Swappable avionics for unmanned aerial vehicle

    公开(公告)号:US10583922B1

    公开(公告)日:2020-03-10

    申请号:US15385669

    申请日:2016-12-20

    Abstract: A configurable unmanned aerial vehicle (UAV) may include swappable avionics that may be selectable for use with other UAV components to build a customized UAV just prior to deployment of the UAV that is configured to deliver a package to a destination. Various factors may be involved in the selection of the avionics, such as an availability of different avionics, payload requirements (size, weight, etc.), environmental conditions along an anticipated route of flight, a region of use of the UAV, compatibility, a distance of the flight, power considerations, security considerations, and/or other factors. The avionics may include various hardware and/or software which may provide control output (e.g., data, power, and/or mechanical) to other components and/or systems, including a propulsion system. Coupling devices may selectively couple the avionics to other components of the UAV, such as to a battery, a cargo bay or package, and/or to a propulsion system.

    Electrical switch for a load in a vehicle

    公开(公告)号:US10115555B1

    公开(公告)日:2018-10-30

    申请号:US14969716

    申请日:2015-12-15

    Abstract: A switch for switching power to a load of a vehicle may be described. In an example, the switch may include a number of members configured to move between switch positions in a predefined order such that a load and a power source are electrically coupled or electrically decoupled via the switch based on the predefined order. In particular, a first member may be configured to move to a first switch position and form a first electrically conductive path having a first electrical property. A second member may be configured to move to a second switch position and form a second electrically conductive path having a second electrical property different from the first electrical property. A third member may be configured to move the second member based on movement of the first member to the first switch position such that movement of the second member to the second switch position may occur based on the movement of the first member to the first switch position.

    UNMANNED AERIAL VEHICLE CONFIGURATION FOR EXTENDED FLIGHT
    6.
    发明申请
    UNMANNED AERIAL VEHICLE CONFIGURATION FOR EXTENDED FLIGHT 有权
    用于扩展飞行的无人驾驶航空器配置

    公开(公告)号:US20160129998A1

    公开(公告)日:2016-05-12

    申请号:US14538570

    申请日:2014-11-11

    Abstract: This disclosure describes a configuration of an unmanned aerial vehicle (UAV) that will facilitate extended flight duration. 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 also includes a pushing motor and propeller assembly that is oriented at approximately ninety degrees to one or more of the lifting motors. When the UAV is moving horizontally, the pushing motor may be engaged and the pushing propeller will aid in the horizontal propulsion of the UAV.

    Abstract translation: 本公开描述了将有助于延长飞行持续时间的无人驾驶飞行器(UAV)的配置。 无人机可能有任何数量的起重马达。 例如,无人机可以包括四台起重电动机(也称为四号机),八台起重马达(八重直升机)等。同样,为了提高水平飞行的效率,无人机还包括一个推动马达和螺旋桨 组件,其定向在一个或多个起重马达上大约九十度。 当无人机水平移动时,推动马达可以接合,推进螺旋桨将有助于无人机的水平推进。

    Unmanned aerial vehicle configuration and deployment

    公开(公告)号:US10717524B1

    公开(公告)日:2020-07-21

    申请号:US15385748

    申请日:2016-12-20

    Abstract: A configurable unmanned aerial vehicle (UAV) may include swappable avionics that may be selectable for use with other UAV components to build a customized UAV just prior to deployment of the UAV that is configured to deliver a package to a destination. Various factors may be involved in the selection of the avionics, such as an availability of different avionics, payload requirements (size, weight, etc.), environmental conditions along an anticipated route of flight, a region of use of the UAV, compatibility, a distance of the flight, power considerations, security considerations, and/or other factors. The avionics may include various hardware and/or software which may provide control output (e.g., data, power, and/or mechanical) to other components and/or systems, including a propulsion system. Coupling devices may selectively couple the avionics to other components of the UAV, such as to a battery, a cargo bay or package, and/or to a propulsion system.

    Identification and position sensor for payload bay

    公开(公告)号:US10179657B1

    公开(公告)日:2019-01-15

    申请号:US15815533

    申请日:2017-11-16

    Abstract: A system including a payload bay having at least one sensor configured to determine the identity of an object being transported in the payload bay and verify that the object is properly seated within the payload bay. As an object is inserted into the payload bay of the vehicle, the sensor(s) detects a pattern located on the side of the object. As the sensor(s) detects the pattern, it transmits information that enables the system to determine both the identity of the object and position of the object within the payload bay. In this way, the sensor(s) enables the system to identify when a wrong object is loaded into the payload bay, and/or when the object is improperly seated within the payload bay.

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