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 |
|---|---|---|---|---|---|---|
| 41 | UAV whith deployable wings and method of flight control | EP10833732.0 | 2010-09-09 | EP2475575B1 | 2017-11-01 | MIRALLES, Carlos, Thomas; PLUMB, Nick; TAO, Tony Shuo; OLSEN, Nathan |
| A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements. | ||||||
| 42 | SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE | EP13832668.1 | 2013-06-07 | EP2858898B1 | 2017-10-18 | ANDRYUKOV, Oleksandr |
| 43 | UNMANNED AERIAL VEHICLE AND METHOD OF CONTROLLING THE SAME | EP15003180.5 | 2015-11-06 | EP3069995A1 | 2016-09-21 | Cho, Taehoon; Shin, Choonghwan |
An unmanned aerial vehicle system according to the present invention includes a housing (2000) mounted on a vehicle (10) and having an inner space, the housing provided with a launching unit, an unmanned aerial vehicle (1000) accommodated in the housing and configured to be launched from the housing when a driving state of the vehicle meets a preset condition, wing units (1210) mounted to the unmanned aerial vehicle and configured to allow the flight of the unmanned aerial vehicle in response to the launch from the housing, an output unit disposed on the unmanned aerial vehicle, and a controller configured to control the wing units to move the unmanned aerial vehicle to a position set based on information related to the driving state when the unmanned aerial vehicle is launched, and control the output unit to output warning information related to the driving state.
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| 44 | DISPOSITIF DE LANCEMENT POUR AÉRONEF COMMANDÉ À DISTANCE | EP14728993.8 | 2014-06-10 | EP3007788A1 | 2016-04-20 | CARPENTIER, Luc; GAUTHIER, Thierry |
| The invention relates to a device designed to launch a drone, comprising a rail (21) extending along a longitudinal axis (22) and a carriage (23), movable on the rail (21), able to support and launch a drone by accelerating the carriage (23) between a loading position and an end-of-travel position, characterized in that it further comprises a spring mechanism (41) configured to exert a return force on the carriage (23) along the longitudinal axis that is substantially constant between the two positions. The spring mechanism (41) comprises at least one spring coiled around a hub, one end of the coiled spring being connected to the carriage (23), the return force exerted on the carriage being generated by winding the spring around the hub. | ||||||
| 45 | SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE | EP13832668.1 | 2013-06-07 | EP2858898A2 | 2015-04-15 | ANDRYUKOV, Oleksandr |
| An unmanned aerial vehicle (UAV) launch tube (100) that has at least one layer of prepeg substrate disposed about an aperture (106) to form a tube, a sabot (110) disposed in an interior of said tube (100), said sabot (110) having a first clasp tab (126), and a clasp (124) detachably coupled to said first clasp tab and contacting an inner circumferential wall (102) of said tube (100) so that said clasp (124) is rotationally constrained by the inner circumferential wall (102) and said first clasp tab (126). | ||||||
| 46 | SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE | EP10833731.2 | 2010-09-09 | EP2475578A2 | 2012-07-18 | MIRALLES, Carlos Thomas; SU, Guan H.; ANDRYUKOV, Oleksandr; MCNEIL, John |
| An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505). | ||||||
| 47 | NOISE SUPPRESSION DEVICE FOR A DRONE LAUNCH TUBE | EP16179915.0 | 2010-09-09 | EP3133019B1 | 2018-12-05 | Miralles, Carlos Thomas; Andryukov, Alexander; Su, Guan H.; McNeil, John |
| An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505). | ||||||
| 48 | ELEVON CONTROL SYSTEM | EP17183571.3 | 2010-09-09 | EP3348955A1 | 2018-07-18 | MIRALLES, Carlos Thomas; PLUMB, Nick; TAO, Tony Shuo; OLSEN, Nathan |
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045,1046,1145,1146,1245,1345,1346,1445,1446,1545,1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
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| 49 | UNMANNED AERIAL COPTER FOR PHOTOGRAPHY AND/OR VIDEOGRAPHY | EP15795669 | 2015-05-22 | EP3145811A4 | 2018-05-23 | BRADLOW HENRY W; BALARESQUE ANTOINE; ENGLIN ROBERT N |
| An unmanned aerial vehicle (UAV) copter for consumer photography or videography can be launched by a user throwing the UAV copter into mid-air. The UAV copter can detect that the UAV copter has been thrown upward while propeller drivers of the UAV copter are inert. In response to detecting that the UAV copter has been thrown upward, the UAV copter can compute power adjustments for propeller drivers of the UAV copter to have the UAV copter reach a predetermined elevation above an operator device. The UAV copter can then supply power to the propeller drivers in accordance with the computed power adjustments. | ||||||
| 50 | PAYLOAD LAUNCHER AND AUTONOMOUS UNDERWATER VEHICLE | EP15751720 | 2015-02-20 | EP3107805A4 | 2018-01-10 | SYLVIA RUSSELL M; LEWIS MARTIN C; WHALEN MARK E; GORDON ROBERT P |
| A payload launch system is described that provides one launch solution suitable for multiple applications. A payload, such as a UAV, is launched from a sealed launch tube using compressed gas or other energy source. The launch tube can be used to transport and protect the payload from harsh environments for extended periods prior to launch. | ||||||
| 51 | Reinforced UAV launch tube | EP10833731.2 | 2010-09-09 | EP2475578B1 | 2017-07-19 | MIRALLES, Carlos Thomas; SU, Guan H.; ANDRYUKOV, Oleksandr; MCNEIL, John |
| 52 | ROTARY-WING AIR VEHICLE AND METHOD AND APPARATUS FOR LAUNCH AND RECOVERY THEREOF | EP15275222 | 2015-10-30 | EP3162707A1 | 2017-05-03 | |
| A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in use, to lift and propel said air vehicle, said rotor devices (16a, 16b) being arranged and configured relative to said main body (12) such that the blades thereof do not cross through a central vertical axis of said main body (12) defining the centre of mass thereof, wherein said main body (12) is provided with an aperture (100) that extends therethrough to define a channel about said central vertical axis. | ||||||
| 53 | HAND-LAUNCHED UNMANNED AERIAL VEHICLE | EP16196359 | 2016-10-28 | EP3162705A1 | 2017-05-03 | ZAHO GUOCHENG; LUO WEI |
| The invention discloses a hand-launched unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The hand-launched unmanned aerial vehicle comprises a body, a tail, at least one power source and a lens bin, wherein the body comprises a middle section, a first side section and a second side section; two sides of the middle section are respectively detachably connected with the first side section and the second side section correspondingly; the tail is fixed to the middle section; the power source is fixed to the middle section; and the lens bin is fixed to the middle section and provided with a flexible cushion. The invention overcomes the technical defects in the prior art that the body maintenance cost of the hand-launched unmanned aerial vehicle is high and the lens bin is very likely to be damaged due to collision between the lens bin of the hand-launched unmanned aerial vehicle and the ground. | ||||||
| 54 | SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE | EP16179915.0 | 2010-09-09 | EP3133019A1 | 2017-02-22 | Miralles, Carlos Thomas; Andryukov, Alexander; Su, Guan H.; McNeil, John |
An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).
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| 55 | SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE | EP13832668 | 2013-06-07 | EP2858898A4 | 2016-03-02 | ANDRYUKOV OLEKSANDR |
| 56 | ELEVON CONTROL SYSTEM | EP10833732 | 2010-09-09 | EP2475575A4 | 2015-07-08 | MIRALLES CARLOS THOMAS; PLUMB NICK; TAO TONY SHUO; OLSEN NATHAN |
| A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements. | ||||||
| 57 | ELEVON CONTROL SYSTEM | EP10833732.0 | 2010-09-09 | EP2475575A2 | 2012-07-18 | MIRALLES, Carlos, Thomas; PLUMB, Nick; TAU, Shuo; OLSEN, Nathan |
| A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements. | ||||||
| 58 | FOLDABLE WINGS FOR AN UNMANNED AERIAL VEHICLE | US15755669 | 2016-08-25 | US20190023374A1 | 2019-01-24 | MOSHE KAHLON; AMIT MORAG |
| An unmanned air vehicle (UAV) having a fuselage, a foldable propulsion means to generate thrust leading to the UAV movement, a driving means to drive the propulsion means and a plurality of flight control surfaces actuators are further included. The UAV further includes at least one pair of foldable wings where the rear portion of the wings is pivotally attached to the fuselage. The wings having at least one roll control surface hinged to at least one of the foldable wings. At least a pair of tail stabilizers having ruddervators flight control surfaces hinged to the tail stabilizers. In a fully extended position or in ready to fly state position, each of the foldable wings are deployed perpendicular to one another and perpendicular to the fuselage to form an offset-x shaped wings, and in a stowed position, each of the wings are positioned parallel to one another and positioned parallel to the fuselage. | ||||||
| 59 | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube | US14887675 | 2015-10-20 | US10124909B2 | 2018-11-13 | Carlos Thomas Miralles; Guan H Su; Alexander Andryukov; John McNeil |
| An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture, and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505). | ||||||
| 60 | Methods for launching and landing an unmanned aerial vehicle | US15608417 | 2017-05-30 | US10101748B2 | 2018-10-16 | Mingyu Wang |
| Methods and apparatus are provided for launching and landing unmanned aerial vehicles (UAVs) including multi-rotor aircrafts. The methods and apparatus disclosed herein utilize positional change of the UAV, visual signal, or other means to effect the launch or landing. The methods and apparatus disclosed herein are user friendly, particularly to amateur UAV users lacking practice of operating a UAV. | ||||||
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