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1. 发明授权

KR100917780B1 가변형 위그선 플랩 장치 失效
标题翻译： VARIABLE TYPE WIG CRAFT FLAP DECIVE
公开(公告)号：KR100917780B1
公开(公告)日：2009-09-21
申请号：KR1020090009529
申请日：2009-02-06
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이한진 , 이창민
IPC分类号： B63B1/16 , B63B1/18 , B64C9/14
CPC分类号： Y02T50/44
摘要： A variable type WIG craft flapping apparatus is provided, which can obtain stability of the aviation by absorbing impact by the waves using each piece plate. A variable type WIG craft flapping apparatus comprises a front flap part(310) and a rear flap part(320). To the front flap part, a flap actuator(313) is connected. The rear flap part is movably connected to the end of the front flap part. The rear flap part is comprised of the soft ductile flat board of the different piece. The variable form WIG craft flapping apparatus includes the rear flap part receiving part(316).
摘要翻译：提供了一种可变式的WIG工艺拍打装置，其可以通过使用每个片板吸收由波浪产生的冲击来获得航空器的稳定性。一种可变式的WIG工艺拍打装置包括前翼片部分（310）和后片部分（320）。向前翼片部分连接有翼片致动器（313）。后挡板部分可移动地连接到前翼片部分的端部。后挡板部分由不同件的柔性延性平板组成。可变形式的WIG工艺拍打装置包括后翼片部分接收部分（316）。

2. 发明授权

KR101135167B1 피치-업 제어가 가능한 위그선 및 위그선의 피치-업 제어 방법 失效
标题翻译：用于控制倾斜的WIG折页和用于控制摆放的倾斜的方法
公开(公告)号：KR101135167B1
公开(公告)日：2012-04-16
申请号：KR1020110065851
申请日：2011-07-04
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 강국진 , 이창민 , 이한진 , 박진형
IPC分类号： B63B1/18 , B60V3/06 , B60V3/08 , B64C15/14
摘要： PURPOSE: A wig craft which can be subjected to pitch-up control and a pitch-up control method for the same are provided to quickly and actively deal with pitch-up by spraying compressed air downward from the rear side of the centroid of a wig craft. CONSTITUTION: A wig craft which can be subjected to pitch-up control comprises a body(110) in which a main wing is installed, a spray assembly(150) which is installed behind the main wing to be located on the rear side of the centroid of the wig craft in the longitudinal direction of the wig craft and sprays compressed air to the lower side of the wig craft, and a control assembly which controls the operation of the spray assembly in order to control the pitch-up state of the wig craft.
摘要翻译：目的：提供可以进行俯仰控制的摆动工艺及其俯仰控制方法，通过从假发的重心的后侧向下喷射压缩空气，快速且积极地处理俯仰工艺。构成：可以进行俯仰控制的假发工艺包括安装有主翼的主体（110），安装在主翼后面的喷涂组件（150），其位于假发工艺在假发工艺的纵向方向上的重心，并将压缩空气喷射到假发工艺的下侧;以及控制组件，其控制喷雾组件的操作以控制假发的俯仰状态工艺。

3. 发明公开

KR1020090095928A 위그선의 양력 증강 장치 无效
标题翻译：用于发条的提升装置
公开(公告)号：KR1020090095928A
公开(公告)日：2009-09-10
申请号：KR1020080021162
申请日：2008-03-06
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이창민 , 이한진
IPC分类号： B63B1/16
CPC分类号： B60V1/08 , B64C3/54
摘要： A device for increasing the upward force of a WIG craft is provided to maximize the ground effect of the WIG craft by making the distance between a wing and a sleep narrow while increasing the cord length and area of the wing. A device for increasing the upward force of a WIG craft comprises a wing body(100), a leading edge extension unit(200), and a trailing edge extension unit(300). The wing body takes in charge of a body of the wing of the WIG craft. The leading edge extension unit comprises a leading edge of the wing body. The leading edge extension unit has a leading edge extended board(210), a leading edge extended board drive motor(220) and leading edge extended board connection rod(230). The leading edge extended board enlarges the wing area and the code length of the wig craft. The trailing edge extension comprises a trailing edge of the wing body. The trailing edge extension unit has a trailing edge extended board(310), a trailing edge extended board drive motor(320) and a trailing edge extended board connection rod(330). The trailing edge extended board enlarges the wing area and the code length of the wig craft. The trailing edge extended board drive motor operates the leading edge extended board. The trailing edge extended board connection rod connects the leading edge extended board and leading edge extended board drive motor.
摘要翻译：提供用于增加WIG工具的向上力的装置，以通过使翼和睡眠之间的距离变窄而使翼的长度和面积增大，从而使WIG工艺的地面效果最大化。用于增加WIG工艺的向上力的装置包括翼体（100），前缘延伸单元（200）和后缘延伸单元（300）。翼体负责WIG工艺的机翼的身体。前缘延伸单元包括翼体的前缘。前缘延伸单元具有前缘延伸板（210），前缘延伸板驱动电机（220）和前缘延伸板连接杆（230）。前缘延伸板扩大了机翼面积和假发工艺的代码长度。后缘延伸部包括翼体的后缘。后缘延伸单元具有后缘延伸板（310），后缘延伸板驱动电机（320）和后缘延伸板连接杆（330）。后缘延伸板扩大了机翼区域和假发工艺的代码长度。后缘延长板驱动电机操作前缘延伸板。后缘延长板连接杆连接前缘延伸板和前缘延伸板驱动电机。

4. 发明授权

KR100899015B1 프로펠러 후류 압력을 이용한 위그선 이수 장치 失效
标题翻译：使用螺旋桨空气压缩水的WIG冲切设备
公开(公告)号：KR100899015B1
公开(公告)日：2009-05-21
申请号：KR1020090008122
申请日：2009-02-02
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이한진 , 이창민
IPC分类号： B63B1/16 , B63B1/18
摘要： 본 발명은 프로펠러의 후류 압력을 이용한 위그선 이수 장치에 관한 것으로, 상기 위그선 이수 장치는 상기 위그선의 주 날개 상면에 설치하여 이수 시 동력을 발생하는 프로펠러 엔진과, 상기 프로펠러 엔진을 지지하는 파일론과, 상기 파일론에 설치되어 프로펠러의 후류를 주 날개 하부로 연결하는 덕트와, 상기 주 날개 끝단에 설치되어 상기 위그선의 이수 시 하방각을 형성하여 양력을 증가시키는 역할을 하는 플랩으로 구성하되, 파일론 전면 일측과 주 날개 하면 일측으로 연결되어, 프로펠러 엔진 후면의 압력을 상기 주 날개 하부로 전달함으로써 공기쿠션의 형성을 용이하게 하는 덕트를 추가로 형성하여, 위그선을 조기에 부상시켜 물의 저항을 감소시키는 효과를 얻을 수 있으며, 종래의 추가 엔진 설비라는 문제점을 해결하여 제작 과정에서 발생하는 비용 및 위그선의 무게를 줄일 수 있는 이점을 제공한다.
위그선, 프로펠러 엔진, 파일론, 덕트, 플랩

5. 发明授权

KR101043931B1 상공 부상형 신재생에너지 발전 장치 失效
标题翻译：用于产生新的和可再生能源的浮动式装置
公开(公告)号：KR101043931B1
公开(公告)日：2011-06-29
申请号：KR1020100117806
申请日：2010-11-25
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 강국진 , 이창민 , 이한진 , 박진형
IPC分类号： F03D5/00 , F03D5/06 , H02S10/00
CPC分类号： F03D5/06 , F05B2240/921 , H02S20/00 , Y02E10/50 , Y02E10/70
摘要： PURPOSE: A new renewable energy generation device is provided to prevent global warming by blocking a part of light by a plurality of kites. CONSTITUTION: A new renewable energy generation device comprises a plurality of kites(100), a plurality of extension lines(200), a power generation unit(300), and an interval holding unit(400). One of kites, which are arranged on edge part, includes a camber and a wing unit. The wing generates power toward the edge of the center of kite. A plurality of extension lines interlinks a plurality of kites on ground. The power generation unit is installed one of extension lines. The power generation unit produces the electrical energy of solar energy and wind force. The interval holding unit forms a plane crossing the extension direction of a plurality of extension lines. The interval holding unit keeps a plurality of kites with at a regular interval.
摘要翻译：目的：提供一种新的可再生能源发电装置，以通过多个风筝阻挡一部分光来防止全球变暖。构成：一种新的可再生能源发电装置，包括多个风筝（100），多条延长线（200），发电单元（300）和间隔保持单元（400）。布置在边缘部分的风筝之一包括一个弧形和一个机翼单元。机翼向风筝中心的边缘发电。多个延长线将多个风筝互相连接。发电单元安装了延长线之一。发电机组产生太阳能和风力的电能。间隔保持单元形成与多个延长线的延伸方向交叉的平面。间隔保持单元以规则的间隔保持多个风筝。

6. 发明公开

KR1020090095929A 코닝 디스플레이 无效
标题翻译：正在显示
公开(公告)号：KR1020090095929A
公开(公告)日：2009-09-10
申请号：KR1020080021163
申请日：2008-03-06
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이창민 , 이한진
IPC分类号： B63B49/00 , G01C21/20 , G08G3/00
CPC分类号： B63B49/00 , G01C21/203 , G08G3/00
摘要： A conning display is provided to allow workers to handle surrounding conditions by transmitting information to a worker at bridge and reducing a time and cost for obtaining necessary information. In a conning display, a ship shape is arranged on the center of a screen. Navigation information relating to an operation state of a minimum instrument is displayed around the ship shape through one screen. The navigation information includes a wind and air speed indicator(A-1), a depth of water indicator(A-2), a heading angle indicator(A-3), a rate of turn indicator(A-4), a propeller RPM(revolution per minute) indicator(A-5), a speed of the ship and a turn direction/speed indicator(A-6), an engine telegraph indicator(A-7), a steering gear indicator(A-8), and a time and ship position indicator(A-9).
摘要翻译：提供了一个隐藏的显示，以允许工人通过向桥梁的工作人员传递信息来处理周围环境，并减少获得必要信息的时间和成本。在一个暗示的显示中，一个船形被布置在屏幕的中心。通过一个屏幕围绕船舶形状显示与最小仪器的操作状态相关的导航信息。导航信息包括风和空气速度指示器（A-1），水位指示器（A-2），航向角度指示器（A-3），转向指示器（A-4），螺旋桨（A-5），转速方向/速度指示器（A-6），发动机电报指示器（A-7），舵机指示器（A-8），和时间和船位置指示（A-9）。

7. 发明授权

KR101043930B1 수면에 대한 이착수 성능 향상을 위한 에어 포켓을 활용한 위그선 및 그의 이착수 방법 失效
标题翻译： WIG CRAFT利用空气袋加强对水和甲烷的吸收/吸收能力，使其在水中脱盐
公开(公告)号：KR101043930B1
公开(公告)日：2011-06-29
申请号：KR1020110021228
申请日：2011-03-10
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 강국진 , 이창민 , 이한진 , 박진형
IPC分类号： B63B1/16 , B60V1/08 , B60V3/08
CPC分类号： B60V1/08 , B60V3/08 , B63B1/38 , B64C35/002 , B64D2201/00 , Y02T70/122
摘要： PURPOSE: A WIG craft using an air pocket and a takeoff and landing method thereof are provided to reduce resistance of water when the WIG craft is take off to thereby decrease fuel consumption. CONSTITUTION: A WIG craft(100) using an air pocket for improve takeoff and landing performance includes a body(110), a wing(120), an unfolding unit(130), and an injection unit(140). The wing is installed symmetrically based on the body. The unfolding unit is installed at the bottom of the wing. When expansion air is injected into the unfolding unit, the unfolding unit is expanded to form the cross section of a base loop shape so as to be unfolded downward. The injection unit is installed at the bottom of the wing. The injection unit injects air to a direction facing the surface of water in an area limited by the unfolding unit.
摘要翻译：目的：提供一种使用气囊的起重工艺及起飞和着陆方法，以在WIG工艺起飞时降低水的阻力，从而降低燃料消耗。构成：使用空气袋改善起飞和着陆性能的工艺（100）包括主体（110），机翼（120），展开单元（130）和注射单元（140）。机翼基于身体对称安装。展开单元安装在机翼的底部。当膨胀空气注入到展开单元中时，展开单元被膨胀以形成基部环形的横截面，以便向下展开。注射单元安装在机翼的底部。注射单元在由展开单元限制的区域中朝向面向水面的方向注入空气。

8. 发明授权

KR100914634B1 복합 해양온실목장 失效
标题翻译：使用温室效应的复合海洋过滤
公开(公告)号：KR100914634B1
公开(公告)日：2009-09-02
申请号：KR1020090008119
申请日：2009-02-02
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이한진 , 이창민 , 박진형 , 강국진
IPC分类号： A01K61/00
CPC分类号： Y02A40/81 , Y02P60/64
摘要： A complex marine greenhouse stock farm is provided, which enables to perform consumption of carbon dioxide which is generated in the industrial complex. A complex marine greenhouse stock farm comprises: a marine greenhouse which is installed at the sea and enables to cultivate the agricultural product using the solar energy; an electric power generator(300) which produces the electricity which is used in the marine greenhouse using the multiple energy source of the nature; a fresh water device which produces the fresh water used in the marine greenhouse by using the solar energy; and a marine farm which is used as the stock farm by installing an artificial fish reef at the lower part of the marine greenhouse.
摘要翻译：提供了一个复杂的海洋温室库存农场，可以实现在工业综合体中产生的二氧化碳的消耗。复杂的海洋温室养殖场包括：海洋温室，安装在海上，能够利用太阳能培养农产品; 产生用于海洋温室中的使用多种能量源的电力的发电机（300）; 一种淡水装置，通过使用太阳能产生用于海洋温室的淡水; 以及在海洋温室下部安装人造鱼礁，用作养殖场的海洋农场。

9. 发明授权

KR100910552B1 위그선 날개 구조 失效
标题翻译： WIG SHIPCRAFT的WING结构
公开(公告)号：KR100910552B1
公开(公告)日：2009-08-03
申请号：KR1020080081188
申请日：2008-08-20
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이한진 , 이창민
IPC分类号： B63B1/16
CPC分类号： B60V1/08 , B60V3/06 , B64C23/076 , Y02T50/164
摘要： A wig ship wing structure is provided to compensate for thrust asymmetry of the right end and the left end generated in moving according to the control applied from a driver of a wig ship hull. A wig ship wing structure comprises a main wing(200), a downward wing, a horizontal tail wing(400), and a vertical tail wing. The main wing is protruded from the side center of a wing ship hull(100). The downward wing is fixed to the external end of the main wing. The horizontal tail wing is horizontally protruded from the stern of the wig ship hull to the outside. The vertical tail wing is vertically formed in a hull axial direction. The front side of the downward wing has a round shape having proper thickness to prevent flow exfoliation.
摘要翻译：提供假发船翼结构以根据从假发船体的驾驶员施加的控制来补偿移动中产生的右端和左端的推力不对称性。假发船翼结构包括主翼（200），向下翼，水平尾翼（400）和垂直尾翼。主翼从翼船船体的侧面中心突出（100）。向下的翼固定到主翼的外端。水平尾翼从假发船体的船尾水平突出到外面。垂直尾翼在船体轴向垂直形成。向下翼的前侧具有适当厚度的圆形以防止流动剥落。

10. 发明授权

KR100910551B1 수평꼬리날개가 없는 위그선 失效
标题翻译： WIG SHIPCRAFT没有水平的尾巴
公开(公告)号：KR100910551B1
公开(公告)日：2009-08-03
申请号：KR1020080081184
申请日：2008-08-20
申请人： 윙쉽테크놀러지 주식회사
发明人： 강창구 , 이한진 , 이창민
IPC分类号： B63B1/16 , B63B1/18
CPC分类号： B64C35/003 , B64C5/08 , B64C23/076 , B64C39/12 , Y02T50/164
摘要： A wig ship without a horizontal tail wing is provided to solve the problem of horizontal tail wing design due to ground effect by forming a canard wing in instead of the horizontal tail wing to obtain pitching stability. A wig ship without a horizontal tail wing comprises a main wing(200), and the downward wing(300) and a canard wing(600). The main wing is protruded from the side center of the wig ship hull(100). The downward wing is fixed to the external end of the main wing. The downward wing is downwardly directed without a joint. The canard wing is protruded from the main wing to the outside of the front end of the hull as a progressing forward of the wig ship. The downward wing comprises a downward panel and a rudder. The downward pane is integrally fixed to the end of the main wing. The rudder is installed to be faced to the rear side of the downward panel.
摘要翻译：提供没有水平尾翼的假发船，通过形成一个鸭翼而不是水平尾翼来解决由于地面效应而导致的水平尾翼设计的问题，以获得俯仰稳定性。没有水平尾翼的假发船包括主翼（200）和向下翼（300）和鸭翼（600）。主翼从假发船体的侧面中心突出（100）。向下的翼固定到主翼的外端。向下的翼向下指向没有关节。随着假发船的前进，鸭翼从主翼突出到船体前端的外侧。向下的翼包括向下的面板和方向舵。向下的窗格一体地固定在主翼的末端。方向舵安装在面向后面板的后侧。

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