Patents by Inventor Thomas H. Brayden

Thomas H. Brayden 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: 6052191
    Abstract: A coating thickness measurement system (10) for measuring a thickness of a coating (12) on a coated substrate (14) is provided. The coating thickness measurement system (10) may comprise a light source (16), a detector system (18), and a processor (20). The light source (16) directs a light beam (22) at an angle (26) oblique to an axis (28) of the coating (12). The light beam (22) striking the coating (12) produces a reflected light beam (36). The detector system (18) measures a reflectivity of the coating (12). The processor (20) receives the reflectivity measurement and determines the reflectivity of the coating (12). The thickness of the coating (12) is determined from the reflectivity of the coating (12).
    Type: Grant
    Filed: October 13, 1998
    Date of Patent: April 18, 2000
    Assignee: Northrop Grumman Corporation
    Inventors: Thomas H. Brayden, Jr., Thomas D. Winters, Jr.
  • Patent number: 5242651
    Abstract: A method of processing a composite structure in an autoclave involves producing a layup (10) with a low density honeycomb core (12) covered by resin impregnated composite face plies (14). The layup is sealed to a mold (18) under a vacuum bag (20). The layup is then cured in an autoclave under high temperatures and pressures. A vacuum is applied between the layup (10) and the vacuum bag (20) via a vacuum port (22), thus creating a pressure differential across the bag (20). This creates a compressive consolidating force on the composite face plies (14). Volatiles emitted during curing are drawn away through the vacuum port (22). The core (12) communicates with the autoclave by means of a pressurization tube (26) which penetrates the mold (18) and into the core (12), thus eliminating the pressure differential between the core (12) and the autoclave. Autoclave pressure is communicated throughout the entire core via perforations (13) in the honeycomb core (12).
    Type: Grant
    Filed: July 25, 1990
    Date of Patent: September 7, 1993
    Assignee: Vought Aircraft Company
    Inventors: Thomas H. Brayden, Donald C. Darrow