PROPELLER BLADE LEADING EDGE SERRATIONS FOR IMPROVED SOUND CONTROL

    公开(公告)号:US20170174319A1

    公开(公告)日:2017-06-22

    申请号:US14975265

    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.

    Geometrically reconfigurable propellers
    24.
    发明授权
    Geometrically reconfigurable propellers 有权
    几何可重构螺旋桨

    公开(公告)号:US09592910B1

    公开(公告)日:2017-03-14

    申请号:US14975167

    申请日:2015-12-18

    Abstract: An aerial vehicle may be equipped with propellers having reconfigurable geometries. Such propellers may have blade tips or other features that may be adjusted or reconfigured while the aerial vehicle is operating, on any basis. Propellers having reconfigurable blade tips joined to blade roots may cause the blade tips to be aligned with the blade roots, or substantially perpendicular to the blade roots, e.g., in order to counter adverse effects of tip vortices, or at any intervening angle. The propellers may be reconfigured at predetermined times during operation of an aerial vehicle, or upon sensing one or more operational characteristics or environmental conditions, as may be desired or required.

    Abstract translation: 飞行器可以配备具有可重构几何形状的螺旋桨。 这样的螺旋桨可以具有叶片尖端或者其他特征,其可以在空中飞行器运行时在任何基础上进行调整或重新配置。 具有连接到叶片根部的可重新配置的叶片尖端的螺旋桨可以导致叶片尖端与叶片根部对准,或者基本上垂直于叶片根部,例如为了抵消尖端旋涡的不利影响或以任何中间角度。 推进器可以在飞行器的操作期间的预定时间重新配置,或者可以根据期望或需要感测一个或多个操作特性或环境条件。

    Propeller blade indentations for improved aerodynamic performance and sound control

    公开(公告)号:US10399665B2

    公开(公告)日:2019-09-03

    申请号:US15968137

    申请日:2018-05-01

    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.

    Propeller blade leading edge serrations for improved sound control

    公开(公告)号:US10099773B2

    公开(公告)日:2018-10-16

    申请号:US14975265

    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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