Hierarchal reference system
    41.
    发明授权

    公开(公告)号:US10593218B1

    公开(公告)日:2020-03-17

    申请号:US16522557

    申请日:2019-07-25

    Abstract: Disclosed are systems and methods for reducing the amount of messaging between aerial vehicles and between controllers of aerial vehicles and simplifying aerial vehicle traffic management. In one implementation, a large service area, such as the United States, may be separated into a series of hierarchal regions. Rather than sending notifications to all agents (e.g., aerial vehicles, controllers) in the service area, each agent may subscribe to one or more regions of the hierarchal regions and only receive messages intended for the subscribed regions. In one example, as discussed below, messages for a particular region are only sent to agents subscribed to that region. Other agents within the larger service area do not receive the messages as they may not be relevant to those agents.

    Ducts with airflow channels
    43.
    发明授权

    公开(公告)号:US10407167B1

    公开(公告)日:2019-09-10

    申请号:US15782787

    申请日:2017-10-12

    Abstract: This disclosure describes a configuration of an aerial vehicle, such as an unmanned aerial vehicle, in which one or more of the propellers are positioned within a duct that includes an active airflow channel within the interior of the duct. The active airflow channel actively moves within the duct so that it remains aligned with the tips of the blades of the propeller within the duct. As the propeller and the active airflow channel rotate, at least some of the airflow structures (e.g., vortices) shed from the blades of the propeller are collected by the active airflow channel and channeled away from the propeller so that a following blade of the propeller does not pass through the collected airflow structures.

    Reducing status notifications using a hierarchal reference system

    公开(公告)号:US10403154B1

    公开(公告)日:2019-09-03

    申请号:US15277880

    申请日:2016-09-27

    Abstract: Disclosed are systems and methods for reducing the amount of messaging between aerial vehicles and between controllers of aerial vehicles and simplifying aerial vehicle traffic management. In one implementation, a large service area, such as the United States, may be separated into a series of hierarchal regions. Rather than sending notifications to all agents (e.g., aerial vehicles, controllers) in the service area, each agent may subscribe to one or more regions of the hierarchal regions and only receive messages intended for the subscribed regions. In one example, as discussed below, messages for a particular region are only sent to agents subscribed to that region. Other agents within the larger service area do not receive the messages as they may not be relevant to those agents.

    Static inverse desymmetrized propellers

    公开(公告)号:US10351262B1

    公开(公告)日:2019-07-16

    申请号:US15230223

    申请日:2016-08-05

    Abstract: Techniques for using a sound spectrum to generate models, which identify unmanned aerial vehicle (UAV) configurations, are described herein. The models may be based on components associated with a UAV, and instructions for manufacture of a UAV may be provided. For example, a sound spectrum may be obtained by a computer system which is used to generate one or more models. The one or more models are based in part on components of a UAV and identify UAV configurations that will generate an expected sound within the identified sound spectrum. The UAV configurations identified by the models are used to instruct manufacture of a UAV.

    PROPELLER BLADE TREATMENTS FOR SOUND CONTROL
    47.
    发明申请

    公开(公告)号:US20190210720A1

    公开(公告)日:2019-07-11

    申请号:US14975209

    申请日:2015-12-18

    Abstract: Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation. Disclosed are systems, methods, and apparatus for actively adjusting the position of one or more propeller blade treatments of a propeller blade of an aerial vehicle during operation of the aerial vehicle. For example, the propeller blade may have one or more propeller blade treatments that may be adjusted between two or more positions. Based on the position of the propeller blade treatments, the airflow over the propeller is altered, thereby altering the sound generated by the propeller when rotating. By altering the propeller blade treatments on multiple propeller blades of the aerial vehicle, the different sounds generated by the different propeller blades may effectively cancel, reduce, and/or otherwise alter the total sound generated by the aerial vehicle.

    Unmanned aerial vehicle protective frame configuration

    公开(公告)号:US10293937B2

    公开(公告)日:2019-05-21

    申请号:US15849374

    申请日:2017-12-20

    Abstract: This disclosure describes a configuration of an unmanned aerial vehicle (UAV) that includes a frame that provides both structural support for the UAV and protection for foreign objects that may come into contact with the UAV. The UAV may have any number of lifting motors. For example, the UAV may include four lifting motors (also known as a quad-copter), eight lifting motors (octo-copter), etc. Likewise, to improve the efficiency of horizontal flight, the UAV may also include one or more pushing motor and propeller assemblies that are oriented at approximately ninety degrees to one or more of the lifting motors. When the UAV is moving horizontally, the pushing motor(s) may be engaged and the pushing propeller(s) will aid in the horizontal propulsion of the UAV.

    Propeller blade trailing edge fringes for improved sound control

    公开(公告)号:US10259562B2

    公开(公告)日:2019-04-16

    申请号:US14975274

    申请日:2015-12-18

    Abstract: Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation. Disclosed are systems, methods, and apparatus for actively adjusting the position of one or more propeller blade treatments of a propeller blade of an aerial vehicle during operation of the aerial vehicle. For example, the propeller blade may have one or more propeller blade treatments that may be adjusted between two or more positions. Based on the position of the propeller blade treatments, the airflow over the propeller is altered, thereby altering the sound generated by the propeller when rotating. By altering the propeller blade treatments on multiple propeller blades of the aerial vehicle, the different sounds generated by the different propeller blades may effectively cancel, reduce, and/or otherwise alter the total sound generated by the aerial vehicle.

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