| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | 凧地上ステーション及びそれを使用するシステム | JP2014547561 | 2012-12-18 | JP2015507569A | 2015-03-12 | ヴァンダー・リンド、デーモン |
| 空中発電に適した地上ステーションを有する凧システムである。凧システムは、タービン駆動発電機をその上に取り付けた1以上の風圧板を具備する凧を含むことができる。このタービン駆動発電機は、揚げる時に用いることができ、垂直に離着陸する特徴を有することができる、動力飛行モードでのモーター駆動プロペラとしての機能も有することができる。離着陸を容易にするように作られた支持台をシステムの一部として用いることができる。この支持台は、つなぎ綱の引っ張る方向に向けて旋回軸の周りに動くよう旋回することができる。【選択図】図1 | ||||||
| 22 | Launching / recovery mechanism and aerodynamic profile element for the aerodynamic profile element | JP2009524080 | 2006-08-15 | JP2010500221A | 2010-01-07 | シュテファン・ヴラゲ; シュテファン・ブラベック |
| ウォータークラフトを駆動するために引っ張り力によってエネルギーを生成する空気力学的プロファイル要素は、上側可撓層、上側層と平行で複数のウェブで上側層へ接続される下側可撓層、上側及び下側層間の内部空間、上側及び下側層の前縁間の空気取入開口、及びウォータークラフトへと接続するための複数の縮帆線を備える。 縮帆線は、第１の端部がプロファイル要素上の離間した位置に固定され、第２の端部が引張ケーブルに接続されている複数の引張線へ接続され、上側及び下側層の縮帆又は伸帆でプロファイル要素のサイズを増減させる。 空気力学的プロファイルの安定のために長手方向に延び棒部材によって発展させられる。 縮帆線の少なくとも１つが棒部材において、第１の端部の固定点からプロファイル要素の横方向に延びる縮帆線部分から、長手方向に延びる縮帆線部分へ向きを変える。 | ||||||
| 23 | 비행연 | KR2020140005382 | 2014-07-17 | KR2020160000306U | 2016-01-27 | 조용균 |
| 동체에전방후방으로날개를부착하고전방날개와후방날개끝 부분에좌우수평안정을도와주는도움수직날개를날개끝 부분에좌우로한개씩부착하므로서비행연의좌우수평안정향상시켯서며전후방날개면뒤측에보조날개도움날개설치하여보조날개는좌우기울기를조절하며도움날개는연이올르고내리는것을도와주며비행연동체뒤에설치된 V형터널수직날개둘은비행연이공중어떠 있을때 바람이부는방향으로향하도록하였다또 공중에떠 있을때 후크끈을이탈시켜공중에서글라이드비행도가능하도록되어있서보조날개, 도움날개, 수직방향타, 후크끈은모두무선조정으로조종하도록한 것이다. | ||||||
| 24 | 풍등(風燈) | KR1020080113241 | 2008-11-14 | KR100884615B1 | 2009-02-23 | 하종률 |
| A wind lamp float is provided to prevent an accident due to fallout by suppressing a fire due to an ignition material and collecting residues of kindling coal separated from the ignition material. A cover unit(10) is made of a paper material. An accommodating groove is formed in the inside of the cover unit. A lower part of the cover unit is opened. A lower supporting plate(21) is formed to surround a circumference of the open lower part of the cover unit. A supporting part(20) is connected to the lower supporting plate in a cross shape and is composed of a cross supporting plate(22) for maintaining the shape of the lower supporting plate. An ignition unit(30) is installed at a center of the cross supporting plate. The ignition unit includes an ignition material and a connective ring. The ignition material is formed by coating a paraffin on a non-flammable material. One end of the connective ring is coupled with a lower part of the ignition material. The other end of the connective ring is connected to a center of the cross supporting plate. | ||||||
| 25 | 애드벌룬 가설물장치보조선 | KR1020060073544 | 2006-08-04 | KR1020080012563A | 2008-02-12 | 김석 |
| An auxiliary line for various temporary installations at an inner center of an advertising balloon is provided to prevent the damage of the advertising balloon by restricting the movement of temporary installations inside the advertising balloon. An auxiliary line for various temporary installations at an inner center of an advertising balloon includes a fixing unit(1), a connecting loop(2), and an auxiliary line(3). The fixing unit is made of the same material as a surface of the advertising balloon. The auxiliary line fixes a position of temporary installation. The position of the temporary installation is fixed at a center of the advertising balloon when injecting helium gas or air into the advertising balloon. When a light bulb is installed in the advertising balloon, heat generated in the light bulb is diffused to protect the advertising balloon. | ||||||
| 26 | 비행 풍력 터빈 정류용 피봇팅 정착대 | KR1020177025993 | 2016-02-26 | KR1020170128322A | 2017-11-22 | 해치트만,브라이언; 반더린드,다몬; 에버스,마이커; 시모니안,마이클 |
| 동체를가지는공중운반체, 공중운반체에고정된제1 단부및 공중운반체가내부로릴 작업될때 테더가둘러싸는탑에위치되는회전가능한드럼에고정된제2 단부를가지는전기전도성테더, 탑으로부터연장되는정착대, 정착대패널에부착되고탑에피봇가능하게장착된하나이상의정착대붐을포함하는공중풍력터빈시스템이제공되고, 공중운반체가정착대에고정될때, 공중운반체는하강된정류위치에배치될수 있고, 공중운반체는탑에대한하나이상의정착대붐의회전에의해서유발된상승된정류위치로이동될수 있다. | ||||||
| 27 | 연 지상 스테이션과 이를 이용하는 시스템 | KR1020167008736 | 2012-12-18 | KR101773312B1 | 2017-08-31 | 밴더린드데이먼 |
| 공중발전(airborne power generation)을위하여구성된지상스테이션을갖는연 시스템. 연시스템은복수의터빈구동발전기를그 위에탑재하는하나이상의에어포일을구비하는연을포함할수 있다. 터빈구동발전기는또한수직이륙및 착륙양태를포함할수 있는이륙을하는동안에사용되는동력비행모드에서모터구동프로펠러로서기능할수 있다. 이륙및 착륙이용이하도록구성된퍼치(perch)는시스템의일부로서사용될수 있다. 퍼치는피벗(pivot)이테더(tether)의장력방향을향하도록회전할수 있다. | ||||||
| 28 | 비행체를 위한 경로 기반 전력 발생 제어 | KR1020167019502 | 2014-10-20 | KR101737751B1 | 2017-05-18 | 젠센,케네쓰; 벤더린드,데몬 |
| 본명세서에기술된방법들및 시스템들은비행체를위한전력발생제어와관련된다. 예시적방법은전력을발생하기위해비행체를실질적으로제1 비행경로를따라측풍-비행방향에서작동시키는단계를포함할수 있다. 제1 비행경로는비행체가전력을발생하게하는실질적인원형경로를포함할수 있다. 비행체가측풍-비행방향에있는동안, 방법은비행체에의해발생되고있는전력을감소시키도록결정하는단계, 및이 결정에응답하여제2 비행경로를결정하는단계를포함할수 있고, 제2 비행경로는제2 비행경로에서작동할때 비행체에의해발생되는전력을감소시킬것이다. 결정될때, 비행체는실질적으로제2 비행경로를따라작동할수 있다. | ||||||
| 29 | 비행체를 위한 경로 기반 전력 발생 제어 | KR1020167019502 | 2014-10-20 | KR1020160090398A | 2016-07-29 | 젠센,케네쓰; 벤더린드,데몬 |
| 본명세서에기술된방법들및 시스템들은비행체를위한전력발생제어와관련된다. 예시적방법은전력을발생하기위해비행체를실질적으로제1 비행경로를따라측풍-비행방향에서작동시키는단계를포함할수 있다. 제1 비행경로는비행체가전력을발생하게하는실질적인원형경로를포함할수 있다. 비행체가측풍-비행방향에있는동안, 방법은비행체에의해발생되고있는전력을감소시키도록결정하는단계, 및이 결정에응답하여제2 비행경로를결정하는단계를포함할수 있고, 제2 비행경로는제2 비행경로에서작동할때 비행체에의해발생되는전력을감소시킬것이다. 결정될때, 비행체는실질적으로제2 비행경로를따라작동할수 있다. | ||||||
| 30 | 연 지상 스테이션과 이를 이용하는 시스템 | KR1020147020298 | 2012-12-18 | KR101611779B1 | 2016-04-11 | 밴더린드데이먼 |
| 공중발전(airborne power generation)을위하여구성된지상스테이션을갖는연 시스템. 연시스템은복수의터빈구동발전기를그 위에탑재하는하나이상의에어포일을구비하는연을포함할수 있다. 터빈구동발전기는또한수직이륙및 착륙양태를포함할수 있는이륙을하는동안에사용되는동력비행모드에서모터구동프로펠러로서기능할수 있다. 이륙및 착륙이용이하도록구성된퍼치(perch)는시스템의일부로서사용될수 있다. 퍼치는피벗(pivot)이테더(tether)의장력방향을향하도록회전할수 있다. | ||||||
| 31 | 연기구를 사용한 감시카메라 및 원격제어기 설치 방법 | KR1020130040365 | 2013-04-12 | KR1020140123272A | 2014-10-22 | 이만규 |
| The present invention relates to an application field for a design of a device for controlling buoyancy and wind power which enable a camera and a remote control device using a kite balloon to float to a desired position. The present invention can reduce the weight of a device and operate a high capacity device by maintaining a stable support structure for controlling the direction of the camera or the like and providing a method for correcting and controlling a position by using the kite balloon minimizing the influence on change in wind and an upper-air movement and position obtaining technique using the kite balloon and a traction line. | ||||||
| 32 | 풍등 | KR1020090042324 | 2009-05-15 | KR1020100123225A | 2010-11-24 | 조대성 |
| PURPOSE: A manner attach to the ignition material to the combustion member. The separate firing tool unnecessaries. CONSTITUTION: The balloon-like outer cover(10) has the opening on bottom. The supporting board(12) is attached to opening. The support stand(13) is composed of the wire in which both ends is fixed to bracket more than 2. The ignition material(17) is attached to the combustion member(14). The combustion member is lit. | ||||||
| 33 | HARDPOINT STRAIN RELIEFS | EP16730605.9 | 2016-06-02 | EP3303128A1 | 2018-04-11 | CADMAN, Gregor, Boone; VANDER LIND, Damon |
| A hardpoint relief pad is described and includes a base surface, a hardpoint overlay, and a first stress relief area. The base surface is configured to conform to and be fixedly attached to an interior surface of an aerial vehicle wing. The hardpoint overlay protrudes above adjacent areas of the hardpoint relief pad and is adapted to conform to a hardpoint. The hardpoint protrudes from the interior surface of the wing and is configured to carry a load fixed to the hardpoint. The hardpoint overlay includes an oculus that is configured to allow the load to be fixed to the hardpoint through the hardpoint overlay. The first stress relief area protrudes above adjacent areas of the hardpoint relief pad and also forms a hollow cavity between the first stress relief area and the interior surface of the wing. | ||||||
| 34 | METHOD AND DEVICE FOR GENERATING ELECTRICAL ENERGY BY MEANS OF A TETHERED FLYING OBJECT | EP14758112.8 | 2014-08-26 | EP3041738B1 | 2018-03-21 | LUCHSINGER, Rolf; GOHL, Flavio |
| The method according to the invention for controlling a flying object (2, 20) having a stiff airfoil ( 21 ) and being controllable by means of a roll movement for carrying out lateral turns, with which the flying object (2, 20) is connected to a ground station (5) by means of at least two tethers (3, 4), such that the flying object ( 2, 20) rolls during flight by means of a differential movement of the tethers (3, 4), and that the flying object (2, 20) is rolled during flight by means of such differential movements and is th us manoeuvred by means of the turning flight that is caused in this way. Said flying object (2, 20) can be operated by means of the controlling reel out speed and reel in speed with an average power maximised over a flight cycle consisting of a power phase and a depower phase. | ||||||
| 35 | PATH BASED POWER GENERATION CONTROL FOR AN AERIAL VEHICLE | EP14872510 | 2014-10-20 | EP3083400A4 | 2017-11-01 | JENSEN KENNETH; VANDER LIND DAMON |
| Methods and systems described herein relate to power generation control for an aerial vehicle. An example method may include operating an aerial vehicle in a crosswind-flight orientation substantially along a first flight path to generate power. The first flight path may include a substantially circular path that allows the aerial vehicle to generate the power. While the aerial vehicle is in the crosswind-flight orientation the method may include determining to reduce the power being generated by the aerial vehicle, and responsive to the determination, determining a second flight path that will reduce the power generated by the aerial vehicle when operating on the second flight path. Once determined, the aerial vehicle may operate substantially along the second flight path. | ||||||
| 36 | SAIL FOR A KITE, KITE AND METHOD FOR MANUFACTURING SAID SAIL | EP16163527.1 | 2016-04-01 | EP3225545A1 | 2017-10-04 | Stiewe, Peter |
The invention is related to a sail (1) for a kite comprising a canopy (2) having a leading edge (3) and a trailing edge (4); a front chamber (6) extending along said leading edge (3); and an inflatable hose (7) disposed in said front chamber (6), wherein said hose (7) being inflated with a compressed fluid, preferably compressed air or compressed gas, so that said hose (7) in said front chamber (6) is forming a front tube (5) of said sail (1), wherein in said inflated state of said hose (7), said hose (7) being dimensionally stable for bringing said sail (1) in a negative dihedral form independent on a load condition of said sail (1) and wherein said hose (7) comprises a predefined curvature in its longitudinal alignment prior its disposal in said front chamber (6). The invention is further related to a kite (K) that uses the above-mentioned sail (1) and methods for manufacturing such sails (1).
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| 37 | DISPOSITIF AEROPORTE | EP15759845.9 | 2015-07-15 | EP3172435A1 | 2017-05-31 | LOZANO, Rogelio |
| The invention concerns an airborne device (10) comprising at least three supporting wings (12) and a linking device (18), the wings being linked to each other by first flexible cables (16), each wing being further linked to the linking device (18) by a second flexible cable (20), the linking device being linked to a third flexible cable (22) intended to be linked to a base (46, 48), the first, second and third cables being tensioned when the airborne device is carried in the wind. | ||||||
| 38 | GEFESSELTES FLÜGELSYSTEM ZUR WINDENERGIENUTZUNG | EP13773600.5 | 2013-09-16 | EP2895740B1 | 2016-11-16 | BORMANN, Alexander; SKUTNIK, Stefan; GEBHARDT, Christian; RANNEBERG, Maximilian |
| 39 | METHOD AND DEVICE FOR GENERATING ELECTRICAL ENERGY BY MEANS OF A TETHERED FLYING OBJECT | EP14758112.8 | 2014-08-26 | EP3041738A1 | 2016-07-13 | LUCHSINGER, Rolf; GOHL, Flavio |
| The method according to the invention for controlling a flying object (2, 20) having a stiff airfoil ( 21 ) and being controllable by means of a roll movement for carrying out lateral turns, with which the flying object (2, 20) is connected to a ground station (5) by means of at least two tethers (3, 4), such that the flying object ( 2, 20) rolls during flight by means of a differential movement of the tethers (3, 4), and that the flying object (2, 20) is rolled during flight by means of such differential movements and is th us manoeuvred by means of the turning flight that is caused in this way. Said flying object (2, 20) can be operated by means of the controlling reel out speed and reel in speed with an average power maximised over a flight cycle consisting of a power phase and a depower phase. | ||||||
| 40 | DISPOSITIF DE MAINTIEN EN ALTITUDE D'UNE CHARGE UTILE DONT LA SOURCE D'ENERGIE DE MAINTIEN EN ALTITUDE EST PERMANENTE ET EXTRAITE DU MILIEU | EP08860994.6 | 2008-12-15 | EP2222555B1 | 2015-02-18 | SAINCT, Hervé; RENAULT, Hervé |
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