Patents by Inventor Jerry Daniels
Jerry Daniels 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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Publication number: 20240079739Abstract: An electrical connection system includes a first electrical contact, and a second electrical contact joined directly to the first electrical contact. The first electrical contact is configured to flex relative to the second electrical contact along a first axis, and configured to flex relative to the first electrical contact along a second axis.Type: ApplicationFiled: February 3, 2023Publication date: March 7, 2024Inventors: Caleb Wang, Patrick Daniel Maguire, Jerry Lan
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Publication number: 20230303244Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: ApplicationFiled: August 22, 2022Publication date: September 28, 2023Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Patent number: 11420737Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: GrantFiled: December 11, 2020Date of Patent: August 23, 2022Assignee: xCraft Enterprises, Inc.Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20220177130Abstract: Various embodiments of systems, apparatus, and/or methods are described for enhanced responsiveness in responding to an emergency situation using unmanned aerial vehicles (drones). Drones are fully autonomous in that they are operated without human intervention from a pilot, an operator, or other personnel. The disclosed drone utilizes movable access doors to provide the capability of vertically takeoff and landing. The drone also includes an emergency recovery system including a mechanism to deploy a parachute in an event of a failure of the on-board autopilot. Also disclosed herein is a drone port that provides an IR-based docking mechanism for precision landing of the drone, with a very low margin of error. Additionally, the drone port includes pads that provide automatic charge to the drone's batteries by contact-based charging via the drone's landing gear legs.Type: ApplicationFiled: February 23, 2022Publication date: June 9, 2022Inventors: Philip E. Burks, James Nipp, Jerry Daniel Claridge, Paul Miller
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Patent number: 11279481Abstract: Various embodiments of systems, apparatus, and/or methods are described for enhanced responsiveness in responding to an emergency situation using unmanned aerial vehicles (drones). Drones are fully autonomous in that they are operated without human intervention from a pilot, an operator, or other personnel. The disclosed drone utilizes movable access doors to provide the capability of vertically takeoff and landing. The drone also includes an emergency recovery system including a mechanism to deploy a parachute in an event of a failure of the on-board autopilot. Also disclosed herein is a drone port that provides an IR-based docking mechanism for precision landing of the drone, with a very low margin of error. Additionally, the drone port includes pads that provide automatic charge to the drone's batteries by contact-based charging via the drone's landing gear legs.Type: GrantFiled: May 11, 2018Date of Patent: March 22, 2022Assignee: PHIRST TECHNOLOGIES, LLCInventors: Philip E. Burks, James Nipp, Jerry Daniel Claridge, Paul Miller
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Publication number: 20220024561Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: ApplicationFiled: December 11, 2020Publication date: January 27, 2022Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20200102093Abstract: A method for deploying a drone including transporting a drone from a first location to a second location with a vehicle and supplying electricity from the vehicle to the drone while the drone is being transported. A launch command can be initiated from within the vehicle to direct the drone to ascend and hover above the vehicle. The drone can be transported in a drone port mounted to the vehicle.Type: ApplicationFiled: October 1, 2019Publication date: April 2, 2020Inventors: Jerry Daniel Claridge, Phil Burks
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Patent number: 10479500Abstract: This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an airframe with rotors and an adjustable cradle to attach a computing device. The computing device, such as a smart phone, tablet, MP3 player, or the like, may provide the necessary avionics and computing equipment to control the UAV autonomously. For example, the adjustable cradle may be extended to fit a tablet or other large computing device, or retracted to fit a smart phone or other small computing device. Thus, the adjustable cradle may provide for the attachment and use of a plurality of different computing devices in conjunction with a single airframe. Additionally the UAV may comprise adjustable arms to assist in balancing the load of the different computing devices and/or additional equipment attached to the airframe.Type: GrantFiled: August 21, 2017Date of Patent: November 19, 2019Assignee: xCraft Enterprises, Inc.Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20190135428Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: ApplicationFiled: June 11, 2018Publication date: May 9, 2019Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20180327091Abstract: Various embodiments of systems, apparatus, and/or methods are described for enhanced responsiveness in responding to an emergency situation using unmanned aerial vehicles (drones). Drones are fully autonomous in that they are operated without human intervention from a pilot, an operator, or other personnel. The disclosed drone utilizes movable access doors to provide the capability of vertically takeoff and landing. The drone also includes an emergency recovery system including a mechanism to deploy a parachute in an event of a failure of the on-board autopilot. Also disclosed herein is a drone port that provides an IR-based docking mechanism for precision landing of the drone, with a very low margin of error. Additionally, the drone port includes pads that provide automatic charge to the drone's batteries by contact-based charging via the drone's landing gear legs.Type: ApplicationFiled: May 11, 2018Publication date: November 15, 2018Inventors: Philip E. Burks, James Nipp, Jerry Daniel Claridge, Paul Miller
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Publication number: 20180290744Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: ApplicationFiled: June 11, 2018Publication date: October 11, 2018Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20180170539Abstract: This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an airframe with rotors and an adjustable cradle to attach a computing device. The computing device, such as a smart phone, tablet, MP3 player, or the like, may provide the necessary avionics and computing equipment to control the UAV autonomously. For example, the adjustable cradle may be extended to fit a tablet or other large computing device, or retracted to fit a smart phone or other small computing device. Thus, the adjustable cradle may provide for the attachment and use of a plurality of different computing devices in conjunction with a single airframe. Additionally the UAV may comprise adjustable arms to assist in balancing the load of the different computing devices and/or additional equipment attached to the airframe.Type: ApplicationFiled: August 21, 2017Publication date: June 21, 2018Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Patent number: 9994313Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: GrantFiled: November 26, 2014Date of Patent: June 12, 2018Assignee: XCraft Enterprises, LLCInventors: Jerry Daniel Claridge, Charles Fischer Manning
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Patent number: 9738380Abstract: This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an airframe with rotors and an adjustable cradle to attach a computing device. The computing device, such as a smart phone, tablet, MP3 player, or the like, may provide the necessary avionics and computing equipment to control the UAV autonomously. For example, the adjustable cradle may be extended to fit a tablet or other large computing device, or retracted to fit a smart phone or other small computing device. Thus, the adjustable cradle may provide for the attachment and use of a plurality of different computing devices in conjunction with a single airframe. Additionally the UAV may comprise adjustable arms to assist in balancing the load of the different computing devices and/or additional equipment attached to the airframe.Type: GrantFiled: March 16, 2015Date of Patent: August 22, 2017Assignee: XCraft Enterprises, LLCInventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20160376004Abstract: This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an airframe with rotors and an adjustable cradle to attach a computing device. The computing device, such as a smart phone, tablet, MP3 player, or the like, may provide the necessary avionics and computing equipment to control the UAV autonomously. For example, the adjustable cradle may be extended to fit a tablet or other large computing device, or retracted to fit a smart phone or other small computing device. Thus, the adjustable cradle may provide for the attachment and use of a plurality of different computing devices in conjunction with a single airframe. Additionally the UAV may comprise adjustable arms to assist in balancing the load of the different computing devices and/or additional equipment attached to the airframe.Type: ApplicationFiled: March 16, 2015Publication date: December 29, 2016Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20160144957Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.Type: ApplicationFiled: November 26, 2014Publication date: May 26, 2016Inventors: Jerry Daniel Claridge, Charles Fischer Manning
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Publication number: 20160053181Abstract: The disclosure provides a gas collection apparatus. The present apparatus may be used, for example, in a system for producing biocoal or biochar or bio-oil from biomass. The present gas collection apparatus may be part of a thermochemical biomass reactor. The present gas collection apparatus may be part of a syngas management system. Embodiments of the present disclosure relate to a gas collection apparatus for fluidly communicating with a retort of a biomass reactor, said collection apparatus comprising two or more gas collection pipes in fluid communication with spaced apart sections of said retort; and a gas collection manifold in fluid communication with said pipes. The gas collection apparatus is designed such that the gases collected by one pipe do not mix with those collected by another within the piping network.Type: ApplicationFiled: March 20, 2014Publication date: February 25, 2016Inventors: Jerry Daniel Ericsson, Daniel Lennart Ericsson
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Publication number: 20160053182Abstract: The present disclosure provides, at least in part, a system for pyrolysis of biomass, the system comprising: (a) a reactor having a retort extending therethrough, said retort comprising a conveyor, an inlet, and an outlet; the reactor further comprising at least one thermosensor, the thermosensor capable of generating a signal when the temperature is above optimal levels; (b) a heating system adapted to heat the reactor; (c) a syn-gas management system; the management system comprising a syn-gas storage tank having an inlet and an outlet, said inlet in fluid communication with the reactor, and said outlet in fluid communication with the heating system and syn-gas outlet such as a flare or storage tank wherein the communication is controlled via a valve configurable between at least a first position where flow is directed to the heating system and a second position where flow is directed to the flare pipe; and (d) a controller in communication with the thermosensor and the valve; wherein the controller switcheType: ApplicationFiled: March 20, 2014Publication date: February 25, 2016Inventors: Jerry Daniel Ericsson, Daniel Lennart Ericsson, Jared Luke Taylor
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Patent number: 8335784Abstract: Methods, systems, graphical user interfaces, and computer-readable media for visually searching and exploring a set of objects are provided. A computer system executes a method that generates three-dimensional representations or two-dimensional representations for a set of objects in response to a user interaction with an interface that displays the three-dimensional representations or the two-dimensional representations. The interface includes filter controls, sorting controls, and classification controls, which are dynamically altered based on the content of a user query or the attributes of the objects in the three-dimensional representations or two-dimensional representations.Type: GrantFiled: August 31, 2009Date of Patent: December 18, 2012Assignee: Microsoft CorporationInventors: Zachary Mark Gutt, Paul Ronald Ray, Rodney Coleman Edwards, Darwin Kengo Yamamoto, Hady Moustafa Abou El Kheir, Brian Whalen MacDonald, Jerry Daniel Bain
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Publication number: 20110055203Abstract: Methods, systems, graphical user interfaces, and computer-readable media for visually searching and exploring a set of objects are provided. A computer system executes a method that generates three-dimensional representations or two-dimensional representations for a set of objects in response to a user interaction with an interface that displays the three-dimensional representations or the two-dimensional representations. The interface includes filter controls, sorting controls, and classification controls, which are dynamically altered based on the content of a user query or the attributes of the objects in the three-dimensional representations or two-dimensional representations.Type: ApplicationFiled: August 31, 2009Publication date: March 3, 2011Applicant: Microsoft CorporationInventors: ZACHARY MARK GUTT, PAUL RONALD RAY, RODNEY COLEMAN EDWARDS, DARWIN KENGO YAMAMOTO, HADY MOUSTAFA ABOU EL KHEIR, BRIAN WHALEN MACDONALD, JERRY DANIEL BAIN