Patents by Inventor Kevin Knott
Kevin Knott 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: 12122535Abstract: An exemplary aircraft transport jack includes a vertical structure having a vertical axis, a bottom end, and a top end, a connector above the bottom end operable to detachably secure the vertical structure to an aircraft member, a wheel assembly with wheels positioned on opposing sides of the vertical structure, and an actuator coupled to the vertical structure and the wheel assembly and operable to move the wheel assembly axially relative to the vertical structure between a lowered position with the wheels on a ground and a raised position with the bottom end on the ground and the wheels above the ground.Type: GrantFiled: May 3, 2021Date of Patent: October 22, 2024Assignee: Textron Innovations Inc.Inventors: Alvin Jones, Vitthal Vishnuthreeth Arakeri, Kevin Knott
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Patent number: 11912403Abstract: An exemplary pitch link centering tool includes a rod having a longitudinal axis, a front face, a rear face, a first rod end and a second rod end, the first rod end having a first aperture with a first rotational axis, the second rod end having a second aperture with a second rotational axis, a first connector coupled to the first rod end, the first connector having a first slot extending in a first radial direction relative to the longitudinal axis and a second connector coupled to the second rod end, the second connector having a second slot extending in a second radial direction relative to the longitudinal axis different from the first radial direction.Type: GrantFiled: May 3, 2021Date of Patent: February 27, 2024Assignee: Textron Innovations Inc.Inventors: Kevin Knott, Vitthal Vishnuthreeth Arakeri
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Patent number: 11760470Abstract: An exemplary rotorcraft lockout system includes a main rotor lockout comprising a base operable to be attached to a bottom surface of a fuselage and a first and a second tension arm operable to be connected to the base and a main rotor hub, and a tail rotor lockout including a clamp operable to connect to a horizontal stabilizer, a rotor arm connector operable to connect to a tail rotor hub, and a tail rotor tension arm operable to interconnect the clamp and the rotor arm connector in tension.Type: GrantFiled: May 3, 2021Date of Patent: September 19, 2023Assignee: Textron Innovations Inc.Inventors: Kevin Knott, Vitthal Vishnuthreeth Arakeri, Alvin Jones, Scott David Poster, Steven Paul Pape, Mark Adam Wiinikka
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Publication number: 20220297831Abstract: An exemplary pitch link centering tool includes a rod having a longitudinal axis, a front face, a rear face, a first rod end and a second rod end, the first rod end having a first aperture with a first rotational axis, the second rod end having a second aperture with a second rotational axis, a first connector coupled to the first rod end, the first connector having a first slot extending in a first radial direction relative to the longitudinal axis and a second connector coupled to the second rod end, the second connector having a second slot extending in a second radial direction relative to the longitudinal axis different from the first radial direction.Type: ApplicationFiled: May 3, 2021Publication date: September 22, 2022Applicant: Bell Textron Inc.Inventors: Kevin KNOTT, Vitthal Vishnuthreeth ARAKERI
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Publication number: 20220297853Abstract: An exemplary aircraft transport jack includes a vertical structure having a vertical axis, a bottom end, and a top end, a connector above the bottom end operable to detachably secure the vertical structure to an aircraft member, a wheel assembly with wheels positioned on opposing sides of the vertical structure, and an actuator coupled to the vertical structure and the wheel assembly and operable to move the wheel assembly axially relative to the vertical structure between a lowered position with the wheels on a ground and a raised position with the bottom end on the ground and the wheels above the ground.Type: ApplicationFiled: May 3, 2021Publication date: September 22, 2022Applicant: Bell Textron Inc.Inventors: Alvin JONES, Vitthal Vishnuthreeth ARAKERI, Kevin KNOTT
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Publication number: 20220297830Abstract: An exemplary rotorcraft lockout system includes a main rotor lockout comprising a base operable to be attached to a bottom surface of a fuselage and a first and a second tension arm operable to be connected to the base and a main rotor hub, and a tail rotor lockout including a clamp operable to connect to a horizontal stabilizer, a rotor arm connector operable to connect to a tail rotor hub, and a tail rotor tension arm operable to interconnect the clamp and the rotor arm connector in tension.Type: ApplicationFiled: May 3, 2021Publication date: September 22, 2022Applicant: Bell Textron Inc.Inventors: Kevin KNOTT, Vitthal Vishnuthreeth ARAKERI, Alvin JONES, Scott David POSTER, Steven Paul PAPE, Mark Adam WIINIKKA
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Publication number: 20210393999Abstract: The present invention includes a safety apparatus and method for protecting users during maintenance operations for a rotorcraft comprising: at least one permanent, semi-permanent, or detachable safety bar, strap, fastener, hook, or loop that is attached or attachable to a rotorcraft, wherein the safety bar, strap, fastener, hook, or loop is positioned in an area or surface between a windshield of the rotorcraft and a tail boom of the rotorcraft and is connectable to a user safety device to provide fall protection from the area or surface.Type: ApplicationFiled: August 31, 2021Publication date: December 23, 2021Inventors: Bob Thornton, Chyau Tzeng, Brian Mesing, Kevin Knott, Mark Wiinikka, Edith Richard, David Platz, Joshua Edler, Sarah Villanueva, Thomas Mast, Joseph Leachman, Daniel John Burns
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Patent number: 11130009Abstract: The present invention includes a safety apparatus and method for protecting users during maintenance operations for a rotorcraft comprising: at least one permanent, semi-permanent, or detachable safety bar, strap, fastener, hook, or loop that is attached or attachable to a rotorcraft, wherein the safety bar, strap, fastener, hook, or loop is positioned in an area or surface between a windshield of the rotorcraft and a tail boom of the rotorcraft and is connectable to a user safety device to provide fall protection from the area or surface.Type: GrantFiled: November 4, 2016Date of Patent: September 28, 2021Assignee: TEXTRON INNOVATIONS INC.Inventors: Bob Thornton, Chyau Tzeng, Brian Mesing, Kevin Knott, Mark Wiinikka, Edith Richard, David Platz, Joshua Edler, Sarah Villanueva, Thomas Mast, Joseph Leachman, Daniel John Burns
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Publication number: 20180126199Abstract: The present invention includes a safety apparatus and method for protecting users during maintenance operations for a rotorcraft comprising: at least one permanent, semi-permanent, or detachable safety bar, strap, fastener, hook, or loop that is attached or attachable to a rotorcraft, wherein the safety bar, strap, fastener, hook, or loop is positioned in an area or surface between a windshield of the rotorcraft and a tail boom of the rotorcraft and is connectable to a user safety device to provide fall protection from the area or surface.Type: ApplicationFiled: November 4, 2016Publication date: May 10, 2018Inventors: Bob Thornton, Chyau Tzeng, Brian Mesing, Kevin Knott, Mark Wiinikka, Edith Richard, David Platz, Joshua Edler, Sarah Villanueva, Thomas Mast, Joseph Leachman, Daniel John Burns