| 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 | 带有柔性机翼的飞行器的自动起飞方法、帆和飞行器 | CN200980153185.7 | 2009-10-28 | CN102272003A | 2011-12-07 | B.贝尔捷 |
| 本发明涉及一种带有柔性机翼的飞行器的自动起飞的方法，其中所述飞行器包括由吊件悬挂在帆上的小车。根据该方法：为所述小车装备自动驾驶仪，该自动驾驶仪控制作用于所述吊件的致动器；为所述帆装备机翼高度传感器，该机翼高度传感器包括双轴加速度计和双轴陀螺测试仪，以及用于与所述自动驾驶仪通信的装置，其中所述陀螺测试仪能够确定帆参考系相对于地面的位置；当起飞时，收集来自于所述机翼高度传感器的信息，以将其传输给自动驾驶仪，以向所述致动器发出指令。本发明还涉及一种实施该方法的帆，其包括带有惯性仪的机翼高度传感器，该惯性仪带有双轴加速度计和双轴陀螺测试仪，以及用于与自动驾驶仪通信的装置。本发明还涉及一种包括这种帆的飞行器。 | ||||||
| 2 | 机翼型伞盖式飞机 | CN92108825.6 | 1992-06-30 | CN1073146A | 1993-06-16 | 史蒂芬·L·斯奈德 |
| 一种无线电控制的飞机，包括一个由电机(36)带动推进器(38)提供动力的机体(1)，在飞行中机体通过可转动地安装在飞机机身上的操纵控制杆(68)而被悬挂，操纵控制杆有连接于负载悬挂吊索(3，5，6)的下端的外端(12，14)，负载悬挂吊索的上端与冲压空气充气式的柔性机翼型伞盖部分(2)相连。飞机的操纵是通过控制杆(68)的转动调节负载悬挂吊索并由此调节伞盖表面。在机身内装有一个无线电接收机(112)，用来控制驱动电机(36)速度。飞机由一个控制飞机的转向和速度的摇控发射机控制。 | ||||||
| 3 | 一种冲压翼伞开伞控制装置 | CN201610753631.X | 2016-08-29 | CN106114855A | 2016-11-16 | 李轲 |
| 本发明涉及冲压翼伞技术领域，特指一种冲压翼伞开伞控制装置，本发明采用在冲压翼伞加工之初，在冲压翼伞上、下翼肋缝合位置增加连接扣圆环，使用连接绳一一穿过圆环，在连接绳上加装延时切割器，在冲压翼伞开伞的过程中，延时切割器保险解除，切断连接翼肋上端圆环的连接绳，冲压翼伞气室束缚被解除，冲压翼伞充气张满，该装置实施比较简单，可以满足不同形状冲压翼伞开伞的需要，通用性强。 | ||||||
| 4 | 一种飞行模态可转换的无人机 | CN201510840392.7 | 2015-11-27 | CN105366037A | 2016-03-02 | 向敏; 石宋华; 游城; 金薇 |
| 本发明涉及无人机飞机制造技术领域，具体涉及一种飞行模态可转换的无人机，尤其涉及一种飞行模态可转换的无人机，系统组成包括：飞行控制计算机、开切伞系统、高度传感器、发动机组、发动机控制装置、滑翔伞、左动力发动机、右动力发动机、飞行控制计算机、发动机控制装置和开切伞系统，所述飞行控制计算机、开切伞系统、高度传感器、发动机组和发动机控制装置信号相连，所述滑翔伞、左动力发动机、右动力发动机、飞行控制计算机、发动机控制装置和开切伞系统机械相连。 | ||||||
| 5 | 翼型伞盖飞机 | CN92108825.6 | 1992-06-30 | CN1030978C | 1996-02-14 | 史蒂芬·L·斯奈德 |
| 一种无线电控制的飞机，包括一个由电机(36)带动推进器(38)提供动力的机体(1)，在飞行中机体通过可转动地安装在飞机机身上的操纵控制杆(68)而被悬挂，操纵控制杆有连接于负载悬挂吊索(3，5，6)的下端的外端(12，14)，负载悬挂吊索的上端与冲压空气充气式的柔性翼形伞盖部分(2)相连。飞机的操纵是通过控制杆(68)的转动调节负载悬挂吊索并由此调节伞盖表面。在机身内装有一个无线电接收机(112)，用来控制驱动电机(36)速度。飞机由一个控制飞机的转向和速度的遥控发射机控制。 | ||||||
| 6 | Eahoirugatauingu | JP8233375 | 1975-07-02 | JPS5133499A | 1976-03-22 | JEIMUZU RICHAADO BIIDO |
| 7 | Paraglider | JP15063489 | 1989-06-15 | JPH0316899A | 1991-01-24 | OGAWA TAKAHISA |
| PURPOSE: To smooth a wind surface, to smooth the flow of air along the wind surface, and to sharply improve flying performance by a method wherein a sheetform wing smoothing material is stretched astride recessed parts formed in an upper or a lower surface and extended longitudinally of a wing. CONSTITUTION: During gliding, air is taken in each wing chamber 5 through an air intake port, each wing chamber 5 is brought into an inflated state, and a wing is spread in an arcuate shape on the whole. In this case, since a force by which the wing is further spread is exerted on the wing by an air flow, a wing smoothing material 11 is pulled toward both sides by means of an upper or a lower surface 2 or 3 and stretched astride recessed part formed in the upper or lower surface 2 or 3 to smooth the surface of the wing. COPYRIGHT: (C)1991,JPO&Japio | ||||||
| 8 | JPS59501742A - | JP50317483 | 1983-09-28 | JPS59501742A | 1984-10-18 | |
| 9 | JPH0420839B2 - | JP50138784 | 1984-03-09 | JPH0420839B2 | 1992-04-07 | SHUNAIDAA SUTEFUEN ERU |
| 10 | Flying motor vehicle | JP18717085 | 1985-08-26 | JPS6164505A | 1986-04-02 | DON AARU POORINGU |
| 11 | JPS60500665A - | JP50138784 | 1984-03-09 | JPS60500665A | 1985-05-09 | |
| 12 | CANOPY, IN PARTICULAR FOR A PARAGLIDER, PARACHUTE, FLEXKITE, OR SURFKITE CANOPY | US15749567 | 2016-07-27 | US20180222594A1 | 2018-08-09 | Michael Nesler |
| The invention relates to a canopy, in particular for a paraglider, parachute, flexkite, or surfkite, comprising an upper sail and a lower sail as well as profile-forming ribs, characterized in that at least two different zones are formed in the canopy that have different opening and emptying times. | ||||||
| 13 | Ground vehicle with flight capability | US14480061 | 2014-09-08 | US09656526B2 | 2017-05-23 | Robert Nolan |
| Ground vehicles that may include flight capability are described. In some examples, a vehicle frame may include a fuel tank with a main tank and at least two auxiliary tanks, with the main tank disposed substantially along the centerline of the vehicle, and the at least two auxiliary tanks extending upward and outward from the main tank. In some examples, vehicles may include a chassis, a cage attached to the chassis, a front wheelbase attached to the chassis and/or cage, a rear wheelbase attached to the chassis and/or cage, a ground steering mechanism connected to the front wheelbase and/or the rear wheelbase, a motor connected to a propeller, and a propeller shroud at least partially encircling the propeller. | ||||||
| 14 | PARAMOTOR WITH DYNAMIC TORQUE COMPENSATION | US14421538 | 2013-09-26 | US20150217853A1 | 2015-08-06 | Miroslav Svec |
| Paramotor with dynamic torque compensation includes a frame (1), harness or seat (2), engine and propeller (3) rotating in a cage (4) characterized by one or more surfaces placed on the frame and/or the cage in such a way that when air flows around them aerodynamic forces are generated in the opposite direction to the propeller torque. These surfaces are characterized by an asymetric profile (13), a symetric profile with non-zero angle of attack (14), an asymmetric profile with non-zero angle of attack (15) or in a form of flaps or ailerons with non-zero angle of attack (16). The surfaces may have adjustable angle of attack (17). | ||||||
| 15 | Apparatus and method for paragliders | US13719108 | 2012-12-18 | US08894015B2 | 2014-11-25 | Adam Edward Alexander Contoret |
| Apparatus and method for propelling a user wearing paragliding equipment are disclosed The apparatus includes at least one thruster for providing thrust in a predetermined direction; and an attachment element for attaching the at least one thruster to a user's body such that the thruster is secured against the front portion of the user's body. | ||||||
| 16 | Flying entertainment vehicle | US12718803 | 2010-03-05 | US08286907B2 | 2012-10-16 | Anthony Paul Dohi; Scott Frazier Watson; Robert Scott Trowbridge |
| An apparatus for use as a flying entertainment vehicle. The apparatus includes a lift system, such as a parawing, that is inflated by air to generate lift and further includes a vehicle frame attached to the lift system such as by suspension lines that also space the lift system apart from the vehicle frame. The apparatus includes a thrust assembly supported on the vehicle frame that is operable to propel the vehicle at a flight speed at which the lift system is operated, e.g., the parawing is inflated, to generate lift to suspend the vehicle frame above the ground. The apparatus includes show elements that may be supported on or by the vehicle frame and be configured to be lift neutral. The show elements function to distract observers away from the lift system such as by appearing to provide the lift or features that cause the vehicle frame to fly. | ||||||
| 17 | Inflatable wing flight vehicle | US12157600 | 2008-06-11 | US08104718B2 | 2012-01-31 | Donald Orval Shaw |
| The invention is an aircraft having an inflatable wing connected to a base unit, with the inflatable wing inflated with a lifting gas such as helium. The inflatable wing has a series of cell structures, and may be configured with ballonets to selectively introduce and expel outside air within the inflatable wing to vary the buoyancy and/or airfoil properties of the inflatable wing. The aircraft is particularly useful at low speeds and in thin atmospheres (such as at high Earth altitudes and on Mars), and can be used for interplanetary missions to explore planetary bodies, such as moons and planets, having atmospheres. | ||||||
| 18 | Personal Propulsion Device With Hands Free Control | US12754601 | 2010-04-05 | US20120020790A1 | 2012-01-26 | Donald Wesley Burgess, JR. |
| An improved personal propulsion device that generally imparts thrust directly to the user. The device allows hands free control of thrust magnitude and direction so both hands can grasp and control bicycle handlebars and brakes, watercraft paddles, ski poles or other apparatuses. The device is adjustable vertically, on the users' back, higher to allow sitting in a canoe or wheelchair and lower for standing on skates, skis, kick scooters etc. In one embodiment, the device includes an air compressor that is operatively connected to a cam mechanism engaged with the propulsion mechanism to provide compressed air. In another embodiment, the device includes a gap control mechanism to reduce or increase the size of the air inlet gap between the lip of the propeller shroud and an air horn to decrease noise levels or increase propulsion. The air horn can be gradiently flexible and warpable to allow controlled movement thereof. | ||||||
| 19 | Safety flier--a parachute-glider air-vehicle with vertical take-off and landing capability | US12655546 | 2010-01-04 | US20110163198A1 | 2011-07-07 | Glenn Leaver |
| One embodiment of a Vertical Take-off and Landing (VToL) air-vehicle (FIG. 1.) having a horizontal rotor, a. providing lift and propulsion, and communicating at or near its centre to structural elements, or fuselage, b. Upon or within the fuselage structure is attached a platform, to which a payload, or occupant or pilot, d. is secured in such a manner as to permit a movement, or range-of-motion, of the payload, as a means of weight-shifting, or mass-balancing, of the vehicle for stability and control in flight. At least two planar elements, or descent-vanes, c.i & c.ii are connected to a structural element of the fuselage at a location which provides vertical and horizontal separation between the rotor and the descent-vanes, thus creating a tandem, biplane arrangement of two aerodynamically active elements which are aerodynamically balanced to provide stability and controllability in hovering flight, in forward flight, and in un-powered gliding and vertical descents. Other embodiments are described and shown. | ||||||
| 20 | Inflatable wing flight vehicle | US12157600 | 2008-06-11 | US20090108135A1 | 2009-04-30 | Donald Orval Shaw |
| The invention is an aircraft having an inflatable wing connected to a base unit, with the inflatable wing inflated with a lifting gas such as helium. The inflatable wing has a series of cell structures, and may be configured with ballonets to selectively introduce and expel outside air within the inflatable wing to vary the buoyancy and/or airfoil properties of the inflatable wing. The aircraft is particularly useful at low speeds and in thin atmospheres (such as at high Earth altitudes and on Mars), and can be used for interplanetary missions to explore planetary bodies, such as moons and planets, having atmospheres. | ||||||
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