Patents by Inventor Mark W. Shorey

Mark W. Shorey 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: 10647856
    Abstract: Aspects described herein generally relate to a material that is the reaction product of: a binder; a curing agent; and a zinc pyrithione represented by the formula: R1, R2, R3, R4, R5, R6, R7, and R8 is independently hydrogen, alkyl, cycloalkyl, alkoxyl, hydroxyl, aryl, or heterocyclyl, uses thereof as a heatshield material, and heatshields.
    Type: Grant
    Filed: November 4, 2016
    Date of Patent: May 12, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Kevin O. Gaw, Mark W. Shorey, Holly M. Rhoe
  • Publication number: 20180127597
    Abstract: Aspects described herein generally relate to a material that is the reaction product of: a binder; a curing agent; and a zinc pyrithione represented by the formula: R1, R2, R3, R4, R5, R6, R7, and R8 is independently hydrogen, alkyl, cycloalkyl, alkoxyl, hydroxyl, aryl, or heterocyclyl, uses thereof as a heatshield material, and heatshields.
    Type: Application
    Filed: November 4, 2016
    Publication date: May 10, 2018
    Applicant: THE BOEING COMPANY
    Inventors: Kevin O. GAW, Mark W. SHOREY, Holly M. RHOE
  • Patent number: 6299106
    Abstract: A thermal insulating blanket for insulating a surface from extreme external temperatures. The blanket includes ceramic fiber batting that insulates the surface from the external temperatures, a frame for supporting the ceramic fiber batting and preventing the ceramic fiber batting from sagging, and a ceramic fabric cover enclosing the ceramic fiber batting and the frame. The ceramic fabric cover defines a first side of the blanket facing externally, and a second side opposite the first side and facing the surface. The blanket also includes a low profile fastener for coupling the blanket to the surface. The fastener is coupled and decoupled from the surface by applying pressure to the first side of the blanket proximate the fastener.
    Type: Grant
    Filed: March 9, 1999
    Date of Patent: October 9, 2001
    Assignee: The Boeing Company
    Inventor: Mark W. Shorey
  • Patent number: 6007026
    Abstract: A system for removably mounting a thermal insulation blanket to a structure such as a launch vehicle exterior surface, includes a blanket formed of a layer of batting with a substantially rigid frame positioned against one side, and a cover (preferably fabric) surrounding the batting layer. The cover holds the frame in place on the surface of the batting. Preferably, the blanket is quilted. For space launch applications, the batting, cover, and quilting thread are ceramic fiber materials suitable for high temperature use. Fasteners are mounted on the frame and extend outward from the cover. Corresponding mating fasteners are mounted on the structure in an arrangement so as to be positioned to engage with the fasteners extending from the blanket cover. A flat or curved blanket can be provided with a frame material that can be shaped to the desired curve.
    Type: Grant
    Filed: June 30, 1997
    Date of Patent: December 28, 1999
    Assignee: The Boeing Company
    Inventor: Mark W. Shorey
  • Patent number: 4802572
    Abstract: A cargo roller system (10) having drive rollers (13) and idler rollers (19) mounted in a tray (14) and selectively engageable with a motor (30) through a gear train (44). The motor (30) engages the gear train (44) through an idler gear (48) mounted in a motor mount (32) and a driven gear (50) mounted to the shaft (52) of the gear train (44). Coupling assemblies (60) connect the two halves of the gear train (44) to the driven gear (50). The coupling assembly (60) comprises a shaft (52) having a cylindrical piston (62) formed on one end thereof and a cylinder (66) slidably receiving the piston (62) on the other end thereof. A V-shaped opening (70) in the outer wall (72) of the cylinder (66) cooperates with a retaining pin (74) passing through the piston (62) translationally moving the gear train (44) into engagement with the rollers as the cylinder (66) is rotated by the motor (30).
    Type: Grant
    Filed: November 2, 1987
    Date of Patent: February 7, 1989
    Assignee: The Boeing Company
    Inventors: Thomas H. Shorey, Mark W. Shorey