专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明专利

SG11201908005PA CONSTANT TENSION TETHER MANAGEMENT SYSTEM FOR TETHERED AIRCRAFT 未知
公开(公告)号：SG11201908005PA
公开(公告)日：2019-09-27
申请号：SG11201908005P
申请日：2018-03-06
申请人： HOVERFLY TECHNOLOGIES INC
发明人： WHITAKER LUCAS
IPC分类号： B64C39/02 , B64F3/00 , B66D1/50
摘要： WO 18/ 165 19 2 Al (12) INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (19) World Intellectual Property Organization International Bureau (43) International Publication Date 13 September 2018 (13.09.2018) WIP0 I PCT olimion °nolo mu H oiciolommio oimIE (10) International Publication Number WO 2018/165192 Al A KRAFT (51) International Patent Classification: B64F 3/00 (2006.01) B66D 1/50 (2006.01) B64C 39/02 (2006.01) (21) International Application Number: PCT/US2018/021199 (22) International Filing Date: 06 March 2018 (06.03.2018) (25) Filing Language: English (26) Publication Language: English (30) Priority Data: 62/467,626 06 March 2017 (06.03.2017) US (71) Applicant: HOVERFLY TECHNOLOGIES, INC. [US/US]; 12151 Research Parkway, Suite 100, Orlando, FL 32826 (US). (72) Inventor: WHITAKER, Lucas, Colt; 12700 Waterford Willow Ln Apt 206, Orlando, FL 32828 (US). (74) Agent: GITTEN, Howard, M. et al.; Lock Lord LLP, P.O. Box 55874, Boston, MA 02205 (US). (81) Designated States (unless otherwise indicated, for every kind of national protection available): AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW. (84) Designated States (unless otherwise indicated, for every kind of regional protection available): ARIPO (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW), Eurasian (AM, AZ, BY, KG, KZ, RU, TJ, TM), European (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR), OAPI (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG). Published: — with international search report (Art. 21(3)) (54) Title: CONSTANT TENSION TETHER MANAGEMENT SYSTEM FOR TETHERED AIRCRAFT (57) : A constant tension tether management system for tethered aircraft 104 includes a ground station for operatively coupling to an unmanned aerial vehicle. The ground station includes a spool rotatably disposed within the ground station and adapted to support a tether thereon. A first pulley is rotatably mounted within 100' . the ground station along a tether travel path. A second pulley is rotatably disposed within the ground station and moves in translation along the tether travel path. The first pulley is disposed along the tether travel path between the spool and the second pulley. GROUNDL,108 STATION FIG. I

2. 发明专利

SG11202108791VA LANDING STRUCTURE FOR AN UNMANNED AERIAL VEHICLE 未知
公开(公告)号：SG11202108791VA
公开(公告)日：2021-09-29
申请号：SG11202108791V
申请日：2020-02-14
申请人： HOVERFLY TECHNOLOGIES INC
发明人： DUCHARME ALFRED , STEPIEN ADAM , TABOR JASON , WHITAKER LUCAS , BURROUGHS DANIEL
IPC分类号： B64F1/22 , B64C39/02
摘要： A system for landing an unmanned aerial vehicle has an unmanned aerial vehicle and a ground-based platform. A guide structure for receiving the unmanned aerial vehicle is mounted on the ground base platform. The guide structure has an inner diameter greater than a smallest outer diameter of the unmanned aerial vehicle landing gear and less than the largest outer diameter of the unmanned aerial vehicle landing gear.

3. 发明专利

SG11202108789RA SYSTEM AND METHOD FOR DETERMINING WIND DIRECTION AND VELOCITY MEASUREMENT FROM ALTITUDE FOR AN UNMANNED AERIAL VEHICLE 未知
公开(公告)号：SG11202108789RA
公开(公告)日：2021-09-29
申请号：SG11202108789R
申请日：2020-02-14
申请人： HOVERFLY TECHNOLOGIES INC
发明人： DUCHARME ALFRED , TOPPING ROBERT
IPC分类号： G01P5/08 , B64C39/02 , B64D45/00
摘要： Wind speed and direction experienced by the UAV at altitude is determined by placing an accelerometer, gyroscope and compass on the UAV. A change in velocity experienced by the UAV is determined by the accelerometer. An orientation relative to a reference plane and an angular velocity experienced by the UAV is determined by the gyroscope. A magnetic bearing of the UAV is determined with the compass. A roll and pitch exhibited by the UAV is determined as a function of the change in velocity, orientation and change in angular velocity. Projected roll and projected pitch vectors onto a horizontal plane cutting through the center of rotation of the UAV are determined as a function of the roll and the pitch. The wind speed of the wind experienced by the UAV is determined as a function of the projected roll vector and projected pitch vector. The wind direction is determined as a function of the projected roll vector and projected pitch vector and the magnetic bearing of the UAV.

4. 发明申请

US20130110325A1 CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE UTILIZING PARALLEL PROCESSING ARCHITECTURE 审中-公开
标题翻译：不平衡车辆使用平行处理结构的控制系统
公开(公告)号：US20130110325A1
公开(公告)日：2013-05-02
申请号：US13659024
申请日：2012-10-24
申请人： Hoverfly Technologies, Inc.
发明人： George Richard Sapp, II , Alfred D. Ducharme , Daniel Burroughs , Stacey L. Ducharme
IPC分类号： G05D1/00
CPC分类号： G05D1/0088 , G05D1/0858
摘要： A UAV has two rotors. First and second sensors sense a first and second type of input respectively. The second type of input is different than the first type, the first sensor providing a first sensor output and the second sensor providing a second sensor output. The first sensor output is input to a first computer and the second sensor output is input to a second computer. The first and second computer communicate in parallel to process the first and second sensor outputs to create a control signal having a predetermined number of variables therein, each variable having an exclusive position within the signal. The first computer outputs a first variable and the second computer outputs a second variable, each output being assigned an exclusive position within the control signal. At least one of the first and second computers outputting the control signal to the rotors.
摘要翻译：无人机有两个转子。第一和第二传感器分别感测第一和第二类型的输入。第二类型的输入与第一类型不同，第一传感器提供第一传感器输出，第二传感器提供第二传感器输出。第一传感器输出被输入到第一计算机，第二传感器输出被输入到第二计算机。第一和第二计算机并行通信以处理第一和第二传感器输出以创建其中具有预定数量的变量的控制信号，每个变量在信号内具有排他位置。第一计算机输出第一变量，第二计算机输出第二变量，每个输出被分配在控制信号内的排他位置。第一和第二计算机中的至少一个将控制信号输出到转子。

5. 发明申请

WO2018165192A1 CONSTANT TENSION TETHER MANAGEMENT SYSTEM FOR TETHERED AIRCRAFT 审中-公开
公开(公告)号：WO2018165192A1
公开(公告)日：2018-09-13
申请号：PCT/US2018/021199
申请日：2018-03-06
申请人： HOVERFLY TECHNOLOGIES, INC.
发明人： WHITAKER, Lucas, Colt
IPC分类号： B64F3/00 , B64C39/02 , B66D1/50
摘要： A constant tension tether management system for tethered aircraft includes a ground station for operatively coupling to an unmanned aerial vehicle. The ground station includes a spool rotatably disposed within the ground station and adapted to support a tether thereon. A first pulley is rotatably mounted within the ground station along a tether travel path. A second pulley is rotatably disposed within the ground station and moves in translation along the tether travel path. The first pulley is disposed along the tether travel path between the spool and the second pulley.

6. 发明专利

AU2020258267A1 Landing structure for an unmanned aerial vehicle 未知
公开(公告)号：AU2020258267A1
公开(公告)日：2021-09-02
申请号：AU2020258267
申请日：2020-02-14
申请人： HOVERFLY TECHNOLOGIES INC
发明人： DUCHARME ALFRED D , STEPIEN ADAM , TABOR JASON , WHITAKER LUCAS COLT , BURROUGHS DANIEL J
IPC分类号： B64F1/22 , B64C39/02
摘要： A system for landing an unmanned aerial vehicle has an unmanned aerial vehicle and a ground-based platform. A guide structure for receiving the unmanned aerial vehicle is mounted on the ground base platform. The guide structure has an inner diameter greater than a smallest outer diameter of the unmanned aerial vehicle landing gear and less than the largest outer diameter of the unmanned aerial vehicle landing gear.

7. 发明专利

AU2020223160A1 System and method for determining wind direction and velocity measurement from altitude for an unmanned aerial vehicle 未知
公开(公告)号：AU2020223160A1
公开(公告)日：2021-09-02
申请号：AU2020223160
申请日：2020-02-14
申请人： HOVERFLY TECHNOLOGIES INC
发明人： DUCHARME ALFRED D , TOPPING ROBERT
IPC分类号： G01P5/08 , B64C39/02 , B64D45/00
摘要： Wind speed and direction experienced by the UAV at altitude is determined by placing an accelerometer, gyroscope and compass on the UAV. A change in velocity experienced by the UAV is determined by the accelerometer. An orientation relative to a reference plane and an angular velocity experienced by the UAV is determined by the gyroscope. A magnetic bearing of the UAV is determined with the compass. A roll and pitch exhibited by the UAV is determined as a function of the change in velocity, orientation and change in angular velocity. Projected roll and projected pitch vectors onto a horizontal plane cutting through the center of rotation of the UAV are determined as a function of the roll and the pitch. The wind speed of the wind experienced by the UAV is determined as a function of the projected roll vector and projected pitch vector. The wind direction is determined as a function of the projected roll vector and projected pitch vector and the magnetic bearing of the UAV.

8. 发明申请

WO2020214236A2 LANDING STRUCTURE FOR AN UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：WO2020214236A2
公开(公告)日：2020-10-22
申请号：PCT/US2020/018280
申请日：2020-02-14
申请人： HOVERFLY TECHNOLOGIES, INC.
发明人： DUCHARME, Alfred, D. , STEPIEN, Adam , TABOR, Jason , WHITAKER, Lucas, Colt , BURROUGHS, Daniel, J.
IPC分类号： B64F1/22
摘要： A system for landing an unmanned aerial vehicle has an unmanned aerial vehicle and a ground-based platform. A guide structure for receiving the unmanned aerial vehicle is mounted on the ground base platform. The guide structure has an inner diameter greater than a smallest outer diameter of the unmanned aerial vehicle landing gear and less than the largest outer diameter of the unmanned aerial vehicle landing gear.

9. 发明申请

WO2020168189A2 SYSTEM AND METHOD FOR DETERMINING WIND DIRECTION AND VELOCITY MEASUREMENT FROM ALTITUDE FOR AN UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：WO2020168189A2
公开(公告)日：2020-08-20
申请号：PCT/US2020/018287
申请日：2020-02-14
申请人： HOVERFLY TECHNOLOGIES, INC.
发明人： DUCHARME, Alfred, D. , TOPPING, Robert
IPC分类号： G01P5/08 , B64C39/02 , B64D45/00
摘要： Wind speed and direction experienced by the UAV at altitude is determined by placing an accelerometer, gyroscope and compass on the UAV. A change in velocity experienced by the UAV is determined by the accelerometer. An orientation relative to a reference plane and an angular velocity experienced by the UAV is determined by the gyroscope. A magnetic bearing of the UAV is determined with the compass. A roll and pitch exhibited by the UAV is determined as a function of the change in velocity, orientation and change in angular velocity. Projected roll and projected pitch vectors onto a horizontal plane cutting through the center of rotation of the UAV are determined as a function of the roll and the pitch. The wind speed of the wind experienced by the UAV is determined as a function of the projected roll vector and projected pitch vector. The wind direction is determined as a function of the projected roll vector and projected pitch vector and the magnetic bearing of the UAV.

10. 发明授权

US10365663B2 Tether orientation sensor for controlling the position of a tethered aircraft 有权
公开(公告)号：US10365663B2
公开(公告)日：2019-07-30
申请号：US15344393
申请日：2016-11-04
申请人： Hoverfly Technologies, Inc.
发明人： Alfred D. Ducharme , Daniel Burroughs , Lucas C. Whitaker
IPC分类号： G05D1/08 , B64C39/02
摘要： An unmanned aerial vehicle has a substrate. A tether sensor is mounted on the substrate. The tether sensor determines an orientation of the tether relative to the substrate. A micro controller, receiving the measured orientation from the tether sensor, determines an orientation of the tether relative to the substrate, and as a function of the orientation, determines a corrective value and outputs the corrective value to the unmanned aerial vehicle as at least one of a roll output and a pitch output control signal.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式