Patents by Inventor David James Taylor

David James Taylor 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).

  • COLORIMETRIC SWEAT SENSING DEVICE AND METHODS OF MAKING THE SAME
    Publication number: 20240148281
    Abstract: Disclosed herein are disposable devices for measuring sweat having low dead volumes and allowing a quick sensory response. Also disclosed herein are methods of making and using such devices.
    Type: Application
    Filed: January 19, 2022
    Publication date: May 9, 2024
    Inventors: Timothy Charles KING, Andrew Robert TAYLOR, Rachel Elizabeth SMITH, Thomas James O’NEILL, Laura Mae DAGLISH, David John NIGHTINGALE, Jack Lawrence WARREN
  • COMUBSTOR SEAL HAVING MULTIPLE COOLING FLUID PATHWAYS
    Publication number: 20090255267
    Abstract: A combustor for a gas turbine includes a first combustor component and a second combustor component. The second combustor component is at least partially insertable into the first combustor component, and the first combustor component and second combustor component define a combustion fluid pathway. A combustor seal is located between the first combustor component and the second combustor component. The combustor seal defines at least one inner cooling pathway between the combustor seal and the second combustor component and at least one outer cooling pathway between the combustor seal and the first combustor component for cooling the first combustor component and second combustor component. A method for cooling a first combustor component and a second combustor component is also disclosed.
    Type: Application
    Filed: April 10, 2008
    Publication date: October 15, 2009
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Wei Chen, Marcus Byron Huffman, David James Taylor
  • Combustor seal having multiple cooling fluid pathways
    Patent number: 7594401
    Abstract: A combustor for a gas turbine includes a first combustor component and a second combustor component. The second combustor component is at least partially insertable into the first combustor component, and the first combustor component and second combustor component define a combustion fluid pathway. A combustor seal is located between the first combustor component and the second combustor component. The combustor seal defines at least one inner cooling pathway between the combustor seal and the second combustor component and at least one outer cooling pathway between the combustor seal and the first combustor component for cooling the first combustor component and second combustor component. A method for cooling a first combustor component and a second combustor component is also disclosed.
    Type: Grant
    Filed: April 10, 2008
    Date of Patent: September 29, 2009
    Assignee: General Electric Company
    Inventors: Wei Chen, Marcus Byron Huffman, David James Taylor