Patents by Inventor James P. Nokes

James P. Nokes 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: 8916067
    Abstract: A method and composition wherein carbonaceous nano-scaled filler material is subjected to atmospheric plasma treatment using carbon monoxide as the active gas. The treatment with carbon monoxide plasma has been found to significantly increase the incorporation of oxygen groups on the surface of the filler material without degrading the surface and thus serves to increase wettability and dispersion throughout the matrix. The composite that incorporates the treated filler material has enhanced mechanical and electrical properties.
    Type: Grant
    Filed: October 19, 2011
    Date of Patent: December 23, 2014
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaidivar, James P. Nokes, Hyun I. Kim
  • Patent number: 8904887
    Abstract: A radio-frequency transparent window having internal conduits for the passage of cooling fluid is configured for simulating a highly uniform thermal environment for testing a device intended for use in space. The device to be tested is placed within a chamber in which a vacuum condition is maintained by a radio-frequency transparent pressure window under a pressure seal. Within the chamber, the thermal window is positioned adjacent, but not in contact with, the pressure window. A radio frequency signal is capable of passing directly through both the thermal window and the pressure window to permit communication with the device being tested within the housing. The thermal window is not in contact with the device so there in no conduction of heat from the device. Radiant heat transfer may occur from the device to the thermal window.
    Type: Grant
    Filed: November 17, 2011
    Date of Patent: December 9, 2014
    Assignee: The Aerospace Corporation
    Inventors: Michael A. Tockstein, James P. Nokes, Jon V. Osborn, Dhruv N. Patel, Alan R. Hopkins, John S. Williams, Gary N. Harper
  • Patent number: 8858070
    Abstract: A system and method for measuring a glass transition temperature of a hydrophobic polymer having a surface tagged with an atmospheric plasma.
    Type: Grant
    Filed: June 3, 2011
    Date of Patent: October 14, 2014
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaldivar, James P. Nokes
  • Patent number: 8551287
    Abstract: A hybrid adhesive incorporating cyanate ester and/or epoxy materials and utilizing atmospheric plasma treatment provides stronger, more reliable joints in structural composite parts.
    Type: Grant
    Filed: October 3, 2010
    Date of Patent: October 8, 2013
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaldivar, James P. Nokes
  • Publication number: 20130125676
    Abstract: A radio-frequency transparent window having internal conduits for the passage of cooling fluid is configured for simulating a highly uniform thermal environment for testing a device intended for use in space. The device to be tested is placed within a chamber in which a vacuum condition is maintained by a radio-frequency transparent pressure window under a pressure seal. Within the chamber, the thermal window is positioned adjacent, but not in contact with, the pressure window. A radio frequency signal is capable of passing directly through both the thermal window and the pressure window to permit communication with the device being tested within the housing. The thermal window is not in contact with the device so there in no conduction of heat from the device. Radiant heat transfer may occur from the device to the thermal window.
    Type: Application
    Filed: November 17, 2011
    Publication date: May 23, 2013
    Applicant: THE AEROSPACE CORPORATION
    Inventors: MICHAEL A. TOCKSTEIN, JAMES P. NOKES, JON V. OSBORN, DHRUV N. PATEL, ALAN R. HOPKINS, JOHN S. WILLIAMS
  • Publication number: 20130099170
    Abstract: A method and composition wherein carbonaceous nano-scaled filler material is subjected to atmospheric plasma treatment using carbon monoxide as the active gas. The treatment with carbon monoxide plasma has been found to significantly increase the incorporation of oxygen groups on the surface of the filler material without degrading the surface and thus serves to increase wettability and dispersion throughout the matrix. The composite that incorporates the treated filler material has enhanced mechanical and electrical properties.
    Type: Application
    Filed: October 19, 2011
    Publication date: April 25, 2013
    Applicant: THE AEROSPACE CORPORATION
    Inventors: RAFAEL J. ZALDIVAR, James P. Nokes, Hyun I. Kim
  • Publication number: 20120307860
    Abstract: A system and method for measuring a glass transition temperature of a hydrophobic polymer having a surface tagged with an atmospheric plasma.
    Type: Application
    Filed: June 3, 2011
    Publication date: December 6, 2012
    Inventors: Rafael J. Zaldivar, James P. Nokes
  • Publication number: 20120082851
    Abstract: A hybrid adhesive incorporating cyanate ester and/or epoxy materials and utilizing atmospheric plasma treatment provides stronger, more reliable joints in structural composite parts.
    Type: Application
    Filed: October 3, 2010
    Publication date: April 5, 2012
    Inventors: Rafael J. Zaldivar, James P. Nokes
  • Publication number: 20020196834
    Abstract: A glass transition temperature Tg measurement system includes a probe point penetrating into a sample under test that has been heated by a heater to a temperature where the sample undergoes a phase change from a solid to a semisolid. A thermocouple is used to measure the temperature while a motion transducer is used to measure the amount of penetration. The penetration amount sharply increases at the glass transition temperature. A portable unit can be used in the field to test the Tg properties of various composite materials used, for example, in structures including buildings and bridges.
    Type: Application
    Filed: June 22, 2001
    Publication date: December 26, 2002
    Inventors: Rafael J. Zaldivar, James P. Nokes, Gary F. Hawkins
  • Patent number: 6425686
    Abstract: A glass transition temperature Tg measurement system includes a probe point penetrating into a sample under test that has been heated by a heater to a temperature where the sample undergoes a phase change from a solid to a semisolid. A thermocouple is used to measure the temperature while a motion transducer is used to measure the amount of penetration. The penetration amount sharply increases at the glass transition temperature. A portable unit can be used in the field to test the Tg properties of various composite materials used, for example, in structures including buildings and bridges.
    Type: Grant
    Filed: June 9, 2000
    Date of Patent: July 30, 2002
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaldivar, James P. Nokes, Gary F. Hawkins
  • Patent number: 6400898
    Abstract: A heater preferably having a plurality of equally spaced heating elements, such as heating lamps, provides a uniform heat radiation pattern for quickly and uniformly heating a large surface area using motor controlled wheels for translating the heater at a constant rate of speed across the surface of a structure in a desired pattern. The heater having a handle for operator manipulation for guiding and turning the heater in the desired pattern. The heater, having a wide lateral distance for radiating a wide uniform radiation pattern is suitable for thermographic application for imaging the heated surface and detecting subsurface defects in the structure, such as composite overwrapped concrete bridge and building structures subject where debonding of the composite/concrete interface is a concern.
    Type: Grant
    Filed: October 18, 2000
    Date of Patent: June 4, 2002
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Eric C. Johnson, James P. Nokes
  • Patent number: 5814734
    Abstract: A thin film stress sensor measures the maximum compressive stress between two elements that are compressed together. The sensor is formed from a thin RTV film impregnated with microballoons and reinforced with carbon fibers to restrain the lateral deformation of the RTV so that more uniform pressure can be exerted on the microballoons when the sensors are uniaxially compressed.
    Type: Grant
    Filed: June 30, 1997
    Date of Patent: September 29, 1998
    Assignee: The Aerospace Corporation
    Inventors: Dick J. Chang, James P. Nokes, Francis Hai
  • Patent number: 5808207
    Abstract: A thin film stress sensor measures the maximum compressive stress between two elements that are compressed together. The sensor is formed from a thin RTV film impregnated with microballoons and reinforced with carbon fibers to restrain the lateral deformation of the RTV so that more uniform pressure can be exerted on the microballoons when the sensors are uniaxially compressed. The testing method includes applying a compressive stress up to an maximum compressive stress to rupture a first portion of the microballoons, and then applying an interrogating pressure causing acoustic emissions emitted by a second portion of the microballoons when the interrogating pressure equals the equivalent maximum compressive stress, so as to determine the maximum compressive stress.
    Type: Grant
    Filed: June 30, 1997
    Date of Patent: September 15, 1998
    Assignee: The Aerospace Corporation
    Inventors: Dick J. Chang, James P. Nokes, Francis Hai