Patents Represented by Attorney, Agent or Law Firm Larry N. Ginsberg
  • Patent number: 6829884
    Abstract: In a first assembly step a coolant liner is formed having an outside surface. A plurality of coolant channels are formed on the outside surface. At least two inner conformal throat support sections and at least two outer conformal throat support sections are formed. The two inner conformal throat support sections are formed around the outside surface of the coolant liner to form a closed inner conformal throat outside surface. The inner conformal throat support sections are joined at inner throat seam lines. At least two outer conformal throat support sections are assembled around the closed inner conformal throat outside surface so as to cover the inner throat seam lines, to form a liner throat support assembly. An inlet manifold and an outlet manifold are assembled around the liner throat support assembly to form a hot isostatic press (HIP) assembly. A HIP'ed assembly is formed by HIP'ing the HIP assembly.
    Type: Grant
    Filed: November 19, 2002
    Date of Patent: December 14, 2004
    Assignee: The Boeing Company
    Inventors: Jeffry A. Fint, Douglas S. Ades, Michael B. Hankins, Maynard L. Stangeland
  • Patent number: 6557799
    Abstract: An acoustically treated bullnose fairing assembly for a thrust reverser of an aircraft, the thrust reverser having an outer fixed structure and a stowable blocker door. The bullnose fairing assembly includes a back sheet, a face sheet and a honeycomb structure positioned between the face sheet and the back sheet—these three items being bonded together and securely affixed to an outer fixed structure of the thrust reverser. The back sheet has a forward end and a back end. The face sheet has a forward portion and a back portion, the back portion being aft of a forward edge of the blocker door when the blocker door is stowed. The forward portion of the face sheet is perforated. The perforated forward portion of the face sheet cooperates with the honeycomb structure to maximize the acoustic performance of the thrust reverser.
    Type: Grant
    Filed: November 9, 2001
    Date of Patent: May 6, 2003
    Assignee: The Boeing Company
    Inventor: Joe E. Sternberger
  • Patent number: 5534697
    Abstract: An electro-optical sensor system for use in observing objects. A staring sensor is provided which includes a staring array of mid-wave infrared (IR) detectors for providing real-time observations of objects. A preprocessor system is connected to the staring sensor for providing temporal filtration of the real-time observations. A remote control is provided for controlling the temporal filtration.
    Type: Grant
    Filed: September 2, 1994
    Date of Patent: July 9, 1996
    Assignee: Rockwell International Corporation
    Inventors: Veron R. Creekmore, John E. Davis