| 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 | FLUGZEUGKONSTRUKTION MIT START UND LANDUNG AUF DEN FÜSSEN DES PILOTEN | EP83903818.0 | 1983-11-30 | EP0127652A1 | 1984-12-12 | RUBIK, Ernö |
| La structure d'avion permet le décollage et l'atterrissage sur les pieds du pilote et représente une structure entre les planeurs en forme de cerf-volant et les avions légers. La caractéristique de la structure d'avion est de présenter des ailes (12) en porte-à-faux ou dotées d'un étayage extérieur et mobiles en particulier dans le même plan grâce à un mécanisme actionné par le pilote (15). | ||||||
| 22 | A THERMALLING SAILPLANE TURN INDICATOR | EP82902707.0 | 1982-09-23 | EP0089967A1 | 1983-10-05 | NORMAN, Colin David |
| Indicateur d'ascendance thermique avec un détecteur (28) monté sur les moignons (12, 13) des ailes d'un planeur pour détecter le mouvement relatif entre ces dernières dû aux moments de flexion s'exerçant sur les ailes lors de la rencontre d'une ascendance thermique, et processeur des signaux du détecteur pour produire des signaux indiquant la direction du virage pour entrer dans l'ascendance thermique. Les signaux du processeur sont affichés et indiquent la force de l'ascendance thermique, ainsi que les directions à gauche ou à droite pour entrer dans l'ascendance thermique. | ||||||
| 23 | An unmanned aerial vehicle harvesting energy in updraft | EP12382052.4 | 2012-02-17 | EP2629166B1 | 2016-08-17 | Criado, Alfredo |
| 24 | AIR EXTRACTOR FROM A COCKPIT OF A CRAFT | EP11717775.8 | 2011-04-06 | EP2555975B1 | 2014-03-26 | JONKER, Adrianus, Stefanus; BOSMAN, Johannes, Jacobus |
| 25 | System and method for airborne wind energy production | EP12157057.6 | 2012-02-27 | EP2631468A1 | 2013-08-28 | Ruiterkamp, Richard, Dr. |
The inventions provides for a system for electric power production from wind (50) comprising a glider (10), said glider (10) having an airfoil (14), on-board steering means (20, 22, 24) for pitching, rolling and yawing the glider (10) when airborne, a flight control means (64) for operation of the steering means (20, 22, 24), and a connection means for a tether (44), the system further comprising a ground station (40), said ground station (40) comprising a reel (42) for the tether (44), a rotating electrical machine (46) connected to the reel (42), and a ground station control means (66) for operation of the reel (42) and the rotating electrical machine (46), and the system further comprising a master control means (62) for operation of the system in at least two alternative operation modes, wherein a first operation mode of the system is provided for electric power production with the rotating electrical machine (46) from a rotation of the reel (42) induced by reeling out the tether (44) using a lift force generated upon exposure of the airfoil (14) of the airborne glider (10) to wind (50), and wherein a second operation mode of the system is provided for system recovery by driving the reel (42) with the rotating electrical machine (46), thereby reeling in the tether (44) onto the reel (42). The invention further provides for a method for operation of a system for electric power production from wind (50), for a glider (10) for a system according to the invention and for use of a glider (10) for production of electric power form wind.
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| 26 | AILE RIGIDE DE PORTANCE VARIABLE PAR DEPLOIEMENT D'UNE AILE SOUPLE | EP04767408.0 | 2004-06-22 | EP1658221B1 | 2007-03-28 | Herzberger, Erick |
| The invention relates to a wing with variable sustentation for small aeroplanes or ULM planes, said wing being characterised in that it has a flexible wing system (3) that can be continuously deployed in the extension of the rigid wing (4) by means of at least one articulated system (5), and in that said flexible wing system (3) and said articulated system (5) are completely incorporated into the rear part of the rigid wing (4) in the configuration of a cruising flight. | ||||||
| 27 | AILE RIGIDE DE PORTANCE VARIABLE PAR DEPLOIEMENT D'UNE AILE SOUPLE | EP04767408.0 | 2004-06-22 | EP1658221A1 | 2006-05-24 | Herzberger, Erick |
| The invention relates to a wing with variable sustentation for small aeroplanes or ULM planes, said wing being characterised in that it has a flexible wing system (3) that can be continuously deployed in the extension of the rigid wing (4) by means of at least one articulated system (5), and in that said flexible wing system (3) and said articulated system (5) are completely incorporated into the rear part of the rigid wing (4) in the configuration of a cruising flight. | ||||||
| 28 | Steering aid for steering a glider | EP94110419.2 | 1994-07-05 | EP0633184A1 | 1995-01-11 | Zakai, Avi |
A steering aid (12) for aiding a glider pilot (10) to steer into an upwardly moving air current, the steering aid comprising channelling means (15, 16) for channelling therethrough a substantially non-turbulent air current and direction sensing means mounted in conjunction with the channelling means for sensing the air current and for producing respective first and second signals, depending on a direction of flow of the air current through the channelling means. An indication means is coupled to the direction sensing means and responsive to the first or second signal for producing respective indication signals. |
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| 29 | Appareil pour l'épandage aérien | EP82400353.7 | 1982-03-02 | EP0061370B1 | 1986-11-26 | Perinet, Roland Jean Yvon |
| 30 | A THERMALLING SAILPLANE TURN INDICATOR. | EP82902707 | 1982-09-23 | EP0089967A4 | 1984-11-07 | NORMAN COLIN DAVID |
| A thermal indicator with a sensor (28) mounted over the wing stubs (12, 13) of a sailplane to detect relative movement therebetween due to bending moments applied to the wings on meeting a thermal and a processor of the sensor signals to generate signals indicative of the direction to be turned to enter the thermal. The processor signals are suitably displayed to indicate thermal strength, and left or right directions to enter the thermal. | ||||||
| 31 | Single use logistic glider | US15715016 | 2017-09-25 | US10040549B2 | 2018-08-07 | Martinus M. Sarigul-Klijn; Maurice P. Gionfriddo; Nesrin Sarigul-Klijn |
| A disposable airdropped glider. The glider body is constructed from precut panels cut from (MDO) or (HDO) plywood and assembled with pocket-screw joinery or piano hinges. A skid board forms a landing surface and a cargo deck roll-off surface. The glider has pivoting wings and struts. The glider has a triple-tail, a flat nose and honeycomb paperboard panels between the nose and the cargo. Wings are pivoted from a position overlying the fuselage to a flying position by gas springs in wing spars which are compressed by a chain attached to the fuselage through a rotating bracket such that the gas springs are compressed when the wings are folded. The airfoils are plastic extrusions with openings that hold the wing spars and co-formed jury spars which attach the upper and lower surface of the wing. A parachute uses a part of the tail structure to form a deployment drogue. | ||||||
| 32 | System and method for air launch from a towed aircraft | US15046789 | 2016-02-18 | US09944410B1 | 2018-04-17 | Gerald D Budd |
| The invention is a system and method of air launching a powered launch vehicle into space or high altitude. More specifically, the invention is a tow aircraft which tows an unpowered glider, with the powered launch vehicle attached thereto, to launch altitude. The powered launch vehicle is released from the unpowered glider and powered on for launch. | ||||||
| 33 | FOLDABLE WING AND ROTOCRAFT AND GLIDER USING THE SAME | US15479301 | 2017-04-05 | US20170283035A1 | 2017-10-05 | Lanping JI; Xu WANG |
| The present invention provides a foldable wing which comprises a wing supporting skeleton, a sliding rail, a skin supporting rib, a skin and a wing movement unit. The wing supporting skeleton comprises a horizontal beam, a longitudinal beam, a wing front edge beam, a wing trailing edge beam, a fixture connector and a sliding block, The wing supporting skeleton is a triangular girder for maintaining planar and sectional shapes of the foldable wing, supporting the skin supporting rib and the skin, and sustaining an aerodynamic load from the skin and a load of a fuselage. After the triangular girder is subjected to a force of the wing movement unit, a shape and an area of the triangular girder are changed so as to achieve folding and unfolding of the foldable wing. A rotocraft and a glider using the foldable wing are also provided. | ||||||
| 34 | Systems, devices, and/or methods for managing targeted payload descent | US14596471 | 2015-01-14 | US09703295B1 | 2017-07-11 | David Anthony Neal, III; Kevin Marlan Ehlmann; William Thomas Gressick; Alec Jacob Devine Bateman; Kenneth Richard Horneman |
| Certain exemplary embodiments can provide a system, machine, device, manufacture, circuit, composition of matter, and/or user interface adapted for and/or resulting from, and/or a method and/or machine-readable medium comprising machine-implementable instructions for, activities that can comprise and/or relate to, providing a guided descent from a release zone and toward an entry zone. | ||||||
| 35 | Systems, devices, and/or methods for managing targeted payload descent | US13836320 | 2013-03-15 | US08939056B1 | 2015-01-27 | David Anthony Neal, III; Kevin Marlan Ehlmann; William Thomas Gressick; Alec Jacob Devine Bateman; Kenneth Richard Horneman |
| Certain exemplary embodiments can provide a system, machine, device, manufacture, circuit, composition of matter, and/or user interface adapted for and/or resulting from, and/or a method and/or machine-readable medium comprising machine-implementable instructions for, activities that can comprise and/or relate to, providing a guided descent from a release zone and toward an entry zone. | ||||||
| 36 | Efficient control and stall prevention in advanced configuration aircraft | US11623042 | 2007-01-12 | US08657226B1 | 2014-02-25 | John William McGinnis |
| Multiple initiatives are applied to achieve synergistic control enhancement and drag reduction benefits in an aircraft having independent airfoils producing downward force opposite to wing lift in normal flight, which are supported in specific wingtip locations. A method is disclosed teaching the exemplary stall resistance and control at high angles of attack demonstrated by preferred embodiments of the invention. | ||||||
| 37 | Partially-Inflated Rigid-Structure Glider | US13925797 | 2013-06-24 | US20130284853A1 | 2013-10-31 | Christopher Paul Farbolin |
| A partially-inflated rigid-structure glider is a portable or collapsible gliding apparatus that a user can transport in a carrying case. The gliding apparatus includes a rigid yet collapsible frame, tension membranes over both on the wings and tail, and inflatable bladder, a pair of drogue brakes, and a left and right steering mechanism. The pair of drogue brakes is located on opposing sides of the gliding apparatus and create drag on its respective side in order to turn the gliding apparatus either left or right. The user can activate either drogue brake with the left and right steering mechanism, which are control lines attached to each drogue brake. The tension membranes are fitted over the frame so that the gliding apparatus has an airfoil shape in order to create lift with the wings and tail while the gliding apparatus is in flight. | ||||||
| 38 | Ram air Rigid Structure Glider | US13187482 | 2011-07-20 | US08490915B2 | 2013-07-23 | Christopher Paul Farbolin |
| The present invention is a ram air rigid structure glider, which uses both ram air inflation and a rigid structure in order to produce the necessary aerodynamic lift to glide through the air. The frame uses two main structural beams, the spar and the keel, to form the general shape of the wings and the tail. The hubs and the network of lines expand the structure laid out by the spur and the keel. The hubs are evenly placed along the spur, and the network of lines are connected and crisscrossed in between the hubs. The sail is a piece fabric wrapped around the frame and has a plurality of cells, which are evenly spaces throughout the sail. The plurality of cells allows the sails to be inflated by ram air pressure. The pilot pod carries the user in the supine position and is attached to the frame. | ||||||
| 39 | Ram Air Rigid Structure Glider | US13187482 | 2011-07-20 | US20120018568A1 | 2012-01-26 | Christopher Paul FARBOLIN |
| The present invention is a ram air rigid structure glider, which uses both ram air inflation and a rigid structure in order to produce the necessary aerodynamic lift to glide through the air. The frame uses two main structural beams, the spar and the keel, to form the general shape of the wings and the tail. The hubs and the network of lines expand the structure laid out by the spur and the keel. The hubs are evenly placed along the spur, and the network of lines are connected and crisscrossed in between the hubs. The sail is a piece fabric wrapped around the frame and has a plurality of cells, which are evenly spaces throughout the sail. The plurality of cells allows the sails to be inflated by ram air pressure. The pilot pod carries the user in the supine position and is attached to the frame. | ||||||
| 40 | SPAR FOR SAILWINGS | US12139373 | 2008-06-13 | US20100001122A1 | 2010-01-07 | Neil Thomas Boertlein |
| A sail wing for a lightweight aircraft comprising a membrane; a front spar; and a tensioned rear wire attached to a trailing edge of the membrane, such that when the front spar is bent to match a curve of the tensioned trailing edge of the sail wing membrane, the sail wing membrane has substantially little or no twist, and results in substantially little or no induced drag. | ||||||
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