Patents by Inventor Adam Warmoth

Adam Warmoth 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).

  • Publication number: 20210350479
    Abstract: Systems and methods for communicating with secondary users of a transportation service are provided. A method can include obtaining a request for a transportation service including an aerial transport of a first user from a first user device associated with the first user. The method can include generating a first multi-modal transportation itinerary for facilitating the aerial transport for the first user. The method can include obtaining data indicative of a second user that is to travel with the first user for at least a portion of the first multi-modal transportation itinerary and determining a second multi-modal transportation itinerary for facilitating the aerial transport for the second user. The method can include communicating passenger itinerary data indicative of the second multi-modal transportation itinerary to a second user device associated with the second user.
    Type: Application
    Filed: May 5, 2021
    Publication date: November 11, 2021
    Inventors: Raphael Max Lurie, Nishit Tewari, Varun Rau, Adam Warmoth, Kevin Tian
  • Publication number: 20210304347
    Abstract: The present disclosure provides systems and methods for systems and methods for generating potential flight plans to be used by a ride sharing network, including dynamic and/or automated changes to flight plans that have been engaged with passengers based on real-time information. In particular, the systems and methods of the present disclosure can operate to generate a fleet-level set of potential flight plans which comply with one or more constraints for a fleet of aircraft. The potential flight plans can be exposed into and used by a ride sharing network to provide transportation to users.
    Type: Application
    Filed: March 25, 2021
    Publication date: September 30, 2021
    Inventors: Eric Richard Mueller, Bogu Wei, Igor Dolgov, Raphael Max Lurie, Adam Warmoth, Kellen Christopher Mollahan, Karl Weston Schulz
  • Publication number: 20210241234
    Abstract: Systems and methods for facilitating a multi-modal transportation service are provided. The method includes obtaining a request for an aerial transport from a user via user device and generating a multi-modal transportation itinerary for the user to facilitate the aerial transport of the user. The method includes determining a state change indicative of the progress of the user through the transportation service and adjusting an aerial software application running on an aerial device associated with an aerial service provider based on the state change. The method includes determining a subsequent state change occurring after the state change, determining a ground vehicle to provide a ground transportation for the user during another leg of the multi-modal transportation service based on the subsequent state, and adjusting a ground software application running on a ground device associated with the ground vehicle service provider based on the subsequent state change.
    Type: Application
    Filed: April 2, 2020
    Publication date: August 5, 2021
    Inventors: Kevin Tian, Adam Warmoth, Hasrat Godil, Nikhil Goel, Varun Rau, Shabnam Emdadi, Raphael Max Lurie
  • Publication number: 20210201686
    Abstract: Systems and methods for communicating aircraft sensory cues are provided. A method can include obtaining aerial vehicle data and facility data for an aerial portion of a multi-modal transportation service. The method can include determining a plurality of sensory cues indicative of information for the aerial portion of the transportation service such as a safe path across a landing pad of the facility, a seating assignment for a passenger, etc. The method can include communicating sensory data indicative of the plurality of sensory cues to at least one of a facility computing system associated with the facility or an aerial computing system associated with the at least one aerial vehicle. The facility computing system and/or aerial computing system can output the sensory cue(s) to at least one passenger or operator of the aerial portion of the multi-modal transportation service in, for example, the facility's landing area.
    Type: Application
    Filed: December 18, 2020
    Publication date: July 1, 2021
    Inventors: Ian Andreas Villa, Matthew Derkach, Philipp Haban, Adam Warmoth, John Conway Badalamenti
  • Publication number: 20210075792
    Abstract: The present disclosure provides systems and methods for real-time planning and fulfillment of multi-modal transportation services in a multi-modal ride sharing network. In particular, aspects of the present disclosure are directed to a computing system that creates an end-to-end multi-modal itinerary responsive to a user request for transportation service between an origin and a destination. The multi-modal itinerary can include two or more transportation legs that include travel via two or more different transportation modalities such as, as examples, via a car and via an aircraft.
    Type: Application
    Filed: November 9, 2020
    Publication date: March 11, 2021
    Inventors: Kevin Tian, Adam Warmoth, Raphael Max Lurie, Hasrat Godil, Nikhil Goel
  • Patent number: 10913528
    Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating, luggage placement, and/or positions of internal components are not coordinated. Among other advantages, dynamically assigning the payloads and adjusting components of the VTOL aircraft can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
    Type: Grant
    Filed: February 11, 2019
    Date of Patent: February 9, 2021
    Assignee: UBER TECHNOLOGIES, INC.
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson
  • Patent number: 10837786
    Abstract: The present disclosure provides systems and methods for real-time planning and fulfillment of multi-modal transportation services in a multi-modal ride sharing network. In particular, aspects of the present disclosure are directed to a computing system that creates an end-to-end multi-modal itinerary responsive to a user request for transportation service between an origin and a destination. The multi-modal itinerary can include two or more transportation legs that include travel via two or more different transportation modalities such as, as examples, via a car and via an aircraft.
    Type: Grant
    Filed: February 10, 2020
    Date of Patent: November 17, 2020
    Assignee: Uber Technologies, Inc.
    Inventors: Kevin Tian, Adam Warmoth, Raphael Max Lurie, Hasrat Godil, Nikhil Goel
  • Publication number: 20200354064
    Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating and/or luggage placement is not coordinated. Among other advantages, dynamically assigning the VTOL aircraft payloads can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
    Type: Application
    Filed: July 22, 2020
    Publication date: November 12, 2020
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson, Jeffrey A. Holden
  • Publication number: 20200300644
    Abstract: The present disclosure provides systems and methods for real-time planning and fulfillment of multi-modal transportation services in a multi-modal ride sharing network. In particular, aspects of the present disclosure are directed to a computing system that creates an end-to-end multi-modal itinerary responsive to a user request for transportation service between an origin and a destination. The multi-modal itinerary can include two or more transportation legs that include travel via two or more different transportation modalities such as, as examples, via a car and via an aircraft.
    Type: Application
    Filed: February 10, 2020
    Publication date: September 24, 2020
    Inventors: Kevin Tian, Adam Warmoth, Raphael Max Lurie, Hasrat Godil, Nikhil Goel
  • Patent number: 10759537
    Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating and/or luggage placement is not coordinated. Among other advantages, dynamically assigning the VTOL aircraft payloads can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
    Type: Grant
    Filed: June 26, 2019
    Date of Patent: September 1, 2020
    Assignee: UBER TECHNOLOGIES, INC.
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson, Jeffrey A. Holden
  • Patent number: 10752363
    Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating and/or luggage placement is not coordinated. Among other advantages, dynamically assigning the VTOL aircraft payloads can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
    Type: Grant
    Filed: November 1, 2018
    Date of Patent: August 25, 2020
    Assignee: UBER TECHNOLOGIES, INC.
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson, Jeffrey A. Holden
  • Publication number: 20190337614
    Abstract: An aircraft with a forward swept wing is configured to transition between vertical flight and forward flight. The aircraft includes propellers attached laterally along the wing. The propellers may be stacked propellers with two or more co-rotating rotors. The aircraft also includes booms attached along the wing and at each free end of the wing. The booms can include boom control effectors configured to direct airflow below a propeller. The aircraft includes one or more cruise propellers, configured to operate during forward flight to generate lift. The aircraft can also include control surfaces on the wings and tail that may tilt during takeoff and landing to yaw the vehicle.
    Type: Application
    Filed: March 18, 2019
    Publication date: November 7, 2019
    Inventors: Ian Andreas Villa, Mark Moore, Adam Warmoth, John Conway Badalamenti, David Lane Josephson
  • Publication number: 20190315471
    Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating and/or luggage placement is not coordinated. Among other advantages, dynamically assigning the VTOL aircraft payloads can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
    Type: Application
    Filed: June 26, 2019
    Publication date: October 17, 2019
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson, Jeffrey A. Holden
  • Publication number: 20190135425
    Abstract: A vertical landing and take-off aircraft VTOL transitions from a vertical takeoff state to a cruise state where the vertical takeoff state uses propellers to generate lift and the cruise state uses wings to generate lift. The aircraft has an M-wing configuration with propellers located on the wingtip nacelles, wing booms, and tail boom. The wing boom and/or the tail boom can include boom control effectors. Hinged control surfaces on the wings, tail boom, and tail tilt during takeoff and landing to yaw the vehicle. The boom control effectors, cruise propellers, stacked propellers, and control surfaces can have different positions during different modes of operation in order to control aircraft movement and mitigate noise generated by the aircraft.
    Type: Application
    Filed: November 3, 2018
    Publication date: May 9, 2019
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson
  • Publication number: 20190135413
    Abstract: An aircraft can include a stacked propeller to generate lift during assent and descent. The stacked propeller includes a first propeller and a second propeller that co-rotate about an axis of rotation. In one embodiment, the blades are coupled to a rotor mast that contains an internal cavity. In one mode of operation, the first propeller and/or the second propeller can be stored in the internal cavity in order to reduce drag during flight. The aircraft can include one or more stacked propellers, such as a port propeller and a starboard propeller, which rotate in opposite directions during one or more modes of flight.
    Type: Application
    Filed: November 3, 2018
    Publication date: May 9, 2019
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson
  • Publication number: 20190135408
    Abstract: The disclosure generally relates to aircraft vehicles, specifically vertical takeoff and landing (VTOL) aircraft that include propellers. A propeller is coupled to a boom and the boom includes a boom control effector. The boom control effector is configured to direct the airflow behind or below the propeller. The boom control effector can be configured to control the yaw movement of the aircraft and mitigate noise from the propeller. A boom control effector can be a single effector or a split effector. The split effector may operate in conjunction with a boom that operates as a resonator to reduce noise produced by the propeller.
    Type: Application
    Filed: November 3, 2018
    Publication date: May 9, 2019
    Inventors: Mark Moore, John Conway Badalamenti, Ian Villa, Adam Warmoth, David Josephson