Vertical takeoff and landing (VTOL) small unmanned aerial system for monitoring oil and gas pipelines
First Claim
1. A system comprising:
- an aircraft, including;
a plurality of wing unit propellers for vertical takeoff and landing;
a control system for controlling flight of the aircraft autonomously;
a sensor section; and
a power manager unit; and
a docking platform, including;
a data exchange unit, wherein the data exchange unit communicates with the sensor section of the aircraft during docking of the aircraft at the docking platform; and
a power supply unit that supplies power to the power manager unit of the aircraft during docking of the aircraft at the docking platform; and
wherein;
the sensor section of the aircraft performs an auto-sensing of data transfer task completion and battery charge completion for resuming travel to a next docking platform.
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Accused Products
Abstract
Extended-range monitoring and surveillance of facilities and infrastructure—such as oil, water, and gas pipelines and power lines—employs autonomous vertical take-off and landing (VTOL) capable, small unmanned aerial system (sUAS) aircraft and docking platforms for accommodating the sUAS aircraft. Monitoring and surveillance of facilities using one or more embodiments may be performed continually by the sUAS flying autonomously along a pre-programmed flight path. The sUAS aircraft may have an integrated gas collector and analyzer unit, and capability for downloading collected data and analyzer information from the sUAS aircraft to the docking platforms. The gas collector and analyzer unit may provide remote sensing and in-situ investigation of leaks and other environmental concerns as part of a “standoff” (e.g., remote from operators of the system or the facilities) survey that can keep field operators out of harm'"'"'s way and monitor health of the environment.
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Citations
20 Claims
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1. A system comprising:
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an aircraft, including; a plurality of wing unit propellers for vertical takeoff and landing; a control system for controlling flight of the aircraft autonomously; a sensor section; and a power manager unit; and a docking platform, including; a data exchange unit, wherein the data exchange unit communicates with the sensor section of the aircraft during docking of the aircraft at the docking platform; and a power supply unit that supplies power to the power manager unit of the aircraft during docking of the aircraft at the docking platform; and
wherein;the sensor section of the aircraft performs an auto-sensing of data transfer task completion and battery charge completion for resuming travel to a next docking platform. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A system comprising:
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an aircraft, including; a plurality of wing unit propellers for vertical takeoff and landing; a control system for controlling flight of the aircraft autonomously; a sensor section; and a power manager unit; and a docking platform, including; a data exchange unit, wherein the data exchange unit communicates with the sensor section of the aircraft during docking of the aircraft at the docking platform; a power supply unit that supplies power to the power manager unit of the aircraft during docking of the aircraft at the docking platform; and a thermal wire mesh for maintaining all-weather operability of the platform with the aircraft.
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9. A method comprising:
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controlling, both autonomously and from a remote operator location, an aircraft having a plurality of wing unit propellers for vertical takeoff and landing; operating sensors from the aircraft along a flight path of the aircraft, wherein; operating the sensors further comprises detecting a level of gas in the atmosphere along the flight path; linking the aircraft to a network providing cloud computing for in-situ evaluation of the detected level of gas in the atmosphere along the flight path; recording data from the sensors; autonomously landing the aircraft at a docking platform; communicating the recorded data from the aircraft to the docking platform during docking of the aircraft at the docking platform; and recharging aircraft batteries from a power supply provided by the docking platform during docking of the aircraft at the docking platform. - View Dependent Claims (10, 11, 12)
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13. A method comprising:
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controlling, both autonomously and from a remote operator location, an aircraft having a plurality of wing unit propellers for vertical takeoff and landing; using GPS positioning guidance to direct the aircraft to a desired location of a pipeline; operating sensors from the aircraft along a flight path of the aircraft; recording data from the sensors, including; recording high resolution thermal and optical images by the aircraft; autonomously landing the aircraft at a docking platform; communicating the recorded data from the aircraft to the docking platform during docking of the aircraft at the docking platform; and recharging aircraft batteries from a power supply provided by the docking platform during docking of the aircraft at the docking platform. - View Dependent Claims (14)
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15. A method comprising:
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controlling, both autonomously and from a remote operator location, an aircraft having a plurality of wing unit propellers for vertical takeoff and landing; operating sensors from the aircraft along a flight path of the aircraft, including; collecting a volume of gas with a gas collection fixture mounted on the aircraft, and injecting the gas into a gas detector unit for detection and analysis; recording data from the sensors; autonomously landing the aircraft at a docking platform; communicating the recorded data from the aircraft to the docking platform during docking of the aircraft at the docking platform; and recharging aircraft batteries from a power supply provided by the docking platform during docking of the aircraft at the docking platform. - View Dependent Claims (16)
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17. A method of autonomous landing of a small unmanned aerial system (sUAS) aircraft, comprising:
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autonomously landing the sUAS aircraft using global positioning system (GPS) on a landing platform large enough to compensate for inaccuracy in GPS positioning; providing guidance of the sUAS aircraft toward the center of the landing platform using the shape of the landing platform; and moving the sUAS aircraft using a force toward the center of the landing platform under the shape-provided guidance, to a position that provides electrical contacts for charging a battery of the sUAS aircraft. - View Dependent Claims (18, 19, 20)
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Specification