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: 11130329Abstract: 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: GrantFiled: February 7, 2020Date of Patent: September 28, 2021Assignee: The Boeing CompanyInventors: Carl R. McIver, Brice A. Johnson, Michael R. Anderson
-
Publication number: 20210245491Abstract: 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: ApplicationFiled: February 7, 2020Publication date: August 12, 2021Applicant: The Boeing CompanyInventors: Carl R. McIver, Brice A. Johnson, Michael R. Anderson
-
Patent number: 9057362Abstract: 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: GrantFiled: September 28, 2011Date of Patent: June 16, 2015Assignee: The Boeing CompanyInventor: Carl R. McIver
-
Patent number: 9019683Abstract: 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: GrantFiled: April 24, 2014Date of Patent: April 28, 2015Assignee: The Boeing CompanyInventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin E. McCrary
-
Publication number: 20140235083Abstract: 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: ApplicationFiled: April 24, 2014Publication date: August 21, 2014Applicant: The Boeing CompanyInventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin E. McCrary
-
Patent number: 8717735Abstract: 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: GrantFiled: December 14, 2011Date of Patent: May 6, 2014Assignee: The Boeing CompanyInventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin McCrary
-
Publication number: 20130153136Abstract: 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: ApplicationFiled: December 14, 2011Publication date: June 20, 2013Applicant: THE BOEING COMPANYInventors: Arthur C. Day, James P. Irwin, Eddie Kwon, Carl R. McIver, Kevin McCrary
-
Publication number: 20130078112Abstract: 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: ApplicationFiled: September 28, 2011Publication date: March 28, 2013Applicant: THE BOEING COMPANYInventor: Carl R. McIver
-
Patent number: 8020673Abstract: 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: GrantFiled: July 30, 2007Date of Patent: September 20, 2011Assignee: The Boeing CompanyInventors: Carl R. McIver, Kevin E. McCrary, John R. Hull, John A Mittleider
-
Patent number: 7633203Abstract: 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: GrantFiled: January 2, 2008Date of Patent: December 15, 2009Assignee: The Boeing CompanyInventors: John R. Hull, Carl R. McIver, John A. Mittleider
-
Publication number: 20090170707Abstract: 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: ApplicationFiled: January 2, 2008Publication date: July 2, 2009Applicant: The Boeing CompanyInventors: John R. Hull, Carl R. McIver, John A. Mittleider
-
Publication number: 20090033145Abstract: 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: ApplicationFiled: July 30, 2007Publication date: February 5, 2009Applicant: The BOEING COMPANYInventors: Carl R. McIver, Kevin E. McCrary, John R. Hull, John A. Mittleider