Patents by Inventor Christopher Kerley

Christopher Kerley 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).

  • Publication number: 20060288477
    Abstract: The invention is entirely new in that there is no other product known to the inventor which accomplishes the aim of enabling an individual to dry his or her feet without stooping or bending and without putting a towel or rug on the floor. The invention quite simply is a water resistant base portion which stays put on the tub (but is easily removable therefrom), accompanied by a convertible portion on which there is a towel mounted, which is easily removable from the base portion for cleaning.
    Type: Application
    Filed: June 22, 2005
    Publication date: December 28, 2006
    Inventor: Christopher Kerley
  • Patent number: 6547476
    Abstract: An integrated separation system and interface structure is disclosed for a variety of deployment applications. In one embodiment, a Universal Spacecraft Separation Node (100) includes a separation nut assembly (102), a separation spring assembly (104) an LV node fitting (106) and an SC node fitting (108). The LV node fitting (106) is connected to a launch vehicle (210) and the SC node fitting (108) is connected to a spacecraft (216). The separation nut assembly (102) holds the fittings (106 and 108) together until separation is desired. Upon separation, the separation spring assembly (104) provides a force to urge the launch vehicle (210) and spacecraft (216) apart. Prior to separation, an annular tongue (224) of fitting (108) mates with an annular groove (226) of fitting (106) to resist shear forces.
    Type: Grant
    Filed: August 17, 1999
    Date of Patent: April 15, 2003
    Assignee: Lockheed Martin Corporation
    Inventors: Mark Kaszubowski, Christopher Kerley
  • Publication number: 20020164204
    Abstract: An integrated separation system and interface structure is disclosed for a variety of deployment applications. In one embodiment, a Universal Spacecraft Separation Node (100) includes a separation nut assembly (102), a separation spring assembly (104) an LV node fitting (106) and an SC node fitting (108). The LV node fitting (106) is connected to a launch vehicle (210) and the SC node fitting (108) is connected to a spacecraft (216). The separation nut assembly (102) holds the fittings (106 and 108) together until separation is desired. Upon separation, the separation spring assembly (104) provides a force to urge the launch vehicle (210) and spacecraft (216) apart. Prior to separation, an annular tongue (224) of fitting (108) mates with an annular groove (226) of fitting (106) to resist shear forces.
    Type: Application
    Filed: August 17, 1999
    Publication date: November 7, 2002
    Inventors: MARK KASZUBOWSKI, CHRISTOPHER KERLEY