Patents by Inventor Michael Reaugh Smith

Michael Reaugh Smith 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).

  • Patent number: 12319406
    Abstract: A compound helicopter includes a fuselage including a fuselage airframe, a translational thrust system coupled to the fuselage airframe and a pylon assembly subject to vibration. The pylon assembly includes a transmission and a rotor system having a main rotor assembly. The compound helicopter also includes a main rotor vibration isolation system including a plurality of augmented liquid inertia vibration eliminator units each having an isolation frequency and each coupled between the fuselage airframe and the pylon assembly to reduce transmission of the pylon assembly vibration to the fuselage airframe at the isolation frequency. Each augmented liquid inertia vibration eliminator unit includes at least one active tuning element movable to tune the isolation frequency thereof.
    Type: Grant
    Filed: February 9, 2024
    Date of Patent: June 3, 2025
    Assignee: Textron Innovations Inc.
    Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
  • Patent number: 12202613
    Abstract: An implementation of an external airbag system may include a plurality of inflatable air bags, a duct coupled to the plurality of inflatable air bags, and an exhaust vent coupled to each of the plurality of inflatable air bags via the duct.
    Type: Grant
    Filed: August 6, 2021
    Date of Patent: January 21, 2025
    Assignee: Textron Innovations Inc.
    Inventors: Cheng-Ho Tho, Michael Reaugh Smith
  • Publication number: 20240246664
    Abstract: A compound helicopter includes a fuselage including a fuselage airframe, a translational thrust system coupled to the fuselage airframe and a pylon assembly subject to vibration. The pylon assembly includes a transmission and a rotor system having a main rotor assembly. The compound helicopter also includes a main rotor vibration isolation system including a plurality of augmented liquid inertia vibration eliminator units each having an isolation frequency and each coupled between the fuselage airframe and the pylon assembly to reduce transmission of the pylon assembly vibration to the fuselage airframe at the isolation frequency. Each augmented liquid inertia vibration eliminator unit includes at least one active tuning element movable to tune the isolation frequency thereof.
    Type: Application
    Filed: February 9, 2024
    Publication date: July 25, 2024
    Applicant: Textron Innovations Inc.
    Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
  • Patent number: 11932380
    Abstract: A compound helicopter includes a fuselage including a fuselage airframe, a translational thrust system coupled to the fuselage airframe and a pylon assembly subject to vibration. The pylon assembly includes a transmission and a rotor system having a main rotor assembly. The compound helicopter also includes a main rotor vibration isolation system including a plurality of augmented liquid inertia vibration eliminator units each having an isolation frequency and each coupled between the fuselage airframe and the pylon assembly to reduce transmission of the pylon assembly vibration to the fuselage airframe at the isolation frequency. Each augmented liquid inertia vibration eliminator unit includes at least one active tuning element movable to tune the isolation frequency thereof.
    Type: Grant
    Filed: January 21, 2021
    Date of Patent: March 19, 2024
    Assignee: Textron Innovations Inc.
    Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
  • Patent number: 11603207
    Abstract: In some implementations, in an emergency in the vehicle, an emergency evacuation path is illuminated using the light emitted from the emergency evacuation rope where at least a portion of the emergency evacuation path extends to a location outside the vehicle. Egress of occupants along the emergency evacuation path is enabled using an emergency evacuation rope.
    Type: Grant
    Filed: December 19, 2019
    Date of Patent: March 14, 2023
    Assignee: Textron Innovations Inc.
    Inventors: Daniel Frank Devitt, Michael Reaugh Smith
  • Patent number: 11584519
    Abstract: In some examples, an oscillatory pumping system comprises: one or more active piston, a fluid, and two motors. The one or more active piston is disposed in a channel fluidically coupling two fluid chambers. The passive piston has a frequency response operable to counteract a vibratory displacement. The fluid is disposed in the channel and the two fluid chambers. The two motors couple to the one or more active piston. The two motors are operable to selectively change the frequency response of the passive piston based on oscillating the one or more active piston.
    Type: Grant
    Filed: April 12, 2019
    Date of Patent: February 21, 2023
    Assignee: TEXTRON INNOVATIONS INC.
    Inventors: Michael Reaugh Smith, Frank B. Stamps, David E. Heverly, II
  • Publication number: 20230038209
    Abstract: An implementation of an external airbag system may include a plurality of inflatable air bags, a duct coupled to the plurality of inflatable air bags, and an exhaust vent coupled to each of the plurality of inflatable air bags via the duct.
    Type: Application
    Filed: August 6, 2021
    Publication date: February 9, 2023
    Inventors: Cheng-Ho Tho, Michael Reaugh Smith
  • Patent number: 11479338
    Abstract: In an embodiment, a ducted fan assembly includes a housing that further includes a rotor. The ducted fan assembly also includes a rim that extends around at least a portion of a perimeter of the ducted fan assembly, where the rim defines an opening surrounding at least a portion of the housing. The ducted fan assembly also includes a skin that is attached to the rim and extends around the at least a portion of a perimeter of the ducted fan assembly to form a leading edge of the ducted fan assembly. The ducted fan assembly also includes a blade positioned on the rim underneath the skin.
    Type: Grant
    Filed: September 29, 2020
    Date of Patent: October 25, 2022
    Assignee: Textron Innovations Inc.
    Inventors: Timothy Brian Carr, William Anthony Amante, Michael Reaugh Smith
  • Publication number: 20220097823
    Abstract: In an embodiment, a ducted fan assembly includes a housing that further includes a rotor. The ducted fan assembly also includes a rim that extends around at least a portion of a perimeter of the ducted fan assembly, where the rim defines an opening surrounding at least a portion of the housing. The ducted fan assembly also includes a skin that is attached to the rim and extends around the at least a portion of a perimeter of the ducted fan assembly to form a leading edge of the ducted fan assembly. The ducted fan assembly also includes a blade positioned on the rim underneath the skin.
    Type: Application
    Filed: September 29, 2020
    Publication date: March 31, 2022
    Inventors: Timothy Brian CARR, William Anthony AMANTE, Michael Reaugh SMITH
  • Patent number: 11214362
    Abstract: An advancing blade concept rotorcraft includes an airframe and a pylon assembly subject to vibration. The pylon assembly includes a dual rotor system having coaxially disposed top and bottom rotor assemblies that counter rotate relative to one another. The advancing blade concept rotorcraft includes a vibration isolation system including at least one pylon link coupled to the airframe and the pylon assembly. The pylon link includes a Liquid Inertia Vibration Eliminator unit operable to reduce transmission of the pylon assembly vibration to the airframe. The advancing blade concept rotorcraft includes active force generators adjacent to the pylon assembly. The active force generators include a first active force generator producing a force in a first direction and a second active force generator producing a force in a second direction to counteract multidirectional oscillations of the pylon assembly, thereby reducing vibration of the advancing blade concept rotorcraft.
    Type: Grant
    Filed: December 16, 2019
    Date of Patent: January 4, 2022
    Assignee: Textron Innovations Inc.
    Inventors: Christopher Edward Foskey, Frank Bradley Stamps, Michael Reaugh Smith
  • Publication number: 20210403148
    Abstract: A compound helicopter includes a fuselage including a fuselage airframe, a translational thrust system coupled to the fuselage airframe and a pylon assembly subject to vibration. The pylon assembly includes a transmission and a rotor system having a main rotor assembly. The compound helicopter also includes a main rotor vibration isolation system including a plurality of augmented liquid inertia vibration eliminator units each having an isolation frequency and each coupled between the fuselage airframe and the pylon assembly to reduce transmission of the pylon assembly vibration to the fuselage airframe at the isolation frequency. Each augmented liquid inertia vibration eliminator unit includes at least one active tuning element movable to tune the isolation frequency thereof.
    Type: Application
    Filed: January 21, 2021
    Publication date: December 30, 2021
    Applicant: Bell Textron Inc.
    Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
  • Patent number: 11203418
    Abstract: A mount system for tiltably supporting a pylon assembly of a rotorcraft. First, second, third and fourth pylon links are each coupled between the pylon assembly and the airframe of the rotorcraft. The first pylon link has a first axis, the second pylon link has a second axis, the third pylon link has a third axis and the fourth pylon link has a fourth axis. Each of the axes intersects at a focal point located proximate a coaxial rotor system having counter-rotating upper and lower rotor assemblies such that the focal point provides a virtual pivot point about which the pylon assembly tilts to generate a control moment about a center of gravity of the rotorcraft that counteracts lateral and fore/aft moments generated by the upper and lower rotor assemblies during rotorcraft maneuvers.
    Type: Grant
    Filed: December 17, 2019
    Date of Patent: December 21, 2021
    Assignee: Textron Innovations Inc.
    Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Michael Scott Seifert
  • Patent number: 11142334
    Abstract: An in-flight impact protection system for aircraft. An aircraft having a panel, with a sensor disposed on the aircraft and adapted to transmit a signal and receive a reflection of the signal. A controller coupled to the sensor and adapted to receive the reflection from the sensor to determine whether an object is near the aircraft's panel. An inflation device, which includes a tube member, is coupled to the controller and positioned inside the aircraft, proximate the panel. After determining that the object is near the panel, the controller can activate the inflation device so that the tube member inflates, thereby buttressing at least a portion of the panel. The panel can be a windshield, fuselage member, or other suitable component.
    Type: Grant
    Filed: December 19, 2017
    Date of Patent: October 12, 2021
    Assignee: Textron Innovations Inc.
    Inventors: Cheng-Ho Tho, Michael Reaugh Smith
  • Patent number: 11131363
    Abstract: A vibration attenuating fluid mount with a partitioned compensator includes an inner member, an outer member, a flexible member having a castellated transition between a fluid passageway and at least one operating chamber. A membrane may be disposed in a volume compensator in fluid communication with one or more operating chambers. The inner member and outer member may be connected via a castellated connection, a swaged lock ring, or a split-lock ring.
    Type: Grant
    Filed: October 16, 2017
    Date of Patent: September 28, 2021
    Assignee: Textron Innovations Inc.
    Inventors: Michael Reaugh Smith, Frank Bradley Stamps, Craig Turner, Maurice Griffin
  • Patent number: 11097836
    Abstract: In some examples, an aircraft comprises an airframe, a rotor system coupled to the airframe, and a vibration attenuation system. The rotor system is operable to exert a vibratory force on the airframe. The vibration attenuation system comprises two or more batteries and elastic devices. The two or more batteries are operable to supply power to the rotor system. The elastic devices coupled to the two or more batteries and the airframe. The elastic devices are configured to attenuate the vibratory force based on facilitating oscillation of the two or more batteries. In other examples, a method comprises coupling elastic devices to two or more batteries and an airframe of an aircraft. The elastic devices receiving a vibratory force via the airframe and attenuate the vibratory force based on facilitating oscillation of the two or more batteries.
    Type: Grant
    Filed: March 21, 2019
    Date of Patent: August 24, 2021
    Assignee: Textron Innovations Inc.
    Inventors: Michael Reaugh Smith, Jouyoung Jason Choi, Joseph Richard Carpenter, Steve Michael Loveland
  • Patent number: 10974822
    Abstract: An anti-tail buffet device leverages existing rotorcraft components to attenuate a tailboom's lateral “ringing” from air buffeting. Anti-buffet masses are tuned to the tailboom's lateral-bending or torsional natural frequency such that when lateral motion occurs, the response at this frequency is cancelled by the anti-buffet system, preventing this vibration from entering into the tailboom structure. Motion stops prevent over-travel. The mass of the tail rotor actuator is soft-mounted, such that its natural frequency is equal to the tailboom's lateral-bending or torsional natural frequency. When lateral loading occurs on the tail rotor disk, the lateral response at this frequency is attenuated by the soft-mounted tail rotor actuator, thereby preventing the vibration in the tailboom structure.
    Type: Grant
    Filed: October 24, 2018
    Date of Patent: April 13, 2021
    Assignee: Textron Innovations Inc.
    Inventors: Michael Reaugh Smith, Jouyoung Jason Choi
  • Publication number: 20200398976
    Abstract: A mount system for tiltably supporting a pylon assembly of a rotorcraft. First, second, third and fourth pylon links are each coupled between the pylon assembly and the airframe of the rotorcraft. The first pylon link has a first axis, the second pylon link has a second axis, the third pylon link has a third axis and the fourth pylon link has a fourth axis. Each of the axes intersects at a focal point located proximate a coaxial rotor system having counter-rotating upper and lower rotor assemblies such that the focal point provides a virtual pivot point about which the pylon assembly tilts to generate a control moment about a center of gravity of the rotorcraft that counteracts lateral and fore/aft moments generated by the upper and lower rotor assemblies during rotorcraft maneuvers.
    Type: Application
    Filed: December 17, 2019
    Publication date: December 24, 2020
    Applicant: Bell Textron Inc.
    Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Michael Scott Seifert
  • Publication number: 20200393851
    Abstract: A high-performance descent system for a multi-rotor aircraft includes a flight control computer comprising a processor, a propulsion system communicatively coupled to the flight control computer and configured to allow a direction of thrust relative to a vertical z-axis to be selected by the flight control computer. The processor is operable to implement a method including preparing the multi-rotor aircraft for a high-performance descent, instructing, via a flight control system, a proprotor to reduce an amount of vertical thrust produced by the proprotor by tilting the proprotor away from a vertical axis, and reducing an altitude of the multi-rotor aircraft.
    Type: Application
    Filed: June 12, 2019
    Publication date: December 17, 2020
    Applicant: Bell Textron Inc.
    Inventors: Sung Kyun KIM, Michael Reaugh SMITH
  • Publication number: 20200324883
    Abstract: In some examples, an oscillatory pumping system comprises: one or more active piston, a fluid, and two motors. The one or more active piston is disposed in a channel fluidically coupling two fluid chambers. The passive piston has a frequency response operable to counteract a vibratory displacement. The fluid is disposed in the channel and the two fluid chambers. The two motors couple to the one or more active piston. The two motors are operable to selectively change the frequency response of the passive piston based on oscillating the one or more active piston.
    Type: Application
    Filed: April 12, 2019
    Publication date: October 15, 2020
    Inventors: Michael Reaugh Smith, Frank B. Stamps, David E. Heverly, II
  • Publication number: 20200298967
    Abstract: In some examples, an aircraft comprises an airframe, a rotor system coupled to the airframe, and a vibration attenuation system. The rotor system is operable to exert a vibratory force on the airframe. The vibration attenuation system comprises two or more batteries and elastic devices. The two or more batteries are operable to supply power to the rotor system. The elastic devices coupled to the two or more batteries and the airframe. The elastic devices are configured to attenuate the vibratory force based on facilitating oscillation of the two or more batteries. In other examples, a method comprises coupling elastic devices to two or more batteries and an airframe of an aircraft. The elastic devices receiving a vibratory force via the airframe and attenuate the vibratory force based on facilitating oscillation of the two or more batteries.
    Type: Application
    Filed: March 21, 2019
    Publication date: September 24, 2020
    Inventors: Michael Reaugh Smith, Jouyoung Jason Choi, Joseph Richard Carpenter, Steve Michael Loveland