Patents by Inventor William E. Fischer

William E. Fischer 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: 7135238
    Abstract: Oxidation protection of a titanium-based alloy is provided with improved fatigue properties by a titanium aluminide coating of between 2 to 12 microns by diffusing the Al into the Ti at a temperature below the melting point of the Al. The coating is gas deposited and protects the titanium-based alloys from oxidation at high temperature utilization.
    Type: Grant
    Filed: October 29, 2004
    Date of Patent: November 14, 2006
    Assignee: Honeywell International, Inc.
    Inventors: Derek Raybould, Paul Chipko, William E. Fischer
  • Patent number: 6855212
    Abstract: Oxidation protection of a titanium-based alloy is provided with improved fatigue properties by a titanium aluminide coating of between 2 to 12 microns by diffusing the Al into the Ti at a temperature below the melting point of the Al. The coating is gas deposited and protects the titanium-based alloys from oxidation at high temperature utilization.
    Type: Grant
    Filed: February 15, 2002
    Date of Patent: February 15, 2005
    Assignee: Honeywell International Inc.
    Inventors: Derek Raybould, Paul Chipko, William E. Fischer
  • Publication number: 20030155043
    Abstract: Oxidation protection of a titanium-based alloy is provided with improved fatigue properties by a titanium aluminide coating of between 2 to 12 microns by diffusing the Al into the Ti at a temperature below the melting point of the Al. The coating is gas deposited and protects the titanium-based alloys from oxidation at high temperature utilization.
    Type: Application
    Filed: February 15, 2002
    Publication date: August 21, 2003
    Applicant: Honeywell International, Inc.
    Inventors: Derek Raybould, Paul Chipko, William E. Fischer
  • Patent number: 6103386
    Abstract: A thermal barrier coating for superalloy turbine engine vanes and blades that are exposed to high temperature gas is disclosed. The coating includes an aluminide or MCrAlY layer, an alumina layer, and a ceramic top layer. The ceramic layer has a columnar grain microstructure. A bond inhibitor is disposed in the gaps between the columnar grains. This inhibitor is preferably alumina.
    Type: Grant
    Filed: October 6, 1997
    Date of Patent: August 15, 2000
    Inventors: Derek Raybould, Thomas E. Strangman, William E. Fischer, Paul A. Chipko