Patents by Inventor John R. Foggia
John R. Foggia has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 11713136Abstract: Disclosed are unmanned aerial vehicle (UAV) positioning mechanisms for moving a UAV across a surface. The positioning mechanisms comprise a first guide assembly arranged opposite to a second guide assembly. A drive system is arranged to move the first guide assembly towards the second guide assembly and guide the UAV from a first position to a second position.Type: GrantFiled: March 12, 2020Date of Patent: August 1, 2023Assignee: Flirtey Holdings, Inc.Inventors: John R Foggia, Jess Hayden, Joseph Rinaldi, Matthew Sweeny
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Publication number: 20220246041Abstract: Embodiments described herein are concerned with system for identifying an aerial vehicle. The system comprises: a radar sub-system, the radar sub-system comprising at least one radar connectable to a static support member and a transceiver configured to transmit data indicative of one or more targets identified by the radar within an airspace; a receiver arranged to receive the data indicative of one or more targets identified by the radar; and a processing system configured to process said data, whereby to identify at least one aerial vehicle. In some embodiments the radar comprises a marine radar.Type: ApplicationFiled: February 17, 2022Publication date: August 4, 2022Inventors: John R FOGGIA, Allison Jade MALLOY, Matthew SWEENY
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Patent number: 11338923Abstract: Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.Type: GrantFiled: November 25, 2019Date of Patent: May 24, 2022Assignee: Flirtey Holdings, Inc.Inventors: Matthew Sweeny, Michel Fathallah, Tom Bass, Kranthi Baddam, John R. Foggia
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Publication number: 20210224739Abstract: Disclosed are transportable unmanned aerial vehicle (UAV) facilities. The facilities comprise a housing having an ingress port arranged to receive a payload for delivery by a UAV. The UAV facility is arranged to determine whether the payload corresponds to a delivery consignment based upon a comparison of one or more determined physical characteristics of the payload with one or more expected characteristics of the delivery consignment.Type: ApplicationFiled: March 10, 2021Publication date: July 22, 2021Inventors: Matthew SWEENY, Jess HAYDEN, Joseph RINALDI, John R. FOGGIA
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Publication number: 20210197982Abstract: Disclosed are unmanned aerial vehicle (UAV) facilities suitable for use by both emergency and non-emergency UAVs. The facilities comprise a housing having first and second moveable platforms. A cover is arranged above the second moveable platform. A drive system operates the first and second moveable platforms and the cover.Type: ApplicationFiled: March 11, 2021Publication date: July 1, 2021Inventors: Matthew SWEENY, John R. FOGGIA, Jess HAYDEN, Joseph RINALDI
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Publication number: 20210107646Abstract: In an embodiment an unmanned aerial vehicle comprises a central body and a plurality of support structures extending outwards from the central body. Each support structure supports a rotor blade assembly and is provided with one or more deformable portions. The rotor blade assembly defines a rotational axis of one or more rotor blades associated with the rotor blade assembly.Type: ApplicationFiled: December 7, 2020Publication date: April 15, 2021Inventors: Matthew SWEENY, John R FOGGIA, Jeremy FRIES
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Publication number: 20200331618Abstract: Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.Type: ApplicationFiled: November 25, 2019Publication date: October 22, 2020Inventors: Matthew SWEENY, Michel FATHALLAH, Tom BASS, Kranthi BADDAM, John R. FOGGIA
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Patent number: 10703494Abstract: Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.Type: GrantFiled: October 14, 2016Date of Patent: July 7, 2020Assignee: Flirtey Holdings, Inc.Inventors: Matthew Sweeny, Michel Fathallah, Tom Bass, Kranthi Baddam, John R. Foggia
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Publication number: 20200207485Abstract: Disclosed are transportable unmanned aerial vehicle (UAV) facilities. The facilities comprise a housing for holding a UAV, where the housing defines a landing area for the UAV. The facilities also comprise a structure for reducing wind speed across the landing area.Type: ApplicationFiled: March 12, 2020Publication date: July 2, 2020Inventors: John R FOGGIA, Jess HAYDEN, Joseph RINALDI, Matthew SWEENY
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Publication number: 20200207484Abstract: Disclosed are unmanned aerial vehicle (UAV) positioning mechanisms for moving a UAV across a surface. The positioning mechanisms comprise a first guide assembly arranged opposite to a second guide assembly. A drive system is arranged to move the first guide assembly towards the second guide assembly and guide the UAV from a first position to a second position.Type: ApplicationFiled: March 12, 2020Publication date: July 2, 2020Inventors: John R FOGGIA, Jess HAYDEN, Joseph RINALDI, Matthew SWEENY
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Publication number: 20200209375Abstract: Embodiments described herein are concerned with system for identifying an aerial vehicle. The system comprises: a radar sub-system, the radar sub-system comprising at least one radar connectable to a static support member and a transceiver configured to transmit data indicative of one or more targets identified by the radar within an airspace; a receiver arranged to receive the data indicative of one or more targets identified by the radar; and a processing system configured to process said data, whereby to identify at least one aerial vehicle. In some embodiments the radar comprises a marine radar.Type: ApplicationFiled: March 12, 2020Publication date: July 2, 2020Inventors: John R FOGGIA, Allison Jade MALLOY, Matthew SWEENY
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Publication number: 20200207474Abstract: Embodiments described herein are methods and systems that relate to delivery of a payload to a particular delivery surface. A payload is collected at a first physical location using a retractable delivery mechanism of a UAV, and the UAV flies to a designated second physical location, whereupon sensor data is obtained using one or more sensors of the UAV. The sensor data is used to obtain characteristics of an area which may be used as a delivery surface at the second physical location. An actual delivery surface is selected based on criteria in the form of rule data specifying an appropriate delivery surface and the sensor data. Once the delivery surface has been selected the retractable delivery lowers the payload towards the selected delivery surface.Type: ApplicationFiled: March 12, 2020Publication date: July 2, 2020Inventors: John R FOGGIA, Andrianah Jade KILGORE, Matthew SWEENY
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Patent number: 10112721Abstract: Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.Type: GrantFiled: October 14, 2016Date of Patent: October 30, 2018Assignee: Flirtey Holdings, Inc.Inventors: Matthew Sweeny, Michel Fathallah, Tom Bass, Kranthi Baddam, John R. Foggia
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Publication number: 20170158338Abstract: Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.Type: ApplicationFiled: October 14, 2016Publication date: June 8, 2017Inventors: Matthew Sweeny, Michel Fathallah, Tom Bass, Kranthi Baddam, John R. Foggia
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Publication number: 20170106986Abstract: Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.Type: ApplicationFiled: October 14, 2016Publication date: April 20, 2017Inventors: Matthew Sweeny, Michel Fathallah, Tom Bass, Kranthi Baddam, John R. Foggia