Patents by Inventor Larry J. Osiecki

Larry J. Osiecki 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: 5897739
    Abstract: A method for making a honeycomb core composite article includes forming a honeycomb core (24) and a precured composite skin (20) having a core edge (32) and a restraint edge (30), respectively. The precured composite skin (20) is placed in combination with a rigid mold member having a mold surface (12s) and the honeycomb core (24) is mated with the precured composite skin (20) to form a mated subassembly (36). An uncured composite skin (22) is laid over the mated subassembly (36) such that a peripheral portion (44) of the uncured composite skin (22) extends beyond the restraint edge (30) by a distance X and such that the peripheral portion (44) is in superposed abutting engagement with the mold surface (12s). The honeycomb core (24), the precured composite skin (20) and the uncured composite skin (22) define a composite lay-up (10) over which a vacuum bag (14) is disposed.
    Type: Grant
    Filed: January 27, 1995
    Date of Patent: April 27, 1999
    Assignee: Sikorsky Aircraft Corporation
    Inventors: William V. Forster, Kenneth M. Nowak, Larry J. Osiecki
  • Patent number: 5558919
    Abstract: A duct cover for use with a duct within a vehicle, the duct cover operative for directing a fluid flow. The duct cover being further operative for minimizing the entrance of foreign object debris into the duct. The duct cover has a flow directing honeycomb portion for conducting the passing fluid flow in a preferred direction. The flow directing honeycomb comprises an array of continuous, polygon shaped open cells which are biased with respect to the initial fluid flow direction. The periphery of the flow directing honeycomb is rigidized to stiffen the same for minimizing the displacements thereof. The rigidity is provided by a framing member comprising upper and lower skin structures affixed to a core material. The framing member is preferably adhesively bonded to the flow directing honeycomb by means of a foaming adhesive and a barrier member. The barrier member is operative for minimizing the expansion of the foaming adhesive into the open cells of the honeycomb.
    Type: Grant
    Filed: September 20, 1993
    Date of Patent: September 24, 1996
    Assignee: United Technologies Corporation
    Inventors: Darryl M. Toni, Peter L. Grant, Craig F. Johnson, Steven R. Hayse, William V. Forster, Kenneth Nowak, Larry J. Osiecki
  • Patent number: 5437756
    Abstract: A simulator dome for a motion base simulator comprises one or more fiber reinforced outer layers, inner layers of a similar material and an intermediate core. The intermediate core is preferably a structural foam of variable density to allow selectively lowering the dome center of gravity to enhance the simulation capabilities of the motion system to simulate various flight maneuvers. By producing the dome from fiber reinforced polymer and using a core of variable density, a dome of unitary construction with no through fasteners is produced, having high strength for withstanding high G maneuvers without cracking or distortion, enhancing simulator effectiveness and increasing the accuracy of the simulated flight conditions.
    Type: Grant
    Filed: June 9, 1994
    Date of Patent: August 1, 1995
    Assignee: United Technologies Corp.
    Inventors: Joseph M. Carlos, Thomas A. Carstensen, William J. Hall, Larry J. Osiecki
  • Patent number: 5182150
    Abstract: A simulator dome for a motion base simulator comprises one or more fiber reinforced outer layers, inner layers of a similar material and an intermediate core. The intermediate core is preferably a structural foam of variable density to allow selectively lowering the dome center of gravity to enhance the simulation capabilities of the motion system to simulate various flight maneuvers. By producing the dome from fiber reinforced polymer and using a core of variable density, a dome of unitary construction with no through fasteners is produced, having high strength for withstanding high G maneuvers without cracking or distortion, enhancing simulator effectiveness and increasing the accuracy of the simulated flight conditions.
    Type: Grant
    Filed: July 16, 1990
    Date of Patent: January 26, 1993
    Assignee: United Technologies, Corp.
    Inventors: Joseph M. Carlos, Thomas A. Carstensen, William J. Hall, Larry J. Osiecki