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11. 发明公开

KR1020040091795A 비행선 동력장치의 폐열을 이용한 부력과 압력 조절 시스템 无效
标题翻译：使用空气动力单元的废热通过调节燃气的温度来实现压力和压力控制系统
公开(公告)号：KR1020040091795A
公开(公告)日：2004-11-02
申请号：KR1020030025355
申请日：2003-04-22
申请人： 김태홍 , 허용만
发明人： 김태홍 , 허용만
IPC分类号： B64B1/62
摘要： PURPOSE: A buoyancy and pressure control system making use of waste heat of a power unit of an air ship is provided to cope with a change caused by leakage of buoyant gas or the external temperature of the air ship by adjusting the temperature of the buoyant gas via the waste heat of combustion gas produced from an internal combustion engine without waste of fuel. CONSTITUTION: A buoyancy and pressure control system making use of waste heat of a power unit of an air ship heats buoyant gas and raises the temperature of the buoyant gas via the waste heat of exhaust gas produced when fuel is burned for propulsion in a power engine comprising an external combustion engine or internal combustion engine of the air ship. The buoyancy and pressure control system comprises a sensor(C) detecting the temperature and pressure of a gasbag; a valve(B) receiving a signal from the sensor and switching a path of exhaust gas; an exchanger(H) connected to the valve; a fan(A) installed to help circulation of the buoyant gas; and a thermal insulator(G) arranged between an exhaust pipe(F) and the gasbag.
摘要翻译：目的：利用空中船舶动力装置余热的浮力和压力控制系统，通过调节浮力气体的温度来应对浮力气体泄漏或空气船外部温度的变化通过从内燃机产生的燃烧气体的废热，而不浪费燃料。构成：利用空运船的动力装置的废热的浮力和压力控制系统加热浮力气体，并且通过燃料燃烧产生的废气的废热在动力发动机中推进时提高浮力气体的温度包括空中船的外燃机或内燃机。浮力和压力控制系统包括检测气囊的温度和压力的传感器（C）; 接收来自所述传感器的信号并切换排气路径的阀（B）; 连接到阀的换热器（H）; 安装风扇（A）以帮助浮力气体循环; 以及布置在排气管（F）和气囊之间的绝热体（G）。

12. 实用新型

KR200235811Y1 야외를 자동 운동하는 물고기 장치 失效
标题翻译：用于户外运动的鱼用设备
公开(公告)号：KR200235811Y1
公开(公告)日：2001-10-06
申请号：KR2020010004843
申请日：2001-02-23
申请人： 김진경
发明人： 김진경
IPC分类号： B64B1/62
摘要： 본 고안의 효과는 공기와 비중이 같은 물고기 모양 장치에 있어서, 지상에 1대 이상의 송신기, 본 고안에서는 3대의 송신기를 설치해 놓고, 물고기 모양 장치 내부에 수신기와 연결된 전계강도 감지부들(23, 25)을 설치하여, 감지된 전계의 감도가 일정치 이하로 떨어지면 하이 신호가 스위칭회로들(31, 32)에 보내져서 크랭크축들(41, 42)이 작동하게 되어 물고기장치가 제자리에서 돌게 되어 일정 범위를 벗어나지 못하거나, 빙글빙글 돌게 되다가 조정자가 원격 조정으로 탈출하는 물고기 모양 장치를 제공하는 것이다.
본 고안의 또 다른 효과는 공기와 비중이 같은 물고기 모양 장치에 있어서, 평상으로는 몸체 전체가 머리 쪽이 약간 치켜올려져서 상향하다가 일정 고도 이상 올라가 기압센서부(14)의 기압이 일정치 이하로 떨어지면 하이 신호가 스위칭회로(33)에 걸리게 되어 크랭크축3(43)가 작동하여 하강하게 되고, 고도가 일정 레벨 이하로 떨어지면 다시 하이 신호가 해제되어 상향하게 되는 물고기 모양 장치를 제공하는 것이다.

13. 发明授权

KR102249117B1 탈 수 있는 로봇새 有权
公开(公告)号：KR102249117B1
公开(公告)日：2021-05-10
申请号：KR1020200121565
申请日：2020-09-21
申请人： 이정용
发明人： 이정용
IPC分类号： B64C33/00 , B64B1/70 , B64B1/62 , B64D27/24 , B64C1/24 , F16K31/06 , G06F3/01 , G05D1/00
摘要： 본발명은탈 수있는로봇새에관한것으로사람이탈 수있는크기로로봇새프레임을형성하고, 로봇새프레임의내부에수소나헬륨가스를주입한밸러스트탱크를구비하여밸러스트탱크로부터분사되는수소나헬륨가스를채움으로써로봇새프레임을부력시키는공기주머니를로봇새프레임의내부에형성한탈 수있는로봇새에관한것이다.

14. 发明公开

KR1020170032135A 날 수 있는 장치 审中-实审
标题翻译：一种能够飞行的装置
公开(公告)号：KR1020170032135A
公开(公告)日：2017-03-22
申请号：KR1020150129980
申请日：2015-09-14
申请人： 이정용
发明人： 이정용
IPC分类号： B64C31/04 , B64C33/02 , B64B1/40 , B64B1/58 , B64B1/62 , B64B1/64 , B64B1/70 , G01C19/00
摘要： 본발명은날 수있는장치에관한것으로서헬륨공기의압축과분사가가능한밸러스트탱크와헬륨공기의분사와흡입이가능한밸러스트탱크의밸브와밸브가내포되는신축적인공기주머니와팔을넣어서파닥일수 있는날개와공기주머니를몸에묶고체결할수 있는체결구가포함되는것으로서헬륨의분사에의하여공중에부양된뒤에팔을파닥거리는날개짓으로전진하고벨러스트탱크에서헬륨을흡임함으로써착륙할수 있게하는날 수있는장치에관한것이다.
摘要翻译：在本发明中翼通过插入柔性气囊和臂这意味着该阀和氦压缩空气的阀和可能的压载舱以及能够注入和抽吸在氦空气喷射padak天的压载舱涉及能够飞行的装置和作为空气中含有能够结合到所述主体紧固在袋通过氦的注入距离襟翼padak推进臂刺激之后在空气中和飞，以允许通过heupim氦在钟形锈罐降落的紧固件＆lt;

15. 发明公开

KR1020140064107A 열기를 이용한 패러글라이더 审中-实审
标题翻译：使用PARAGLIDER的热量
公开(公告)号：KR1020140064107A
公开(公告)日：2014-05-28
申请号：KR1020120131060
申请日：2012-11-19
申请人： 주식회사 윈텍에이티에스
发明人： 송현도
IPC分类号： B64C31/02 , B64D17/00 , B64B1/62
摘要： The present invention relates to a paraglider using heat capable of expanding a canopy using the variation of internal air density to rise upward by blowing heat into the canopy of a paraglider formed with a principle of wings of an airplane, flying at variable speeds by adjusting the angle of attack and the angle of bank depending on air currents, and flying without a burner by continuously expanding the canopy using wind at flight altitudes where the paraglider can fly safely. The present invention comprises the canopy having multiple cells arranged at regular intervals and communicating each other to be filled with the air, and capable of forming lift by allowing the bottom surface to have relatively faster speed and lower pressure of the wind than the top surface by Beroulli′s law; a harness which is connected to the canopy by multiple suspension wires, and on which a pilot can seat to fly at the altitudes where the canopy can fly by steering the angle of attack and the angle of bank with steering wires; an air inlet protruding from the center of the bottom surface of the canopy to communicate with at least one cell; and a burner arranged under the air inlet so that the canopy can be floated at the flyable altitudes by blowing the heat into the cells to have lower air density than atmosphere.
摘要翻译：本发明涉及一种滑翔伞，其使用能够使用内部空气密度的变化来扩展冠层的热量，其通过向形成有以飞行器的机翼的原理形成的滑翔伞的顶篷中的热量向上升高，以可变速度飞行，通过调节迎角和岸线的角度取决于气流，并且在没有燃烧器的情况下飞行，通过在滑翔机可以安全飞行的高度飞行中不断地扩张冠层。本发明包括具有以规则间隔布置并且彼此连通以填充空气的多个电池的顶盖，并且能够通过允许底表面比顶表面具有相对更快的速度和更低的风压力来形成升力 Beroulli定律通过多个悬挂线连接到天篷的线束，并且驾驶员可以通过转向迎角和转向线的角度在座舱可以飞行的高度处飞行; 从顶盖的底面的中心突出的空气入口与至少一个电池连通; 以及布置在空气入口下方的燃烧器，使得顶盖可以通过将热量吹入电池而具有比大气更低的空气密度浮动在可飞行高度。

16. 发明公开

KR1020100068546A 극진공 비행기 无效
标题翻译：空值
公开(公告)号：KR1020100068546A
公开(公告)日：2010-06-24
申请号：KR1020080126943
申请日：2008-12-15
申请人： 이남훈
发明人： 이남훈
IPC分类号： B64B1/62 , B64C29/04 , G08G5/02
CPC分类号： B64C29/04 , B64B1/06 , B64C25/02 , B64C25/68
摘要： PURPOSE: An extreme vacuum airplane is provided to reduce fuel and enable vertical taking off and landing without a runway by mounting an extreme vacuum around the top of the airplane. CONSTITUTION: A method for manufacturing an extreme vacuum airplane comprises following steps. An extreme vacuum floating tank is coupled with an airplane. The rotation of a jet engine is enabled. The possibility of vertical taking off and landing is measured. The emergent landing on the water is safely enabled.
摘要翻译：目的：提供极端的真空飞机，以减少燃料，并通过在飞机顶部安装极端的真空，无需跑道即可垂直起飞和着陆。构成：制造极端真空飞机的方法包括以下步骤。极端的真空浮筒与飞机相连。启用喷气发动机的旋转。测量垂直起降的可能性。水上的紧急着陆是安全启用的。

17. 发明公开

KR1020080036953A 원격 통신 또는 그 외의 과학적 용도의 플랫폼과 같은 무인 비행선 失效
标题翻译：作为电信或其他科学用途平台的无人机
公开(公告)号：KR1020080036953A
公开(公告)日：2008-04-29
申请号：KR1020077028907
申请日：2005-06-30
申请人： 아라비, 카멜
发明人： 아라비,카멜
IPC分类号： B64B1/60 , B64B1/62
CPC分类号： B64B1/60 , B64B1/62
摘要： The aim of the invention is to position an unmanned aircraft (1) that is used as a platform (10) for telecommunication or other scientific purposes at a predetermined altitude in the stratosphere. Said aim is achieved by an unmanned aircraft (1) comprising a pressurized balloon (11) which is filled with gas and supports the platform (10). The pressurized balloon (11) is arranged within an outer balloon (12; 12') which is provided with an aerodynamic external shape in the stratosphere and forms a low-pressure or high-pressure insulating chamber (20; 50) around the pressurized balloon (11), said insulating chamber (20; 50) being optionally filled with a medium. Furthermore, heating and cooling means are provided for the medium circulating in the insulating chamber (20; 50) while means encompassing electrically driven propellers (15) or similar located outside the outer balloon (12, 12') are supplied for maintaining the position of the platform relative to the Earth. The negative effects that extreme differences in temperature have on the gas pressure in the pressurized balloon are thus largely cancelled such that the pressurized balloon can be made of a lighter and cheaper material and the service life thereof is effectively extended.
摘要翻译：本发明的目的是将用作平台（10）的无人驾驶飞机（1）定位在平流层中的预定高度处的电信或其他科学目的。所述目的是通过一种无人驾驶飞机（1）来实现的，该飞机包括一个充满气体并支撑平台（10）的加压球囊（11）。加压球囊（11）布置在外球囊（12; 12'）内，其在平流层中设置有空气动力学外形，并在加压气球周围形成低压或高压绝缘室（20; 50）（11），所述绝缘室（20; 50）任选地填充有介质。此外，为在绝缘室（20; 50）中循环的介质提供加热和冷却装置，同时供应包含位于外球囊（12,12'）外部的电动螺旋桨（15）或类似物的装置，用于保持相对于地球的平台。因此，极端的温度差异对加压气囊中的气体压力的负面影响被大大地抵消，使得加压球囊可以由更轻和更便宜的材料制成，并且其使用寿命有效地延长。

18. 发明授权

KR102453997B1 가스 주입장치 有权
公开(公告)号：KR102453997B1
公开(公告)日：2022-10-14
申请号：KR1020210116438
申请日：2021-09-01
IPC分类号： B64B1/62 , B64C39/02 , G01W1/08 , G01F1/00 , G01F1/20 , G01F15/00 , G01F15/06 , F17C7/00 , F17C13/02

19. 发明授权

KR101913719B1 부양장치가 장착된 드론 有权
公开(公告)号：KR101913719B1
公开(公告)日：2018-10-31
申请号：KR1020170085646
申请日：2017-07-05
申请人： 공주대학교 산학협력단
发明人： 박성영
IPC分类号： B64C39/02 , B64C27/08 , B64D43/00 , B64C27/12 , B64D47/08 , B64D1/22 , B64B1/62 , B64B1/64
CPC分类号： B64C39/024 , B64B1/62 , B64B1/64 , B64C27/08 , B64C27/12 , B64C2201/024 , B64C2201/101 , B64C2201/108 , B64D1/22 , B64D43/00 , B64D47/08
摘要： 부양장치가장착된드론이개시된다. 본발명에따른부양장치가장착된드론은, 원격제어장치와제어신호를상호통신하면서공중비행하여물품을이동시키는것으로, 회전력에의해양력을발생시켜공중비행하면서사용자가원하는방향으로이동되도록구비되는비행수단과, 상기비행수단이양측에결합되어공중비행되면서원격제어장치와제어신호를상호통신하는드론몸체와, 상기드론몸체의상부일측에구비되어제어신호에의해부양력이가변되도록기체를주입또는배출시키는부양조절장치를포함하여구성된다. 이에따르면, 사용자에의해원격제어되어공중을비행함으로교통체증등에따른이동의지연이발생되지않으며, 공기보다가벼운기체가충전되는부력구가구비되어중량물의운반시무게로인해드론에가해지는하중을저감시켜드론의비행을용이하게하고, 배터리에충전된전기에너지가방전되어드론의회전익이작동을정지하여도부력구에충전된기체로인해지상으로서서히하강되므로드론의추락으로인한기물및 드론의파손과인명피해와같은안전사고를방지하는효과가있다.

20. 发明公开

KR20180072428A 가정용 미디어 포털 기능을 탑재한 무소음 무인 비행 장치 및 이의 제어 방법 审中-公开
公开(公告)号：KR20180072428A
公开(公告)日：2018-06-29
申请号：KR20160175977
申请日：2016-12-21
申请人： MOCAN CO LTD
发明人： KIM HYUN KYU
IPC分类号： B64C39/02 , B64B1/40 , B64B1/62 , B64D47/08
CPC分类号： B64C39/024 , B64B1/40 , B64B1/62 , B64C2201/022 , B64C2201/042 , B64C2201/101 , B64C2201/127 , B64C2201/141 , B64D1/00 , B64D47/08 , Y02T50/53
摘要： 가정용미디어포털기능을탑재한무소음무인비행장치및 이의제어방법을제공한다. 무인비행장치는상기무인비행장치의일측에구비되어기체가주입되도록구성되는벌룬, 상기무인비행장치의몸체에구비되어상기벌룬에주입되는기체를가열하도록구성되는가열기, 상기몸체에포함되어상기가열기에전력을공급하도록구성되는배터리, 상기몸체의일측면에구비되어상기배터리로부터공급되는전력을이용하여상기무인비행장치에추력을제공하도록구성되는로터및 상기몸체에포함되고상기무인비행장치의위치정보를기초로상기가열기와상기로터의구동을제어하도록구성되는제어기를포함할수 있다.

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