公开(公告)号：WO2021137905A2

公开(公告)日：2021-07-08

申请号：PCT/US2020/052221

申请日：2020-09-23

Applicant: ROGERS CORPORATION

Inventor： DAIGLE, Robert C. ,  WILLIAMS, Shawn P. ,  BRANDSTEIN, Mark

IPC: G01S7/00 ,  G01S13/86 ,  G01S13/93 ,  B64C1/36 ,  B64C2201/027 ,  B64C2201/12 ,  B64C39/024 ,  G01S13/87 ,  G01S13/935 ,  G01S7/003 ,  G01S7/006

Abstract: A radar-enabled multi-vehicle system includes: at least two vehicles, each vehicle having: at least one antenna; a radar module configured and disposed to be in signal communication with the at least one antenna, the radar module configured to transmit and receive radar signals from and to the at least one antenna; a connectivity module configured and disposed to be in signal communication with the radar module, and to be in signal communication with a corresponding connectivity module of another one of the at least two vehicles; and, a power source configured and disposed to provide operational power to the at least one antenna, the radar module, and the connectivity module.

公开(公告)号：WO2021064300A1

公开(公告)日：2021-04-08

申请号：PCT/FR2020/000249

申请日：2020-10-06

Applicant: BRUMEAU, David ,  GRUGEON, Alain

Inventor： BRUMEAU, David ,  GRUGEON, Alain

IPC: B64C39/02 ,  B64C2201/027 ,  B64C2201/126 ,  B64C2201/146 ,  B64C2211/00 ,  B64C39/024

Abstract: Drone professionnel fonctionnel piloté à distance par un utilisateur dont l'électronique de commande (500) dialogue avec l'électronique de commande de pilotage du drone (300) caractérisé en ce que l'architecture mécanique est modulaire avec une embase (1) sur laquelle se fixent des pales, sur l'embase peut se solidariser mécaniquement et électroniquement des modules fonctionnels (3) dont l'électronique de commande fonctionnelle (300) coopère avec l'électronique de commande de pilotage du drone (100), notamment au moyen d'une architecture logicielle d'identification qui affecte à l'utilisateur un écran d'affichage spécifique de commande du module fonctionnel et de l'embase calculé en fonction de l'identité du module fonctionnel dont l'identité est lue par le dialogue entre les électroniques de commande de pilotage de l'embase (100) et celle du module fonctionnel (300).

公开(公告)号：WO2021061810A1

公开(公告)日：2021-04-01

申请号：PCT/US2020/052268

申请日：2020-09-23

Applicant: AMAZON TECHNOLOGIES, INC.

Inventor： METZNER, Jordan Anthony ,  PATERSON, Michael Edward James ,  WILD, Benjamin ,  SIMINOFF, James Wyatt

IPC: G08B19/00 ,  G08B13/196 ,  G08B29/18 ,  B64C1/00 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C39/005 ,  B64C39/024 ,  G08B13/1965 ,  G08B21/12 ,  G08B21/182 ,  G08B29/188

Abstract: An aerial vehicle is programmed or configured to respond to reports of events or conditions within spaces of a facility. The aerial vehicle travels to a location of a reported event or condition and captures data using onboard sensors. The aerial vehicle independently determines whether the reported event or condition is occurring, or is otherwise properly addressed by resources that are available at the location, using images or other data captured by the onboard sensors. Alternatively, the aerial vehicle transmits a request for additional resources to be provided at the location, where necessary. A map of the location generated based on images or other data captured by the onboard sensors may be utilized for any purpose, such as to make one or more recommendations of products that are appropriate for use at the facility.

公开(公告)号：WO2021053600A2

公开(公告)日：2021-03-25

申请号：PCT/IB2020/058711

申请日：2020-09-18

Applicant: KANDASAMY, Dushan

Inventor： KANDASAMY, Dushan

IPC: B64C39/06 ,  G01P13/02 ,  B64C25/62 ,  B64C39/02 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/162 ,  B64C39/024 ,  B64C39/062

Abstract: The present invention discloses a drone, comprising a cyclical hull with one or more cyclical rings, an external structure, and a piezoelectric system. The external structure comprises a fixed wing and a rotary turbine construction. The external structure is securely and rotationally connected to the cyclic ring. The external structure is configured to rotate exponentially around the cyclical hull, thereby enabling a stabilization capability of the drone to forward in the desired direction. The piezoelectric system is mounted on the cyclical hull for efficiently analyzing onward wind direction, thereby effectively rotating the external structure at high speeds to enable the structural integrity of the drone. The drone further comprises one or more locking systems to unlock the cyclical rotational turbine based on an alert received from the piezoelectric system. Further, the drone comprises a camera for capturing a surrounding view of the drone.

公开(公告)号：WO2022235677A1

公开(公告)日：2022-11-10

申请号：PCT/US2022/027481

申请日：2022-05-03

Applicant: BEIROBOTICS LLC

Inventor： BEIRO, Michael Kenneth ,  CORBIN, Alvin Leroy ,  COBLE, Chase Hamilton ,  SCHUL, David Carson

IPC: B64D1/22 ,  B64C2201/027 ,  B64C2201/126 ,  B64C2201/128 ,  B64C39/024 ,  G01R31/085 ,  H02G1/02

Abstract: A payload support frame is adapted to suspend a payload from an unmanned aerial vehicle (UAV) during flight. The frame comprises at least one elongated rigid segment, at least one upper flexible segment at an upper end of the rigid segment, and at least one lower flexible segment at a lower end of the rigid segment. One or more of (a) the at least one rigid segment, (b) the at least one upper flexible segment, or (c) the at least one lower flexible segment comprise a dielectric material. The upper flexible segment is adapted to be selectively attachable, directly or indirectly, to the UAV. The lower flexible segment is adapted to be selectively attachable, directly or indirectly, to the payload.

公开(公告)号：WO2021258399A1

公开(公告)日：2021-12-30

申请号：PCT/CN2020/098339

申请日：2020-06-27

Applicant: SZ DJI TECHNOLOGY CO., LTD.

Inventor： MENON, Arjun Sukumar ,  DU, Jiexi ,  LIU, Yucheng ,  LIU, Weifeng

IPC: G09B29/00 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/146 ,  B64C39/024 ,  G01C21/3837 ,  G01C21/3852 ,  G01C21/3893 ,  H04N5/04 ,  H04N5/247 ,  H04N7/18

Abstract: There is a method for mapping in a movable object environment. The method of mapping may include obtaining mapping data from a scanning sensor (202) of a compact payload (124) coupled to an unmanned aerial vehicle (UAV) (104), the compact payload (124) comprising the scanning sensor (202), one or more cameras (204, 206), and an inertial navigation system (INS) (208) configured to be synchronized using a reference clock signal (1302), obtaining feature data from a first camera of the one or more cameras (204, 206) (1304), obtaining positioning data from the INS (208) (1306), associating the mapping data with the positioning data based at least on the reference clock signal to generate geo-referenced data (1308), and storing the geo-referenced data and the feature data to a removable storage medium (216) (1310).

公开(公告)号：WO2021248003A1

公开(公告)日：2021-12-09

申请号：PCT/US2021/035911

申请日：2021-06-04

Applicant: SAUDI ARABIAN OIL COMPANY ,  ARAMCO SERVICES COMPANY

Inventor： PARROTT, Brian ,  ABDELLATIF, Fadl

IPC: B64C9/14 ,  B64C21/02 ,  B64C39/02 ,  B64D1/00 ,  B64C39/10 ,  G01N1/22 ,  G01N1/00 ,  G01N33/00 ,  B64C3/14 ,  B64C21/08 ,  B64C2201/021 ,  B64C2201/027 ,  B64C2201/028 ,  B64C2201/104 ,  B64C2201/12 ,  B64C39/024 ,  G01N1/2273 ,  G01N2001/2279 ,  G01N33/0004 ,  G01N33/0009

Abstract: A fixed wing drone comprises an air channel embedded therein. The air channel has an upstream an air inlet. A microcontroller mounted within the drone is configured to control navigation of the drone. An air scoop having a section positioned adjacent the inlet to the air channel is adjustable between a first position to capture and divert air into the inlet and thereby to air channel and a second position to block air flow into the air inlet. The air scoop is positioned to divert air flow into the air channel and to the gas sensor during forward flight of the drone. In one embodiment, the fixed wing drone comprises an aircraft having a fuselage and at least two wings. In another embodiment, the fixed wing drone has a flying wing construction, that is, is a tailless design.

公开(公告)号：WO2021239924A2

公开(公告)日：2021-12-02

申请号：PCT/EP2021/064300

申请日：2021-05-27

Applicant: AIRFORESTRY AB

Inventor： ROMAR, Markus ,  GELIN, Olle ,  ANDERSSON, Mauritz

IPC: A01G23/02 ,  A01G23/08 ,  B64C39/00 ,  B64C39/02 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/146 ,  B64C39/024 ,  B64D1/22

Abstract: The present invention relates to a system for remote and/or autonomous cutting at least a portion of a harvested tree trunk, at least a portion of a tree trunk to be harvested, at least a portion of a tree trunk during harvesting or at least a portion of a tree trunk during transporting, said system comprising: a remotely and/or autonomously controlled Unmanned Aerial Vehicle (100), UAV, means (116) for cutting at least a portion of a tree trunk attachable to said UAV (100), means for detecting at least a portion of a tree (135), means for detecting at least one tree parameter of at least a portion of a tree (135) and/or at least one growing condition of at least a portion of a tree (tree), a base station (120) for communication with said UAV (100), and means configured for selecting at least one cutting position on at least a portion of a tree trunk depending on the at least one detected tree parameter and/or the at least one detected growing condition of at least a portion of a tree (135).

公开(公告)号：WO2021225651A2

公开(公告)日：2021-11-11

申请号：PCT/US2021/016392

申请日：2021-02-03

Applicant: SUPPES, Galen, J.

Inventor： SUPPES, Galen, J.

IPC: B64D3/00 ,  B64C39/02 ,  B64F1/04 ,  B64F1/08 ,  B64C37/02 ,  B64C3/38 ,  B64C29/00 ,  B64C19/02 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/12 ,  B64C39/024 ,  B64D2211/00

Abstract: Towed aerodynamic platforms approach the behavior of flat plate airfoils to achieve high lift -to-drag (L:D) performance when operated at low pitch angles. A lead aircraft may tow multiple platforms to form train units. Low form drag and high L:D enable solar aircraft that are more robust and faster than approaches extending wingspan rather than extending the length of the aerial train. Applications extend beyond solar aircraft and include vehicles towed along an overhead monorail system and aerial drones.

公开(公告)号：WO2021190216A1

公开(公告)日：2021-09-30

申请号：PCT/CN2021/077219

申请日：2021-02-22

Applicant: 深圳市格上格创新科技有限公司

Inventor： 杨超峰

IPC: B64C39/02 ,  B64D47/08 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/127

Abstract: 一种全景摄像无人机，包括中空结构的机身（100）、多个摄像头（200）、稳定器（310、320、330）和主动力装置（400）。主动力装置可以配置为第一旋翼系统（410）和第一旋转机构（430）的方式，第一旋转机构控制第一旋翼系统旋转以产生使无人机飞行的推力。主动力装置还可以配置为第二旋翼系统（510）的方式，第二旋翼系统包含旋翼（511）和桨盘倾斜机构（512A），桨盘倾斜机构可以控制旋翼的桨盘相对于机身转动以产生使无人机飞行的推力。第一旋翼系统或第二旋翼系统设于机身内部。稳定器能够输出使机身旋转的力矩和/或使无人机平移的推力。该全景摄像无人机可拍摄720°全景影像，在飞行过程中机身姿态可以保持在预设的范围内，保证所拍摄的全景影像的稳定性。