Patents by Inventor Craig English

Craig English 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: 11920871
    Abstract: A thermal battery system may be provided comprising: a vessel comprising a phase change material and a gas; a heat exchanger configured to transfer heat to and/or from the phase change material; a temperature sensor configured to detect an indication of a temperature of the gas; a pressure sensor configured to detect an indication of a pressure of the gas; and a processor configured to determine a state of charge of the thermal battery system from the indication of the pressure and the indication of the temperature of the gas.
    Type: Grant
    Filed: November 25, 2020
    Date of Patent: March 5, 2024
    Assignee: ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC.
    Inventors: Nader Maharmeh, Craig English, Eric Donovan, Eugene Jansen, Ryan Young
  • Publication number: 20220163270
    Abstract: A thermal battery system may be provided comprising: a vessel comprising a phase change material and a gas; a heat exchanger configured to transfer heat to and/or from the phase change material; a temperature sensor configured to detect an indication of a temperature of the gas; a pressure sensor configured to detect an indication of a pressure of the gas; and a processor configured to determine a state of charge of the thermal battery system from the indication of the pressure and the indication of the temperature of the gas.
    Type: Application
    Filed: November 25, 2020
    Publication date: May 26, 2022
    Applicant: Rolls-Royce North American Technologies Inc.
    Inventors: Nader Maharmeh, Craig English, Eric Donovan, Eugene Jansen, Ryan Young
  • Patent number: 10208668
    Abstract: A cooling system for a gas turbine is provided that may include a drive shaft, a shield of a combustor of the gas turbine engine, and a conduit. The drive shaft may be configured to mechanically couple a compressor of the gas turbine engine to a turbine of the gas turbine engine. The shield may be positioned between the compressor and the turbine. The combustor may be configured to drive the turbine. The conduit may be configured to supply a cooling fluid to a gap between an outer surface of the drive shaft and the shield of the combustor.
    Type: Grant
    Filed: September 30, 2015
    Date of Patent: February 19, 2019
    Assignees: ROLLS-ROYCE CORPORATION, ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC.
    Inventors: Joseph Clegg, Craig English, Behram Kapadia, Kenneth M. Pesyna, Jason Lee Swindle, Jason Wayne Rector, Christopher Vincent, Nicholas D. Metzger, Daniel G. Edwards
  • Publication number: 20170089263
    Abstract: A cooling system for a gas turbine is provided that may include a drive shaft, a shield of a combustor of the gas turbine engine, and a conduit. The drive shaft may be configured to mechanically couple a compressor of the gas turbine engine to a turbine of the gas turbine engine. The shield may be positioned between the compressor and the turbine. The combustor may be configured to drive the turbine. The conduit may be configured to supply a cooling fluid to a gap between an outer surface of the drive shaft and the shield of the combustor.
    Type: Application
    Filed: September 30, 2015
    Publication date: March 30, 2017
    Inventors: Joseph Clegg, Craig English, Behram Kapadia, Kenneth M. Pesyna, Jason Lee Swindle, Jason Wayne Rector, Christopher Vincent, Nicholas D. Metzger, Daniel G. Edwards