Patents by Inventor Richard E. Wallsom

Richard E. Wallsom 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: 4963052
    Abstract: A mechanical end joint system for connecting structural column elements and eliminating the possibility of free movement between joint halves during loading or vibration has a node joint body having a cylindrical engaging end, and a column end body having a cylindrical engaging end. Each of the cylindrical engaging ends has an integral semicircular tongue and an integral semicircular groove. The node joint body has a conical aperture at the center of its cylindrical engaging end. The column end joint body has an internal latch mechanism housed therein, with the internal latch mechanism having a latch bolt element slidably disposed along the longitudinal axis of the column end joint body at the cylindrical engaging end. The internal latch mechanism also has a spring mechanism disposed along the longitudinal axis of the column end joint body, as well as a compressible preload mechanism and plunger means housed therein.
    Type: Grant
    Filed: March 30, 1990
    Date of Patent: October 16, 1990
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Harold G. Bush, Martin M. Mikulas, Jr., Richard E. Wallsom
  • Patent number: 4685535
    Abstract: A mobile remote manipulator system 10 is disclosed for assembly, repair and logistics transport on, around and about a space station square bay truss structure. The vehicle is supported by a square track arrangement supported by guide pins integral with the space station truss structure 12 and located at each truss node 40. Propulsion is provided by a central push-pull drive mechanism 20 that extends out from the vehicle one full structural bay over the truss and locks drive rods 38 into the guide pins 30. The draw bar is now retracted and the mobile remote manipulator system is pulled onto the next adjacent structural bay. Thus, translation of the vehicle is "inchworm" style. The drive bar can be locked onto two (2) guide pins while the extendable draw bar is within the vehicle and then push the vehicle away one bay providing bi-directional push-pull drive.
    Type: Grant
    Filed: July 31, 1985
    Date of Patent: August 11, 1987
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Harold G. Bush, Martin M. Mikulas, Jr., Richard E. Wallsom, J. Kermit Jensen
  • Patent number: 4578920
    Abstract: A collapsible-expandable truss structure 16 including first and second spaced surface truss layers (18, 20) having an attached core layer 22 is disclosed. The surface truss layers are composed of a plurality of linear struts 40 arranged in multiple triangular configurations with each linear strut being hinged at its center 41 and hingedly connected at each end thereof to a nodular joint 25. A passive spring 64 serves as the expansion force to move the folded struts from a stowed collapsed position to a deployed operative final truss configuration. Damper 62 controls the rate of spring 64 expansion for synchronized deployment of truss 16 as the folded configuration is released for deployment by restraint belts 72a and 73a synchronously extending under the control of motor (71) driven spools 72 and 73.
    Type: Grant
    Filed: November 30, 1983
    Date of Patent: April 1, 1986
    Assignee: The United States of America as represented by the secretary of the United States National Aeronautics and Space Administration
    Inventors: Harold G. Bush, Martin M. Mikulas, Jr., Richard E. Wallsom
  • Patent number: 4518277
    Abstract: A device for connecting, rotating and locking together a pair of structural half-columns 11 is disclosed. The device is composed of an identical pair of cyclindrical hub assemblies 12,12a connected at their inner faces by a spring loaded hinge 20; each hub assembly having a structural half-column attached to its outer end. Each hub assembly has a spring loading locking ring 14,14a member movably attached adjacent to its inner face and includes a latch 32,32a member for holding the locking ring in a rotated position subject to the force of its spring. Each hub assembly also has a hammer 36,36a member for releasing the latch on the opposing hub assembly when the hub assemblies are rotated together. The spring loaded hinge connecting the hub assemblies rotates the hub assemblies and attached structural half-columns together bringing the inner faces of the opposing hub assemblies into contact with one another.
    Type: Grant
    Filed: June 11, 1982
    Date of Patent: May 21, 1985
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Harold G. Bush, Richard E. Wallsom
  • Patent number: 4340318
    Abstract: A mechanical end joint system, useful for the transverse connection of strut elements to a common node, comprises a node joint half 15 with semicircular tongue 14 and groove 60 and a strut joint half 24 with semicircular tongue 25 and groove 21. The two joint halves are engaged transversely and the connection is made secure by the inherent physical property characteristics of locking latches 12 and 26 (FIGS. 1-6) or by a spring-actioned shaft 70 (FIG. 7). A quick release mechanism (FIG. 7) provides rapid disengagement of the joint halves.
    Type: Grant
    Filed: December 5, 1979
    Date of Patent: July 20, 1982
    Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Harold G. Bush, Richard E. Wallsom