Swappable avionics for unmanned aerial vehicle
First Claim
1. An unmanned aerial vehicle (UAV) comprising:
- a propulsion system comprising;
a propulsion frame;
a plurality of propulsion units coupled to the propulsion frame, each propulsion unit of the plurality of propulsion units including a rotor, a speed controller, and a motor; and
a propulsion port to provide at least one of power or control data to the plurality of propulsion units;
a detachable avionics system comprising;
an avionics frame;
a housing to enclose avionics components within the avionics frame;
a propulsion coupling feature to selectively couple to the propulsion system, the propulsion coupling feature to toggle between a first position that engages the propulsion system and a second position that is free from engaging the propulsion system;
an avionics port including at least a data port and a power port, the avionics port to couple to the propulsion port of the propulsion system to provide the at least one of the power or the control data;
a battery coupled to at least one of the detachable avionics system or the propulsion system, the battery to provide power to the avionics port;
a cargo bay that includes a door and that is coupled to at least one of the detachable avionics system or the propulsion system, the cargo bay configured to transport and selectively release packages from the UAV; and
control logic to selectively open the door to deposit the packages from the cargo bay at specific locations during a flight to be traversed by the UAV.
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Accused Products
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.
33 Citations
20 Claims
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1. An unmanned aerial vehicle (UAV) comprising:
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a propulsion system comprising; a propulsion frame; a plurality of propulsion units coupled to the propulsion frame, each propulsion unit of the plurality of propulsion units including a rotor, a speed controller, and a motor; and a propulsion port to provide at least one of power or control data to the plurality of propulsion units; a detachable avionics system comprising; an avionics frame; a housing to enclose avionics components within the avionics frame; a propulsion coupling feature to selectively couple to the propulsion system, the propulsion coupling feature to toggle between a first position that engages the propulsion system and a second position that is free from engaging the propulsion system; an avionics port including at least a data port and a power port, the avionics port to couple to the propulsion port of the propulsion system to provide the at least one of the power or the control data; a battery coupled to at least one of the detachable avionics system or the propulsion system, the battery to provide power to the avionics port; a cargo bay that includes a door and that is coupled to at least one of the detachable avionics system or the propulsion system, the cargo bay configured to transport and selectively release packages from the UAV; and control logic to selectively open the door to deposit the packages from the cargo bay at specific locations during a flight to be traversed by the UAV. - View Dependent Claims (2, 3, 4, 5)
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6. An avionics device comprising:
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a frame; a housing, the housing at least partially enclosing interior avionics components within the frame; a plurality of fins coupled to an exterior of the housing to dissipate heat from an interior of the housing; a first coupling feature to selectively couple the avionics device to a propulsion system to form an unmanned aerial vehicle (UAV); and a first data interface configured to couple to at least a corresponding second data interface of the propulsion system, wherein the housing forms a fuselage of the UAV after assembly of the UAV. - View Dependent Claims (7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A system comprising:
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a propulsion component comprising; a plurality of propulsion units, individual propulsion units of the plurality of propulsion units including a rotor and a motor; and a propulsion port to provide at least one of power or control data to the plurality of propulsion units; a detachable avionics device comprising; a frame; a housing to at least partially enclose avionics components within the frame; a propulsion coupling feature to selectively couple to the propulsion component; and an avionics port including at least a data port and a power port, the avionics port to couple to the propulsion port of the propulsion component to provide the at least one of the power or the control data; and a battery coupled to at least one of the detachable avionics device or the propulsion component, the battery to provide power to the avionics port, wherein the propulsion component and the detachable avionics device form an unmanned aerial vehicle (UAV) and the housing forms a fuselage of the UAV after assembly of the UAV. - View Dependent Claims (17, 18, 19, 20)
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Specification