevators structure comprises circle cylindrical structure provide multi floor Section levels. major center structure of center elevator provide transportations from Bottom cockpit levels to top cockpit floor levels.First section levels of multi floors provide bottom cockpit, escape cockpit with eject Rockets, control office, passenger rooms, bed rooms, food service rooms, lavatory rooms, Landing pads, winching machines with multi ropes.Second section levels of multi floors provide center elevators, circle center hangers, jet And rocket fuel tank storages and power plants, outer multi docking bays, multi robotic Arms anchor at outer walls at docking bays.Third section levels floors provide center elevators, circle cylindrical multi soft envelopes from top of middle floors to top of ceiling floors, circle cylindrical carbon fiber composite outer envelopes from top of middle floors to top floors, each envelopes of multi envelopes filled pressurized helium gas which make it float at atmosphere.Fourth section levels of top floor structure provide top cockpit, escape with eject rockets.
Abstract translation: 天空/太空电梯结构包括圆柱形结构，提供多层剖面。 中心电梯的主要中心结构提供从底部驾驶舱级别到顶级驾驶舱楼层的运输。 多层楼的第一层楼层提供底部驾驶舱，带弹出式的逃生驾驶舱火箭，控制室，客房，床房，食品服务室，卫生间，落地板，多根绞车绞车。 多层楼的二级楼层提供中心电梯，圆中心衣架，喷气式火箭燃料箱储存库和发电厂，外部多坞站，多机器人武器锚在对接舱的外墙。 第三级楼层提供中心电梯，圆形多层软包装，从中层楼顶至天花板顶层，圆形碳纤维复合外包装，从中层楼顶至顶层，多层信封填充加压氦气， 使其在大气中漂浮。 顶层结构的第四部分水平提供顶部驾驶舱，与弹出火箭逃脱。
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公开(公告)号：US08500070B2
公开(公告)日：2013-08-06
申请号：US12456008
申请日：2009-06-10
Applicant: Sunstar Im
Inventor： Sunstar Im
IPC: B64G1/14
CPC classification number: B64C39/068 , B64C3/56 , B64G1/14 , B64G1/401
Abstract: The present invention relates to a spacecraft structure that comprises a flat-wide body center fuselage, right and left side arch-wings and rocket propulsion power plant compartments, wherein the arch-wing is anchored to the fuselage via a foldable hinge mechanism. The fuselage structure is constructed as a single solid structure body of the spacecraft. A top portion at the rear of fuselage comprises a jet propulsion power plant to provide thrust during take-off from the airport. Both the left and right side arch-wings are anchored to a front and a rear portion of the center fuselage structure. Both the front and rear wing portions enable spacecraft lift and superior maneuverability during flight. The spacecraft is air tight and water tight and includes floatation devices.
Abstract translation: 本发明涉及一种包括平面宽体中心机身，左右侧拱翼和火箭推进动力装置隔间的航天器结构，其中，拱翼通过可折叠的铰链机构锚固在机身上。 机身结构构造为航天器的单一固体结构体。 机身后部的顶部包括喷气式推进动力装置，用于在从机场起飞时提供推力。 左右两侧拱翼都固定在中央机身结构的前部和后部。 前翼部分和后翼部分都能够使飞船上的升降机和机动性高。 航天器是气密和防水的，包括浮动装置。
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Patent Agency Ranking
公开(公告)号：US08439294B2
公开(公告)日：2013-05-14
申请号：US12384802
申请日：2009-04-09
Applicant: Sunstar Im
Inventor： Sunstar Im
IPC: B64B1/06
CPC classification number: B64B1/08 , B64B1/005 , B64B1/16 , B64B1/18 , B64B1/20 , B64B1/28 , B64B1/58 , B64B2201/00 , B64C2201/00 , B64G1/005
Abstract: The structure provided multi-Levels of the center fuselage, two front wings, Extended mid-two wings and two rear wings with two vertical winglets.The fuselage has a cross section of half circle shaped fuselage.The first level comprises multi-fuel tanks, water tanks, Helium gas tanks, hydraulic, Pneumatic systems and plurality of the multi-landing gear bays and multi-cargo Compartments.The first level comprises a top cockpit and the plurality of the multi-passenger Cabins.The second level is comprises multi-central posts, multi-guy wires on the top center Beams, mid level, lower level center beams, leak proof sealed floor gates for the Multi-gas envelopes structure, under belly multi-pontoon air bags.The first level further comprises multi-jet power plants with multi-chute flaps.The second level may comprises, carbon fiber honey comb sandwich composite Multi-envelopes and multi-level soft gas envelopes.
Abstract translation: 该结构提供了中央机身的多层次，两个前翼，扩展中二翼和两个后翼与两个垂直的小翼。 机身有半圆形的机身横截面。 第一级包括多燃料箱，水箱，氦气罐，液压，气动系统和多个起落架舱和多货舱。 第一级包括顶部驾驶舱和多个多乘客舱。 第二层包括多中心柱，多中心柱，多中心杆，顶级中心梁，中级，下层中心梁，多气体信封结构的防漏密封地板门，腹部多浮桥气囊。 第一级还包括具有多溜槽襟翼的多喷射发电厂。 第二级可以包括碳纤维蜂蜜夹心复合多信封和多层软气体包络。
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公开(公告)号：US20110114792A1
公开(公告)日：2011-05-19
申请号：US12592031
申请日：2009-11-18
Applicant: Sunstar Im
Inventor： Sunstar Im
IPC: B64G1/00
CPC classification number: B64G9/00
Abstract: Sky station structure comprises circle center core structure and circle outer Ring structure which comprises multi floor section levels.Major center core structure center elevator provide transportations from bottom Cockpit floor levels to top cockpit floor levels.First section levels of multi floors provide cockpit, control office, passenger Compartments, bed rooms, food service compartments, lavatory rooms, landing Pads, rope with winching machines and jet and rocket fuel tanks.Second section levels of multi floors provide center elevators, circle center Hangers, large circle outer ring hangers, jet and rocket power plants at outer Ring structures, inner docking and outer docking bays, multi robotic arms at Outer walls of docking bays,Third section levels of first floor levels provide center elevators, cylindrical Multi soft envelopes from floor levels to top levels of floors, cylindrical carbon Fiber honey comb composite outer envelopes from floor levels to top levels of Floors, multi envelopes of each envelope filled pressurized helium gas which Make it float at atmosphere.Third section levels of outer ring structure provide center post from floor to top Truss structure, cylindrical multi soft envelopes from floor levels to top of Truss structure, large cylindrical carbon fiber honey comb composite outer Envelopes from floor levels to top levels center truss structure, each envelope Floor zone need floor gate for repair and Inspection works.Fourth section levels comprises large circle outer truss structure, top of truss Bridge connected from center core structure to top of outer truss structure.Fifth section levels of top floor structure provide top cockpit and top control Tower.Also guy wire anchor at center of top control tower to top truss of outer Ring structures.
Abstract translation: 天台站结构包括圆心核心结构和圆外环结构，包括多层楼层。 主要中心核心结构中心电梯提供从底部驾驶舱楼层到顶部驾驶舱楼层的运输。 多层楼的第一层楼提供驾驶舱，控制室，乘客舱，床房，食品服务舱，卫生间，登陆垫，绞车绳和喷气式火箭燃料箱。 多层楼的二级楼层提供中心电梯，圆心衣架，大圆外环衣架，外环结构的射流和火箭发电厂，内对接和外部坞站，对接舱的外墙多机器人手臂，第三节 一层楼层提供中央电梯，圆柱形多层软包装，从地板层到顶层楼层，圆柱形碳纤维蜂蜜梳状复合外壳，从地板层到顶层，每个信封的多个信封填充加压氦气，使其成为 漂浮在大气层。 外环结构三级水平提供从地板到顶部的中心柱桁架结构，从地板到圆顶的桁架结构的圆柱形多层软包，大圆柱形碳纤维蜂巢复合材料外层从地层到顶层中心桁架结构的信封 信封地板区需要地板门进行维修和检查工作。 第四部分水平包括大圆外桁架结构，桁架顶部从中心芯结构连接到外桁架结构顶部。 顶层结构的第五段水平提供顶级驾驶舱和顶级控制塔。 还有顶部控制塔的中心的家伙线锚到外部环形结构的顶部桁架。
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公开(公告)号：US08464979B2
公开(公告)日：2013-06-18
申请号：US12455473
申请日：2009-06-02
Applicant: Sunstar Im
Inventor： Sunstar Im
Abstract: An aircraft structure is provide, an aircraft structure for an aircraft. including front Wing and rear wing of the Swan-Wing, vertical winglets and the first level Floor body. the fuselage has a cross-section of substantially flat fuselage shape being is Wide enough to provide lifting force. the front wing of the Swan-Wing are Disposed horizontally in front portion of the fuselage. rear wings of the Swan-Wing are disposed horizontally in rear portion of the fuselage. the vertical winglets Are disposed at the top of the rear fuselage. the first level disposed fuel tank storages, a Plurality of landing gear bays, cockpit with control panels, various avionics and Cabin doors.The top of the rear fuselage disposed jet power plants, the fuselage provide lifting force And the wings provides steering force and lifting force the whole structure of an aircraft Comprises carbon fiber honey comb composite molded structure which lighter weight And shear strong structure. the cockpit and cabin disposed. front window, rear Window, side window and doors. under the belly of the Swan-Wing disposed Pontoons.
Abstract translation: 提供飞机结构，用于飞机的飞机结构。 包括天鹅翼的前翼和后翼，垂直小翼和一级地板体。 机身具有基本平坦的机身形状的截面宽度足以提供提升力。 天鹅翼的前翼水平放置在机身的前部。 天鹅翼的后翼水平放置在机身的后部。 垂直小翼被置于后机身的顶部。 第一级设置燃料箱储存器，多个起落架舱，带控制面板的驾驶舱，各种航空电子设备和客舱门。 后部机身顶部设置喷气发电厂，机身提供提升力，机翼提供转向力和提升力整个飞机结构包括碳纤维蜂蜜复合模制结构，重量更轻，剪切坚固结构。 驾驶舱和客舱处理。 前窗，后窗，侧窗和门。 在天鹅翼的肚皮下放置了浮桥。
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公开(公告)号：US08333346B2
公开(公告)日：2012-12-18
申请号：US12592031
申请日：2009-11-18
Applicant: Sunstar Im
Inventor： Sunstar Im
IPC: B64G1/00
CPC classification number: B64G9/00
Abstract: A single center elevator, circle inner-ring, circle outer-ring elevator, vertical fuselage flight, vertical plan multi-floor section, bottom escape cockpit, top escape cockpit, mass-levitate, ascend, descend flight, first, second, third, fourth section, control tower, bed, food service, lavatory, landing pad, winch machine, jet/rocket fuel tank, circle passage hole, rope anchor hook, earth terminal station, center-hanger, up nozzle, down nozzle, Jet/rocket power plants, inner-docking bays, outer docking bays, multi robotic arms, cone shaped circular, glue, cylindrical multi-soft envelopes, cylindrical thick outer wall envelope, ceramic fiber fabric, geometric form, web-mesh carbon wire, upper chute-flap, down chute flap, helium gas, float, circle center post pole, truss bridge, top circle truss, hover, anchors, parking zone, V-shaped circle, laser, floor gate, test-gauge, repair/inspection, guy-wires, heavy grade mesh-ceramic fiber, launch/docking platforms, light grade web-mesh ceramic fiber, cargo-transporter, airship, disc-shaped circle structure.
Abstract translation: 单中心电梯，圆环内圈，圆外环电梯，垂直机身飞行，垂直方案多层楼，底部逃逸驾驶舱，顶部逃逸驾驶舱，群众悬浮，上升，下降飞行，第一，第二，第三， 第四节，控制塔，床，食品服务，洗手间，着陆垫，绞车机，喷气/火箭燃油箱，圆通道孔，绳锚钩，地面站，中心挂架，上喷嘴，下喷嘴，喷气/火箭 发电厂，内对接舱，外部坞站，多机器人手臂，锥形圆形，胶水，圆柱形多软包络，圆柱形厚壁外壳，陶瓷纤维织物，几何形状，网状碳丝， 襟翼，下滑槽，氦气，浮子，圆心柱，桁架桥，顶圆桁架，悬停，锚，停车场，V形圈，激光，地板门，测试仪，维修/检查， 电线，重级网状陶瓷纤维，发射/对接平台，轻质网状网眼 c纤维，货物运输，飞艇，圆盘形圆形结构。
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公开(公告)号：US20110000999A1
公开(公告)日：2011-01-06
申请号：US12455473
申请日：2009-06-02
Applicant: Sunstar Im
Inventor： Sunstar Im
Abstract: An aircraft structure is provide, an aircraft structure for an aircraft. Including front wings And rear wings of the Swan-Wings, vertical winglets and the first level floor body. The Fuselage has a cross-section of substantially flat fuselage shape being is wide enough to Provide lifting force. The front wings of the Swan-Wings are disposed horizontally in Front portion of the fuselage. The rear wings of the Swan-Wings are disposed Horizontally in rear portion of the fuselage.The vertical winglets are disposed at the top of the rear fuselage.The first level disposed fuel tank storages, a plurality of landing gear bays, cockpits with Control panels, various avionics and cabin doors.The top of the rear fuselage disposed jet power plants, the fuselage provide lifting force And the wings provides steering force and lifting force the whole structure of an aircraft Comprises carbon fiber honey comb composite molded structure which lighter weight And shear strong structure. The cockpit and cabins disposed. Front window, rear window Side window and doors. Under the belly of the Swan-Wings disposed pontoons.
Abstract translation: 提供飞机结构，用于飞机的飞机结构。 包括前翼和天鹅翼的后翅，垂直的小翼和一楼的地板。 机身的横截面基本平坦，机身宽度足以提供提升力。 天鹅翼的前翼水平放置在机身的前部。 天鹅翼的后翼横向设置在机身的后部。 垂直小翼设置在后机身的顶部。 第一级设置燃料箱储存器，多个起落架舱，具有控制面板的驾驶舱，各种航空电子设备和舱门。 后部机身顶部设置喷气发电厂，机身提供提升力，机翼提供转向力和提升力整个飞机结构包括碳纤维蜂蜜复合模制结构，重量更轻，剪切坚固结构。 驾驶舱和小屋处理。 前窗，后窗侧窗和门。 在天鹅翼的腹部处置浮筒。
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