Patents by Inventor Carl R. McIver

Carl R. McIver 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: 11130329
    Abstract: An apparatus is provided for peeling a liner away from a substrate. The apparatus comprises a first member rotatable about an axis. The apparatus also comprises a second member disposed on the first member and for generating a suction force to be applied to the liner to peel a portion of the liner away from the substrate when the suction force of the second member is applied to the liner and the first member is rotating about its axis. The apparatus further comprises a third member synchronized to rotation of the first member about its axis such that the third member clamps the peeled portion of the liner against the first member while the second member is applying suction force to the liner and the first member is rotating about its axis.
    Type: Grant
    Filed: February 7, 2020
    Date of Patent: September 28, 2021
    Assignee: The Boeing Company
    Inventors: Carl R. McIver, Brice A. Johnson, Michael R. Anderson
  • Publication number: 20210245491
    Abstract: An apparatus is provided for peeling a liner away from a substrate. The apparatus comprises a first member rotatable about an axis. The apparatus also comprises a second member disposed on the first member and for generating a suction force to be applied to the liner to peel a portion of the liner away from the substrate when the suction force of the second member is applied to the liner and the first member is rotating about its axis. The apparatus further comprises a third member synchronized to rotation of the first member about its axis such that the third member clamps the peeled portion of the liner against the first member while the second member is applying suction force to the liner and the first member is rotating about its axis.
    Type: Application
    Filed: February 7, 2020
    Publication date: August 12, 2021
    Applicant: The Boeing Company
    Inventors: Carl R. McIver, Brice A. Johnson, Michael R. Anderson
  • Patent number: 9057362
    Abstract: A vacuum pump may comprise a grating, and a sublimation element. The grating may have a grating opening and a grating interior that may be bounded by at least one grating surface. The sublimation element may be located within the grating interior and may be configured to sublimate and form a reactive film on the grating interior upon heating of the sublimation element above the sublimation temperature. The reactive film may be effective to capture gas molecules entering the grating interior through the grating opening and contacting the reactive film.
    Type: Grant
    Filed: September 28, 2011
    Date of Patent: June 16, 2015
    Assignee: The Boeing Company
    Inventor: Carl R. McIver
  • Patent number: 9019683
    Abstract: A method for sealing an interface to attenuate high energy currents and voltages traveling thereacross may include forming a cover defining an inner volume shaped to enclose the interface; forming a filled sealant including a semi-rigid sealant mixed with a filler having a multiplicity of discrete particles of different composition than the semi-rigid sealant; placing the filled sealant within the inner volume; and placing the cover containing the filled sealant over the interface such that the filled sealant is adjacent the interface.
    Type: Grant
    Filed: April 24, 2014
    Date of Patent: April 28, 2015
    Assignee: The Boeing Company
    Inventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin E. McCrary
  • Publication number: 20140235083
    Abstract: A method for sealing an interface to attenuate high energy currents and voltages traveling thereacross may include forming a cover defining an inner volume shaped to enclose the interface; forming a filled sealant including a semi-rigid sealant mixed with a filler having a multiplicity of discrete particles of different composition than the semi-rigid sealant; placing the filled sealant within the inner volume; and placing the cover containing the filled sealant over the interface such that the filled sealant is adjacent the interface.
    Type: Application
    Filed: April 24, 2014
    Publication date: August 21, 2014
    Applicant: The Boeing Company
    Inventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin E. McCrary
  • Patent number: 8717735
    Abstract: A seal for attenuating energy from an electrical discharge across an interface may include a cover defining an inner volume containing a filled sealant including a semi-rigid sealant mixed with a filler having a multiplicity of discrete particles of different composition than the semi-rigid sealant such that the filled sealant is adjacent the interface when the cover is placed over said interface. A method for sealing an interface may include forming a cover defining an inner volume shaped to enclose the interface, forming a filled sealant including a semi-rigid sealant mixed with a filler having a multiplicity of discrete particles of different composition than said semi-rigid sealant, placing the filled sealant within said inner volume and placing the cover containing the filled sealant over the interface such that the filled sealant is adjacent the interface.
    Type: Grant
    Filed: December 14, 2011
    Date of Patent: May 6, 2014
    Assignee: The Boeing Company
    Inventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin McCrary
  • Publication number: 20130153136
    Abstract: A seal for attenuating energy from an electrical discharge across an interface may include a cover defining an inner volume containing a filled sealant including a semi-rigid sealant mixed with a filler having a multiplicity of discrete particles of different composition than the semi-rigid sealant such that the filled sealant is adjacent the interface when the cover is placed over said interface. A method for sealing an interface may include forming a cover defining an inner volume shaped to enclose the interface, forming a filled sealant including a semi-rigid sealant mixed with a filler having a multiplicity of discrete particles of different composition than said semi-rigid sealant, placing the filled sealant within said inner volume and placing the cover containing the filled sealant over the interface such that the filled sealant is adjacent the interface.
    Type: Application
    Filed: December 14, 2011
    Publication date: June 20, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin McCrary
  • Publication number: 20130078112
    Abstract: A vacuum pump may comprise a grating, and a sublimation element. The grating may have a grating opening and a grating interior that may be bounded by at least one grating surface. The sublimation element may be located within the grating interior and may be configured to sublimate and form a reactive film on the grating interior upon heating of the sublimation element above the sublimation temperature. The reactive film may be effective to capture gas molecules entering the grating interior through the grating opening and contacting the reactive film.
    Type: Application
    Filed: September 28, 2011
    Publication date: March 28, 2013
    Applicant: THE BOEING COMPANY
    Inventor: Carl R. McIver
  • Patent number: 8020673
    Abstract: A braking system for a high speed, high load rotor operating in a vacuum and suspended by a magnetic field such as in a flywheel energy storage device includes a pair of calipers disposed on opposed sides of the rotor for actuating a pair of annular friction discs into engagement with opposed sides of the rotor. Each caliper includes a mounting ring on its outer edge and an inner shallow annular groove in which it disposed one of the friction discs. A circulating fluid under pressure is directed into each annular groove for urging each friction disc into engagement with one of the opposed surfaces of the rotor for safely bringing the rotor to a stop such as in an emergency. The circulating fluid removes the heat generated by the braking action, while the controlled pressure applied by the discs also controls the position of the rotor when static such as during initialization.
    Type: Grant
    Filed: July 30, 2007
    Date of Patent: September 20, 2011
    Assignee: The Boeing Company
    Inventors: Carl R. McIver, Kevin E. McCrary, John R. Hull, John A Mittleider
  • Patent number: 7633203
    Abstract: Methods and apparatuses to provide improved auxiliary damping for superconducting bearings in superconducting levitation systems are disclosed. In a superconducting bearing, a cryostat housing the superconductors is connected to a ground state with a combination of a damping strip of material, a set of linkage arms to provide vertical support, and spring washers to provide stiffness. Alternately, the superconducting bearing may be supported by a cryostat connected to a ground state by posts constructed from a mesh of fibers, with the damping and stiffness controlled by the fiber composition, size, and mesh geometry.
    Type: Grant
    Filed: January 2, 2008
    Date of Patent: December 15, 2009
    Assignee: The Boeing Company
    Inventors: John R. Hull, Carl R. McIver, John A. Mittleider
  • Publication number: 20090170707
    Abstract: Methods and apparatuses to provide improved auxiliary damping for superconducting bearings in superconducting levitation systems are disclosed. In a superconducting bearing, a cryostat housing the superconductors is connected to a ground state with a combination of a damping strip of material, a set of linkage arms to provide vertical support, and spring washers to provide stiffness. Alternately, the superconducting bearing may be supported by a cryostat connected to a ground state by posts constructed from a mesh of fibers, with the damping and stiffness controlled by the fiber composition, size, and mesh geometry.
    Type: Application
    Filed: January 2, 2008
    Publication date: July 2, 2009
    Applicant: The Boeing Company
    Inventors: John R. Hull, Carl R. McIver, John A. Mittleider
  • Publication number: 20090033145
    Abstract: A braking system for a high speed, high load rotor operating in a vacuum and suspended by a magnetic field such as in a flywheel energy storage device includes a pair of calipers disposed on opposed sides of the rotor for actuating a pair of annular friction discs into engagement with opposed sides of the rotor. Each caliper includes a mounting ring on its outer edge and an inner shallow annular groove in which it disposed one of the friction discs. A circulating fluid under pressure is directed into each annular groove for urging each friction disc into engagement with one of the opposed surfaces of the rotor for safely bringing the rotor to a stop such as in an emergency. The circulating fluid removes the heat generated by the braking action, while the controlled pressure applied by the discs also controls the position of the rotor when static such as during initialization.
    Type: Application
    Filed: July 30, 2007
    Publication date: February 5, 2009
    Applicant: The BOEING COMPANY
    Inventors: Carl R. McIver, Kevin E. McCrary, John R. Hull, John A. Mittleider