Patents by Inventor Steve L. Patterson

Steve L. Patterson 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: 11718384
    Abstract: A hat-stringer assembly for an aircraft comprises a hat stringer with a first hat-stringer leg, a second hat-stringer leg, a first hat-stringer sidewall, a connecting wall, a second hat-stringer sidewall, and a ventilation opening, extending through the connecting wall. The hat stringer assembly also comprises a fitting, comprising a first channel member in contact with the first hat-stringer sidewall and the first hat-stringer leg. The fitting also comprises a second channel member in contact with the second hat-stringer sidewall and the second hat-stringer leg. The fitting further comprises a web cap, in contact with the first channel member and the second channel member. The web cap comprises a web-cap opening, which is in fluidic communication with the ventilation opening.
    Type: Grant
    Filed: July 30, 2021
    Date of Patent: August 8, 2023
    Assignee: The Boeing Company
    Inventors: Steve L. Patterson, Daniel M. Levine, Jeffrey E. Barnes, Jeffrey F. Stulc, Christopher R. Loesche, Garrett C. Hanson
  • Patent number: 11597495
    Abstract: A vented hat stringer for an aircraft comprises a first hat-stringer leg with a first-hat-stringer-leg surface, a second hat-stringer leg with a second-hat-stringer-leg surface, a first hat-stringer sidewall, a second hat-stringer sidewall, and a hat-stringer connecting wall, comprising a hat-stringer-connecting-wall surface and a virtual hat-stringer-connecting-wall symmetry plane, passing through hat-stringer connecting wall. The vented hat stringer further comprises a ventilation opening, extending through at least one of the first hat-stringer sidewall or the hat-stringer connecting wall, or extending through at least one of the second hat-stringer sidewall or the hat-stringer connecting wall. The ventilation opening defines a ventilation-opening centerline, wherein the ventilation-opening centerline does not coincide with the virtual hat-stringer-connecting-wall symmetry plane.
    Type: Grant
    Filed: July 30, 2021
    Date of Patent: March 7, 2023
    Assignee: The Boeing Company
    Inventors: Steve L. Patterson, Daniel M. Levine, Jeffrey E. Barnes, Jeffrey F. Stulc, Christopher R. Loesche, Garrett C. Hanson
  • Publication number: 20230030180
    Abstract: A vented hat stringer for an aircraft comprises a first hat-stringer leg with a first-hat-stringer-leg surface, a second hat-stringer leg with a second-hat-stringer-leg surface, a first hat-stringer sidewall, a second hat-stringer sidewall, and a hat-stringer connecting wall, comprising a hat-stringer-connecting-wall surface and a virtual hat-stringer-connecting-wall symmetry plane, passing through hat-stringer connecting wall. The vented hat stringer further comprises a ventilation opening, extending through at least one of the first hat-stringer sidewall or the hat-stringer connecting wall, or extending through at least one of the second hat-stringer sidewall (116) or the hat-stringer connecting wall. The ventilation opening defines a ventilation-opening centerline, wherein the ventilation-opening centerline does not coincide with the virtual hat-stringer-connecting-wall symmetry plane.
    Type: Application
    Filed: July 30, 2021
    Publication date: February 2, 2023
    Applicant: The Boeing Company
    Inventors: Steve L. Patterson, Daniel M. Levine, Jeffrey E. Barnes, Jeffrey F. Stulc, Christopher R. Loesche, Garrett C. Hanson
  • Publication number: 20230031639
    Abstract: A hat-stringer assembly (100) for an aircraft (500) comprises a hat stringer (110) with a first hat-stringer leg (140), a second hat-stringer leg (150), a first hat-stringer sidewall (114), a connecting wall (112), a second hat-stringer sidewall (116), and a ventilation opening (128), extending through the connecting wall (112). The hat stringer assembly (100) also comprises a fitting (200), comprising a first channel member (210) in contact with the first hat-stringer sidewall (114) and the first hat-stringer leg (140). The fitting (200) also comprises a second channel member (240) in contact with the second hat-stringer sidewall (116) and the second hat-stringer leg (150). The fitting (200) further comprises a web cap (260), in contact with the first channel member (210) and the second channel member (240). The web cap (260) comprises a web-cap opening (262), which is in fluidic communication with the ventilation opening (128).
    Type: Application
    Filed: July 30, 2021
    Publication date: February 2, 2023
    Applicant: The Boeing Company
    Inventors: Steve L. Patterson, Daniel M. Levine, Jeffrey E. Barnes, Jeffrey F. Stulc, Christopher R. Loesche, Garrett C. Hanson
  • Publication number: 20090078828
    Abstract: Anti-ice valve components are provided that include a servo housing, a valve body, and a transfer tube. The servo housing includes a surface having a cavity formed therein. The valve body is spaced apart from the servo housing and includes a surface having a cavity formed therein. The transfer tube has a first end, a second end, and a length, where the first end is disposed in the servo housing cavity, the second end is disposed in the valve body cavity, and the length extends between the first end and the second end and has a portion forming a bend of at least 180 degrees.
    Type: Application
    Filed: September 25, 2007
    Publication date: March 26, 2009
    Applicant: HONEYWELL INTERNATIONAL, INC.
    Inventors: Maureen Sugai, Don J. Atkins, William H. Reed, Joel E. LaBenz, Steve L. Patterson, Dan E. Hitzler