Patents Examined by Christopher P. Ellis
  • Patent number: 11001378
    Abstract: A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream. At least one tail conduit is fluidly coupled to the generator. First and second fore ejectors are coupled to the main body and respectively coupled to a starboard side and port side of the vehicle. The fore ejectors respectively comprise an outlet structure out of which fluid flows. At least one tail ejector is fluidly coupled to the tail conduit. The tail ejector comprises an outlet structure out of which fluid flows. A primary airfoil element includes a closed wing having a leading edge and a trailing edge. The leading and trailing edges of the closed wing define an interior region. The at least one propulsion device is at least partially disposed within the interior region.
    Type: Grant
    Filed: June 27, 2018
    Date of Patent: May 11, 2021
    Assignee: JETOPTERA, INC.
    Inventor: Andrei Evulet
  • Patent number: 11001366
    Abstract: Some embodiments described herein relate to a wing that is coupled to a body of a vehicle and configured to rotate forward from a deployed configuration, in which the wing extends from the body to a retracted configuration in which a tip portion of the wing is closer to a nose portion of the body than a root portion of the wing is to the nose portion. A hinged beam having a first portion pivotably coupled to a second portion is configured to transmit loads associated with flight from the wing to the body.
    Type: Grant
    Filed: January 31, 2017
    Date of Patent: May 11, 2021
    Inventor: Samuel Hall Bousfield
  • Patent number: 11001379
    Abstract: An airborne computational facility uses an energy collection system to provide energy for operation. An airborne balloon is provided with a photovoltaic collector array, and uses energy generated by the photovoltaic collector array to power an on-board computational facility. Data for computation is received by a communication module and computational results are transmitted by the communication module.
    Type: Grant
    Filed: November 5, 2018
    Date of Patent: May 11, 2021
    Inventors: Robert Matthew Panas, Philip Rettger, Cynthia Panas, Jonathan Harrington, Matthew Offenbacher
  • Patent number: 10995479
    Abstract: An aircraft has: an aircraft fuselage, a cabin region formed in the aircraft fuselage, underfloor region separated from the cabin region by a floor partition, and a fresh-water supply system. The fresh-water supply system has a fresh-water provision unit arranged in the underfloor region. The fresh-water supply system has multiple water extraction units which are each arranged in the cabin region, and a water line network branched off from the fresh-water provision unit and extending to the water extraction units. Each water extraction unit has a shut-off valve, a filter unit and a tapping point, which are coupled in series by means of water lines. Each filter unit has an exchangeable water filter with a first filter material designed for filtering particles out of the water flowing through the water filter and with a second filter material designed for softening the water flowing through the water filter.
    Type: Grant
    Filed: August 23, 2018
    Date of Patent: May 4, 2021
    Inventors: Volker Alps, Thomas Wiese, Sebastian Flashaar, Matthias Reiss
  • Patent number: 10994827
    Abstract: A wing arrangement for an aircraft, comprising a wing having a base section and a tip section pivotably connected to base section such that the tip section is pivotable about a pivot axis between a deployed position and a stowed position. The wing arrangement also comprises a latching arrangement which includes an engagement portion, a latching actuator selectively movable between a first actuator position and a second actuator position, an elastically deformable structure, and a latching element. When the tip section is pivoted from the stowed or deployed position into an engagement position, the elastically deformable structure is initially deformed, and as the tip section pivots further into the deployed or stowed position, the elastic deformation of the elastically deformable structure decreases.
    Type: Grant
    Filed: May 15, 2018
    Date of Patent: May 4, 2021
    Inventors: Christoph Winkelmann, Wilfried Ellmers, Stephen Briancourt, David Brakes
  • Patent number: 10993427
    Abstract: The present invention relates generally to fishing equipment, more specifically but not by way of limitation, a fishing lure apparatus that includes a first portion and a second portion wherein the fishing lure apparatus is configured to provide a first position and a second position for a fishing line secured thereto in order to facilitate release of the fishing lure apparatus on which it is snagged.
    Type: Grant
    Filed: May 21, 2019
    Date of Patent: May 4, 2021
    Inventor: Michael Griffith Brockhouse
  • Patent number: 10973214
    Abstract: A gig comprises a shaft; a spear head assembly comprising: a spear shaft; one or more spear prongs located at a first end of the spear shaft; and a ring, wherein the ring is secured to the spear shaft; and a stringer, wherein the stringer is removably or slidably connected to the ring. There can be more than one spear head assembly that can be used to spear more than one fish. Each of the spear head assemblies can be connected to the stringer via the rings whereby the fish can remain in the water until such time as it is desired to remove the fish. At that point, a person can simply draw the stringer towards them in order to retrieve the fish.
    Type: Grant
    Filed: December 13, 2018
    Date of Patent: April 13, 2021
    Inventor: Justin Grudzinski
  • Patent number: 10974830
    Abstract: A workpiece manipulation system to provide high-precision manipulation of a workpiece by an aircraft. The workpiece manipulation system comprises a lifting mechanism to couple with the aircraft, an end-effector, and a processor. The lifting mechanism includes one or more joint actuators to extend or retract the lifting mechanism relative to the aircraft. The end-effector includes an end-effector actuator to control an operation of the end-effector to manipulate the workpiece. The processor is communicatively coupled with the aircraft processor and configured to control operation of the end-effector actuator and the one or more joint actuators. In operation, the processor provides feedback to the aircraft.
    Type: Grant
    Filed: December 28, 2017
    Date of Patent: April 13, 2021
    Assignee: Auror Flight Scienes Corporation
    Inventors: William Bosworth, Devin Richard Jensen, Jae-Woo Choi
  • Patent number: 10974826
    Abstract: Apparatus, systems, and methods are contemplated for electric powered vertical takeoff and landing (eVTOL) aircraft. Such are craft are engineered to carry safely carry at least 500 pounds (approx. 227 kg) using at least four, and more preferably at least six variable speed tilt rotors. In some embodiments one or more rotors cooperate to generate at least 50% of the lift, and more preferably at least 70% of the lift, during rotorborne flight (e.g., vertical takeoff, hover, etc). At least some of the blades of each of the at least four rotors are not feathered, retracted, or folded during forward flight. At least one of the variable speed tilt rotors is engineered to be optionally powered by multiple motors, and by multiple battery packs or other independently operating electric power sources. The vehicle preferably flies in an autopilot or pilotless mode and has a relatively small (e.g., less than 45? diameter) footprint.
    Type: Grant
    Filed: March 13, 2019
    Date of Patent: April 13, 2021
    Assignee: Overair, Inc.
    Inventors: Abe Karem, William Martin Waide
  • Patent number: 10967973
    Abstract: A cargo transport system comprising a spine assembly and a container assembly. The spine assembly comprises a rigid spine and a plurality of mounts arranged on the rigid spine in a plurality of mount rows. The container assembly comprises a plurality of containers and is secured to the spine assembly using at least a subset of the plurality of mounts. Each container of the plurality of containers comprises a plurality of fittings for securing the container to the spine assembly and/or another container of the container assembly. Each mount row extends along a width of the spine assembly, and the plurality of mount rows are spaced apart at regular distance intervals along a length of the spine.
    Type: Grant
    Filed: January 10, 2018
    Date of Patent: April 6, 2021
    Assignee: Biosphere Aerospace, LLC
    Inventor: Elie Helou, Jr.
  • Patent number: 10946956
    Abstract: An unmanned aerial system includes an elongated fuselage having first and second rotational degrees of freedom. A forward propulsion assembly is disposed at the forward end of the fuselage. The forward propulsion assembly includes a forward rotor hub assembly rotatably coupled to the fuselage and reversibly tiltable about a first gimballing axis to provide a first moment on the fuselage in the first rotational degree of freedom. An aft propulsion assembly is disposed at the aft end of the fuselage. The aft propulsion assembly includes an aft rotor hub assembly rotatably coupled to the fuselage and reversibly tiltable about a second gimballing axis to provide a second moment on the fuselage in the second rotational degree of freedom. The first gimballing axis is out of phase with the second gimballing axis to control the orientation of the fuselage.
    Type: Grant
    Filed: August 30, 2018
    Date of Patent: March 16, 2021
    Assignee: Textron Innovations Inc.
    Inventor: Kip Gregory Campbell
  • Patent number: 10945423
    Abstract: An apparatus for controlling mosquito populations by eradicating mosquito eggs. The apparatus consists of a spawning tank and a multi-purpose spawning tank cover. The cover of the spawning tank is used as a depressor bowl and the spawning tank functions as a confining chamber. Experimental results show that the mosquito egg eradicating apparatus can effectively eradicate 90% of field mosquito eggs in four hours.
    Type: Grant
    Filed: October 1, 2020
    Date of Patent: March 16, 2021
    Inventor: Logan Cheng
  • Patent number: 10940943
    Abstract: A float has a front-to-back length, a width, and a height where the front-to-back length of the float is strictly greater than the height of the float which in turn is strictly greater than the width of the float. At least a bottom portion of the float is watertight. The float includes an access panel to access the inside of the float. A battery is inside the float and is accessible via the access panel.
    Type: Grant
    Filed: July 11, 2018
    Date of Patent: March 9, 2021
    Assignee: Kitty Hawk Corporation
    Inventors: Cameron Robertson, Todd Reichert
  • Patent number: 10932456
    Abstract: A blade body of a fishing lure comprises a first protruding side and a second protruding side, creating a gap, and a jig body connected to the blade body such that when the blade body and jig body are connected and pulled through water, the blade body moves in a side to side motion limited by contact between the jig body and the first and second protruding sides.
    Type: Grant
    Filed: July 26, 2018
    Date of Patent: March 2, 2021
    Inventor: Jason K Schwartz
  • Patent number: 10919611
    Abstract: A safety open and closing system for an overpressure door on fuselage of an aircraft. Wherein the safety opening and closing system allows safe access through the overpressure door to the compartment. The safety open and closing system including an assembly of a hollow beam, a blocking bar in the hollow beam, a spring biasing the blocking bar with respect to the hollow beam and a lever at the end of the blocking beam which pivots between a position A that allows closure of the overpressure door and a position B preventing closure of the door.
    Type: Grant
    Filed: February 7, 2018
    Date of Patent: February 16, 2021
    Assignee: Airbus Operations S.L.
    Inventors: David López Fernández, Maria Aránzazu García Patino, Sergio Gil GonzáLez
  • Patent number: 10906637
    Abstract: A propulsion assembly for a rotorcraft includes a blade assembly, a drive shaft coupled to the blade assembly and an electric motor coupled to the drive shaft and operable to provide rotational energy to the drive shaft to rotate the blade assembly. The propulsion assembly includes a landing assistance turbine coupled to the drive shaft and operable to selectively provide rotational energy to the drive shaft during an underpowered descent to rotate the blade assembly and provide upward thrust, thereby reducing a descent rate of the rotorcraft prior to landing.
    Type: Grant
    Filed: May 17, 2018
    Date of Patent: February 2, 2021
    Assignee: Textron Innovations Inc.
    Inventors: Frank Bradley Stamps, Michael K. McNair, John Richard McCullough
  • Patent number: 10905090
    Abstract: A control device which, when it is installed as part of a fence, allows a small animal to pass from a first side of the fence to the other side of the fence, but prevents an animal which has passed through the device from returning to the first side of the fence. The control device can comprise (1) a mouth which (i) is exposed on the first side of the fence and (ii) has an open cross-section, and (2) an extending passage which extends away from the mouth to an exit. The extending passage can narrow as it extends from the mouth to the exit.
    Type: Grant
    Filed: April 2, 2020
    Date of Patent: February 2, 2021
    Inventors: Vincent P. Morris, Richard H. Sherratt
  • Patent number: 10899461
    Abstract: A hybrid-electric aerial vehicle is disclosed comprising: an airframe; a plurality of longitudinal booms extending radially from the airframe; a passively charged internal combustion engine operatively coupled with a fuel tank, a generator operatively coupled with the passively charged internal combustion engine; a battery bank operatively coupled with the generator; and a plurality of motors. The passively charged internal combustion engine has an intake engine valve, an exhaust engine valve, and a combustion chamber, wherein the intake engine valve is delayed to provide an expansion ratio in the combustion chamber that is greater than a compression ratio in the combustion chamber. Each of said plurality of motors may be positioned at a distal end of one of said plurality of longitudinal booms and be operatively coupled with a propeller, wherein the plurality of motors is electrically coupled with the battery bank and the generator.
    Type: Grant
    Filed: January 10, 2018
    Date of Patent: January 26, 2021
    Assignee: Aurora Flight Sciences Corporation
    Inventors: Evangelos Livieratos, Riley Griffin, Nathan Varney, Amanda Kaufman
  • Patent number: 10899434
    Abstract: A wingtip device may be attached to a baseline wing of an aircraft. The wingtip device may comprise a vertical portion coupled to the baseline wing. The vertical portion may comprise a leading edge and trailing edge. The leading edge and trailing edge may be nonlinear shapes. For example, compound curves, smooth continuous higher order polynomials, or combinations thereof. The leading edge and trailing edge may be shaped as to locate the wingtip device further aft than a conventional winglet design.
    Type: Grant
    Filed: May 13, 2019
    Date of Patent: January 26, 2021
    Assignee: Tamarack Aerospace Group, Inc.
    Inventor: Nicholas R. Guida
  • Patent number: 10903380
    Abstract: A method of fabricating an airfoil, and the airfoil or airfoil skin so fabricated, including a solar cell array arranged on the surface of the airfoil by providing and utilizing an assembly fixture having a smooth, concave surface. An uncured supporting film composed of a composite material (such as a carbon fiber composite) is mounted directly on the back side of the solar cells; and the film of composite material is co-cured on the assembly fixture so that the array of interconnected solar cells is bonded to the supporting film. The bonded and cured film of composite material and an array of interconnected solar cells is then removed from the assembly fixture.
    Type: Grant
    Filed: May 11, 2018
    Date of Patent: January 26, 2021
    Assignee: Vanguard Space Technologies, Inc.
    Inventors: Matthew Wrosch, Eric McNaul, Theodore Stern, Fadel Hernandez