Patents by Inventor Sean A. Hainze

Sean A. Hainze 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: 8091460
    Abstract: The invention efficiently and effectively secures and releases a rail-launched missile. An asymmetrical secure-release wheel (70) is defined by several surfaces which extend radially outward from a pivot hole (70K). The surfaces include a wheel unlatch surface (70H), a wheel notch stop surface (70D), a wheel detent surface (70G), a clockwise stop surface (70C) and a counterclockwise stop surface (70B). The wheel (70) is rotatable within a wheel housing (72). When a missile is loaded onto the launch rail, the middle shoe of the missile engages the detent surface (70G) of the wheel. During missile launch, the plume of the missile moves a trigger (110) which pulls a connecting rod (52) aft which results in a wheel lock (78) being disengaged from the detent surface (70G). A microswitch (56) provides a signal indicating whether the wheel (70) is in a latched or unlatched state.
    Type: Grant
    Filed: April 29, 2010
    Date of Patent: January 10, 2012
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventors: Sean A. Hainze, Donald E. Davis
  • Publication number: 20110265637
    Abstract: The invention efficiently and effectively secures and releases a rail-launched missile. An asymmetrical secure-release wheel (70) is defined by several surfaces which extend radially outward from a pivot hole (70K). The surfaces include a wheel unlatch surface (70H), a wheel notch stop surface (70D), a wheel detent surface (70G), a clockwise stop surface (70C) and a counterclockwise stop surface (70B). The wheel (70) is rotatable within a wheel housing (72). When a missile is loaded onto the launch rail, the middle shoe of the missile engages the detent surface (70G) of the wheel. During missile launch, the plume of the missile moves a trigger (110) which pulls a connecting rod (52) aft which results in a wheel lock (78) being disengaged from the detent surface (70G). A microswitch (56) provides a signal indicating whether the wheel (70) is in a latched or unlatched state.
    Type: Application
    Filed: April 29, 2010
    Publication date: November 3, 2011
    Applicant: United States of America as represented by the Secretary of the Army
    Inventors: Sean A. Hainze, Donald E. Davis