Patents by Inventor Keith R. Karasek

Keith R. Karasek 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: 6797332
    Abstract: A method for forming a carbon deposit inhibiting thermal barrier coating for an internal element or component of a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.
    Type: Grant
    Filed: September 9, 2003
    Date of Patent: September 28, 2004
    Assignee: Honeywell International, Inc.
    Inventors: Thomas E. Strangman, Dave Narasimhan, Jeffrey P. Armstrong, Keith R. Karasek
  • Publication number: 20040047998
    Abstract: A carbon deposit inhibiting thermal barrier coating for an internal element or component in a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.
    Type: Application
    Filed: September 9, 2003
    Publication date: March 11, 2004
    Inventors: Thomas E. Strangman, Dave Narasimhan, Jeffrey P. Armstrong, Keith R. Karasek
  • Patent number: 6656600
    Abstract: A carbon deposit inhibiting thermal barrier coating for an internal element or component in a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.
    Type: Grant
    Filed: August 16, 2001
    Date of Patent: December 2, 2003
    Assignee: Honeywell International Inc.
    Inventors: Thomas E. Strangman, Dave Narasimhan, Jeffrey P. Armstrong, Keith R. Karasek
  • Publication number: 20030035945
    Abstract: A carbon deposit inhibiting thermal barrier coating for an internal element or component in a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.
    Type: Application
    Filed: August 16, 2001
    Publication date: February 20, 2003
    Applicant: Honeywell International, Inc.
    Inventors: Thomas E. Strangman, Dave Narasimhan, Jeffrey P. Armstrong, Keith R. Karasek
  • Patent number: 4923719
    Abstract: This invention relates to a method of coating fibers by contacting the fibers with an organochlorosilane, drying and heating the fibers at a temperature of about 300.degree. to 500.degree. C., thereby coating the fibers. The choice of organochlorosilane and atmosphere under which the heating takes place will determine the composition of the coating.
    Type: Grant
    Filed: August 22, 1988
    Date of Patent: May 8, 1990
    Assignee: Allied-Signal Inc.
    Inventors: Keith R. Karasek, William L. Olson, Jeffry T. Donner
  • Patent number: 4732877
    Abstract: Alumina fibers whose surface is coated with zirconia to retain their identity in an alumina matrix when the mixture is sintered at temperatures needed to form a fully dense ceramic. The resulting fully dense ceramic composite shows the beneficial effects of such reinforcing fibers by having increased crack toughness.
    Type: Grant
    Filed: May 5, 1986
    Date of Patent: March 22, 1988
    Assignee: Allied-Signal Inc.
    Inventors: William L. Olson, Keith R. Karasek
  • Patent number: 4508158
    Abstract: Methods are disclosed for manufacturing graphite fiber metal matrix bearing materials using liquid metal pressure infiltration to achieve a high degree of intimate wetting, contact and infiltration of a compliant metal between and around graphite (carbon) fibers to provide graphite fiber metal matrix bearing material having a predetermined volume percentage of graphite fibers. In one embodiment, graphite fibers are wrapped around a removable cylindrical mandrel and the graphite fiber-wrapped mandrel is inserted into a mold and the mold which contains a liquid compliant metal, such as lead, to cause intimate wetting, contact and infiltration of the compliant metal between and around all of the graphite fibers.
    Type: Grant
    Filed: February 22, 1983
    Date of Patent: April 2, 1985
    Assignee: International Harvester Company
    Inventors: Maurice F. Amateau, Keith R. Karasek