子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 一种无人机拍摄器方向调整方法及智能穿戴设备 | CN201610373169.0 | 2016-05-31 | CN106054871A | 2016-10-26 | 刘均; 刘新; 宋朝忠; 欧阳张鹏 |
| 本发明实施例提供了一种无人机拍摄器方向调整方法及智能穿戴设备，其中，方法包括：通过三轴加速度传感器获取当前智能穿戴设备在三维坐标轴上的加速度参数；根据所述三维坐标轴上的加速度参数，确定方向调整参数；向与所述智能穿戴设备关联的无人机发送所述方向调整参数，以使所述无人机根据所述方向调整参数调整拍摄器的拍摄方向。采用本发明，可以更方便的对无人机拍摄器方向进行调整，从而提高对无人机操控的便捷度。 | ||||||
| 2 | 低空太阳能飞行器 | CN201610667675.0 | 2016-08-08 | CN106275428A | 2017-01-04 | 李玉强 |
| 一种座椅式低空太阳能飞行器，座椅有左翼阵列电风机群和右翼阵列电风机群及底部阵列电风机群，椅后有慢速推进电风机和左右转向电风机及警示红灯，驾驶员头顶上有光伏太阳能电池毯，椅下有蓄电池，光电进入蓄电池后再向电机供电，用不完的电储存夜间用，有电量表指南针高度时速表，有脚操作杆手操作柄，可升降前进左右转向悬停和慢速向前，有垃圾袋食品袋防风罩护腿罩，手机托架耳塞及望远镜托架和收音交通广播，座椅四个脚有缓冲撑簧和万向轮，驾驶员头顶上的光伏太阳能电池毯能当降落伞，有安全带，所有屋顶可降落或折叠放于家中阳台或阳台上起飞降落。 | ||||||
| 3 | 一种基于无人机的大气污染监测系统及监测方法 | CN201610765565.8 | 2016-08-29 | CN106210662A | 2016-12-07 | 台海江 |
| 本发明提供了一种基于无人机的大气污染监测系统及监测方法，包括无人机本体和地面站；无人机本体上设有数据采集控制单元，数据采集控制单元的输入端分别与气体检测模块、GPS导航模块、温湿度传感器和机载电源相连，数据采集控制单元的输出端分别与机载图传电台、SD存储卡和数据导出接口相连，数据采集控制单元分别与CCD光学相机和机载数传电台双向传输数据。地面站设有工控机，工控机分别与数传电台、显示器和存储单元双向传输数据，工控机的输入端与图传电台相连，电源向工控机、图传电台和数传电台供电。本大气污染监测系统采用无人机进行现场监测，可使检测人员远离污染，提高监测效率，保证监测数据准确、快捷。 | ||||||
| 4 | 多轴载人飞行器 | CN201510520687.6 | 2015-08-21 | CN105151296A | 2015-12-16 | 陶亮; 申守健; 秦立新 |
| 本申请公开了一种多轴载人飞行器，包括机架和安装于机架上的动力装置、传动装置、旋翼装置、变距装置、座椅和控制装置，其中，所述传动装置，连接所述动力装置与所述旋翼装置；所述旋翼装置，包括旋翼头和螺旋桨，所述旋翼头对称安装于所述机架上，所述螺旋桨安装于所述旋翼头上，所述旋翼头和螺旋桨的数量至少为三组；所述变距装置，所述变距装置与所述旋翼装置相连接；所述座椅和操作装置对应设置于所述机架结构的中部，所述动力装置与所述旋翼装置连接；所述控制装置，分别与所述动力装置、所述旋翼装置和所述操作装置连接；飞行的过程中操作更加简便，面对各种飞行状态时能够轻松的应对，结构简单但实现的功能全面。 | ||||||
| 5 | Airborne photovoltaic solar device and method | US14533280 | 2014-11-05 | US09246433B2 | 2016-01-26 | Leonid Goldstein |
| An airborne photovoltaic solar system, comprising a parabolic reflector-concentrator (110, 1210), spread by wind, a solar panel (102, 1202) raised to high altitude using at least one lighter than air balloon (103, 1201), tracking the sun using aerodynamic surfaces and/or changes in buoyancy, relying on wind and/or cold air to cool the solar panel in one embodiment, as well as related methods and variations and alternatives. | ||||||
| 6 | Skyboard | US261697 | 1988-10-24 | US4898345A | 1990-02-06 | Dan Clayton |
| A skyboard which is an apparatus using the combination of a specially designed surfboard and a parachute to enable the rider to ride the skyboard in a manner similar to the rider's positioning on a surfboard and which will enable the rider to ride the air currents of the sky in a much more exciting manner than through conventional gliders or hand gliders. The skyboard is a lightweight object formed in the general shape of a surfboard and which is modified to include at least a pair of front wings and a pair of rear wings on its lateral sides, a pair of fins on its underside and a pair of foot or shoe binders on its upper surface to accommodate and hold the rider's feet or shoes. The skyboard can be used as an air current surfing board to enable a rider to stand on the object and maneuver it with his feet in a manner similar to the maneuvering of a surfboard to cause the fins on the underside of the skyboard to catch and channel the air flow and give it and the rider lift, and to permit the pair of front side wings and rear side wings to give the skyboard stability and lift as it glides over the air currents. | ||||||
| 7 | Solar powered aircraft | US263829 | 1981-05-15 | US4415133A | 1983-11-15 | William H. Phillips |
| A cruciform wing structure for a solar powered aircraft is disclosed. Solar cells 28 are mounted on horizontal wing surfaces 20, 22. Wing surfaces 24, 26 with spanwise axis perpendicular to surfaces 20, 22 maintain these surfaces normal to the sun's rays by allowing aircraft to be flown in a controlled pattern at a large bank angle.The solar airplane may be of conventional design with respect to fuselage, propeller and tail, or may be constructed around a core 70 and driven by propeller mechanisms 75, 76, 77, and 78 attached near the tips of the airfoils. | ||||||
| 8 | Ultralight aircraft | US15041424 | 2016-02-11 | US10093427B2 | 2018-10-09 | Simon Burns |
| An aircraft which has a supporting structure which has at least one fuselage, a wing structure and at least one drive apparatus. The drive apparatus has at least one propeller and a drive motor. The aircraft has at least one energy store for providing energy for operation of the drive apparatus. The at least one drive apparatus and the at least one energy store are mechanically connected to the supporting structure and/or the wing structure of the aircraft by a securing device. | ||||||
| 9 | Phugoid peaks trajectory for hypersonic glide vehicles | US14818559 | 2015-08-05 | US09639085B1 | 2017-05-02 | Barry M. Hellman |
| A new apparatus and method for determining trajectories for hypersonic glide vehicles significantly reduces integrated, or total, heat load, with little reduction in time to distance and maximum range. The new approach identifies a trajectory having large phugoid oscillations and plotting a glide trajectory along the peaks of the phugoid oscillations. The glide trajectory is determined by calculating a first altitude that results in a maximum lift to drag ratio trajectory having damped or small phugoid oscillations, then calculating a different altitude that results in larger phugoid oscillations, and higher phugoid peaks, and finally plotting a trajectory from the first altitude that follows the peaks of the higher phugoid oscillation trajectory. The thus calculated trajectory can be input into a glide vehicle guidance system for controlling the trajectory of the glide vehicle from a point where it reaches the first altitude. | ||||||
| 10 | AIRBORNE PHOTOVOLTAIC SOLAR DEVICE AND METHOD | US14533280 | 2014-11-05 | US20150053255A1 | 2015-02-26 | Leonid Goldstein |
| An airborne photovoltaic solar system, comprising a parabolic reflector-concentrator (110, 1210), spread by wind, a solar panel (102, 1202) raised to high altitude using at least one lighter than air balloon (103, 1201), tracking the sun using aerodynamic surfaces and/or changes in buoyancy, relying on wind and/or cold air to cool the solar panel in one embodiment, as well as related methods and variations and alternatives. | ||||||
| 11 | Aircraft system monitoring air humidity to locate updrafts | US985940 | 1997-12-05 | US6012675A | 2000-01-11 | Jan Henri Cocatre-Zilgien |
| An aircraft system intended for gliders and low power-to-weight aircraft, to aid the pilot in locating updrafts associated with the buoyancy of humid air in the convective layer of the atmosphere, namely moist thermals. The system comprises a pair of laterally spaced hygrometers, generally at the wingtips. Four types of hygrometer units are described; resistive, piezoelectric, spectrometric, and capacitive. Humidity data is transmitted to the cockpit by telemetry links, of which four types are also described; by dedicated wiring, by carrier current using wingtip position lights wiring, by modulated infrared beams, and by low-power radio waves. The system monitors the difference of humidity between left and right sensors, and also the rate of change of humidity of one or both sensors as a function of time. This lateral and eventually axial differential humidity information is presented to the pilot via a visual interface such as bargraph displays and computer monitors, or via an audio interface producing sounds of variable pitch or beat in one or more cockpit loudspeakers, or via both interfaces simultaneously. For humidity measurements inherently sensitive to temperature, such as relative humidity, either the hygrometers are heated, or their temperature is also measured so that temperature effects can be subsequently removed by computation. This system enables the pilot to get a better understanding of the thermodynamics of the convective layer of the atmosphere. | ||||||
| 12 | WINGS FOR FLYING OBJECTS (VARIANTS) | US16342541 | 2017-10-12 | US20190241249A1 | 2019-08-08 | Gevorg Serezhaevich NOROYAN |
| The group of inventions relates to the field of aircraft. In each variant, a flying object (FO) comprises a body and wings. In a first variant, an FO comprises wings mounted so as to be capable of rotating the FO. In a second variant, an FO comprises a body on which is mounted a rim with side wings. In a third variant, an FO comprises wings in the shape of a triangular prism, one side of which is fastened to the body, and the other two sides of which are spherical with arcs of different radii. In a fourth variant, the FO comprises tail wings fastened to the body such that the exhaust gases from the nozzle impinge on the wings and create a force which rotates the FO. | ||||||
| 13 | ULTRALIGHT AIRCRAFT | US15041424 | 2016-02-11 | US20160236789A1 | 2016-08-18 | Simon BURNS |
| An aircraft which has a supporting structure which has at least one fuselage, a wing structure and at least one drive apparatus. The drive apparatus has at least one propeller and a drive motor. The aircraft has at least one energy store for providing energy for operation of the drive apparatus. The at least one drive apparatus and the at least one energy store are mechanically connected to the supporting structure and/or the wing structure of the aircraft by a securing device. | ||||||
| 14 | Aircraft Lift And Propulsion From Disparate Air Flows | US14116853 | 2012-05-18 | US20140097301A1 | 2014-04-10 | Henry C. DeBey |
| Generally, an inventive aircraft (1) having at least a first lift body (2) and a second lift body (3) each controllably configurable to correspondingly generate an amount of lift (4) sufficient to remain aloft at a first elevation (5) and a second elevation (6) a sufficient distance apart (7) to subject the first lift body (2) and the second lift body (3) to sufficiently disparate fluid flow characteristics (8) to propel the aircraft (1). | ||||||
| 15 | Passive-restraint prone cockpit | US09520512 | 2000-03-08 | US06315244B1 | 2001-11-13 | Julius Theodore Cage, III |
| This invention features a prone pilot's couch conformable to the front of the pilot's body, relieving his arms of the need to support the body; twist- and pull-handgrips placed to the sides of the pilot's body for convenient control-surface actuation; a helmet brace for positive-g flight maneuvers; passive shoulder braces which confine the chest to the pilot's couch in all flight attitudes, when forward exertion is applied by the legs; and channels conforming to three sides of the pilot's legs, having a lip or shelf which protrudes outward from a bracing area between the pilot's legs, for support during inverted flight maneuvers, forward exertion being applied by the legs. | ||||||
| 16 | Vertical take-off and landing aircraft | US09334696 | 1999-06-16 | US06293491B1 | 2001-09-25 | Aloys Wobben |
| The invention concerns a vertical take-off and landing aircraft (10) with a plurality of lift (26a-26p) and thrust rotors (20a,20b), in which all rotors have their own electric motor (48a-48p,50a,50b) as a drive. | ||||||
| 17 | Method and apparatus for use in harnessing solar energy to provide initial acceleration and propulsion of devices | US121493 | 1980-02-14 | US4403755A | 1983-09-13 | Gunter E. Gutsche |
| The present invention relates to a method of providing thrust and added lift to a vehicle by accelerating fluid heated by solar energy. The present invention also relates to apparatus for carrying out the aforementioned method. Accordingly, the present invention relates to a method of providing initial acceleration and propulsion or enhancing the initial acceleration and propulsion of a vehicle in an environment having at least some fluid, the vehicle being of the type having at least one member, at least a portion of which is treated for absorbing solar radiation for heating fluid adjacent the member for use in propelling the vehicle through the environment. By use of direct and/or focused solar radiation, fluid is heated, accelerated and deflected away from a vehicle by natural or forced convection to provide thrust and lift of the vehicle. | ||||||
| 18 | Ultraleichtflugzeug | EP15000418.2 | 2015-02-12 | EP3056426A1 | 2016-08-17 | Burns, Simon |
Es wird ein Fluggerät angegeben, das eine Tragestruktur aufweist, die mindestens einen Rumpf, eine Flügelstruktur und wenigstens eine Antriebsvorrichtung aufweist. Die Antriebsvorrichtung weist mindestens einen Propeller und einen Antriebsmotor auf. Das Fluggerät weist mindestens einen Energiespeicher zum Bereitstellen von Energie für den Betrieb der Antriebsvorrichtung auf. Die mindestens eine Antriebsvorrichtung und der mindestens eine Energiespeichersind mittels einer Sicherungseinrichtung mechanisch mit der Tragestruktur und/oder der Flügelstruktur des Fluggeräts verbunden.
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| 19 | Dispositif de stabilité répondant aux réflexes humains dans l'air | EP90401696.1 | 1990-06-15 | EP0463262A1 | 1992-01-02 | Jault, Pascal |
Dispositif de stabilité répondant aux réflexes humains dans l'air, il est du type transmetteur de mouvement pour angles, un dispositif d'attache des pieds sur les tiges principales, permettent à l'homme par l'action de ses forces exercées de se diriger dans l'air. |
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| 20 | ARICRAFT LIFT AND PROPULSION FROM DISPARATE AIR FLOWS | PCT/US2012038638 | 2012-05-18 | WO2012159056A3 | 2013-01-31 | DEBEY HENRY C |
| Generally, an inventive aircraft (1) having at least a first lift body (2) and a second lift body (3) each controllably configurable to correspondingly generate an amount of lift (4) sufficient to remain aloft at a first elevation (5) and a second elevation (6) a sufficient distance apart (7) to subject the first lift body (2) and the second lift body (3) to sufficiently disparate fluid flow characteristics (8) to propel the aircraft (1). | ||||||
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