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).
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Patent number: 12319406Abstract: 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: GrantFiled: February 9, 2024Date of Patent: June 3, 2025Assignee: Textron Innovations Inc.Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
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Patent number: 12202613Abstract: 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: GrantFiled: August 6, 2021Date of Patent: January 21, 2025Assignee: Textron Innovations Inc.Inventors: Cheng-Ho Tho, Michael Reaugh Smith
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Publication number: 20240246664Abstract: 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: ApplicationFiled: February 9, 2024Publication date: July 25, 2024Applicant: Textron Innovations Inc.Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
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Patent number: 11932380Abstract: 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: GrantFiled: January 21, 2021Date of Patent: March 19, 2024Assignee: Textron Innovations Inc.Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
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Patent number: 11603207Abstract: 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: GrantFiled: December 19, 2019Date of Patent: March 14, 2023Assignee: Textron Innovations Inc.Inventors: Daniel Frank Devitt, Michael Reaugh Smith
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Patent number: 11584519Abstract: 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: GrantFiled: April 12, 2019Date of Patent: February 21, 2023Assignee: TEXTRON INNOVATIONS INC.Inventors: Michael Reaugh Smith, Frank B. Stamps, David E. Heverly, II
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Publication number: 20230038209Abstract: 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: ApplicationFiled: August 6, 2021Publication date: February 9, 2023Inventors: Cheng-Ho Tho, Michael Reaugh Smith
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Patent number: 11479338Abstract: 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: GrantFiled: September 29, 2020Date of Patent: October 25, 2022Assignee: Textron Innovations Inc.Inventors: Timothy Brian Carr, William Anthony Amante, Michael Reaugh Smith
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Publication number: 20220097823Abstract: 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: ApplicationFiled: September 29, 2020Publication date: March 31, 2022Inventors: Timothy Brian CARR, William Anthony AMANTE, Michael Reaugh SMITH
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Patent number: 11214362Abstract: 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: GrantFiled: December 16, 2019Date of Patent: January 4, 2022Assignee: Textron Innovations Inc.Inventors: Christopher Edward Foskey, Frank Bradley Stamps, Michael Reaugh Smith
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Publication number: 20210403148Abstract: 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: ApplicationFiled: January 21, 2021Publication date: December 30, 2021Applicant: Bell Textron Inc.Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Bradley Joseph Passe
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Patent number: 11203418Abstract: 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: GrantFiled: December 17, 2019Date of Patent: December 21, 2021Assignee: Textron Innovations Inc.Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Michael Scott Seifert
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Patent number: 11142334Abstract: 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: GrantFiled: December 19, 2017Date of Patent: October 12, 2021Assignee: Textron Innovations Inc.Inventors: Cheng-Ho Tho, Michael Reaugh Smith
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Patent number: 11131363Abstract: 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: GrantFiled: October 16, 2017Date of Patent: September 28, 2021Assignee: Textron Innovations Inc.Inventors: Michael Reaugh Smith, Frank Bradley Stamps, Craig Turner, Maurice Griffin
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Patent number: 11097836Abstract: 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: GrantFiled: March 21, 2019Date of Patent: August 24, 2021Assignee: Textron Innovations Inc.Inventors: Michael Reaugh Smith, Jouyoung Jason Choi, Joseph Richard Carpenter, Steve Michael Loveland
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Patent number: 10974822Abstract: 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: GrantFiled: October 24, 2018Date of Patent: April 13, 2021Assignee: Textron Innovations Inc.Inventors: Michael Reaugh Smith, Jouyoung Jason Choi
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Publication number: 20200398976Abstract: 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: ApplicationFiled: December 17, 2019Publication date: December 24, 2020Applicant: Bell Textron Inc.Inventors: Frank Bradley Stamps, Michael Reaugh Smith, Michael Scott Seifert
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Publication number: 20200393851Abstract: 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: ApplicationFiled: June 12, 2019Publication date: December 17, 2020Applicant: Bell Textron Inc.Inventors: Sung Kyun KIM, Michael Reaugh SMITH
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Publication number: 20200324883Abstract: 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: ApplicationFiled: April 12, 2019Publication date: October 15, 2020Inventors: Michael Reaugh Smith, Frank B. Stamps, David E. Heverly, II
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Publication number: 20200298967Abstract: 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: ApplicationFiled: March 21, 2019Publication date: September 24, 2020Inventors: Michael Reaugh Smith, Jouyoung Jason Choi, Joseph Richard Carpenter, Steve Michael Loveland