Solid Propellant Charge Initiates Starting (e.g., Cartridge Starter, Etc.) Patents (Class 60/789)
  • Patent number: 10138812
    Abstract: A gas turbine engine sealing air system including a bearing chamber seal to prevent lubricant fluid loss from a fluid chamber, the sealing effected by ingress of sealing air. The system includes an air vent duct coupled to the bearing chamber seal. An ejector is located within the air vent duct to pump sealing air from the bearing chamber seal and through the air vent duct. A first duct is coupled between a starter air system of the gas turbine engine and the ejector to provide motive fluid to the ejector during gas turbine engine starting.
    Type: Grant
    Filed: November 23, 2012
    Date of Patent: November 27, 2018
    Assignee: ROLLS-ROYCE plc
    Inventors: Peter Ellison Heaton, Crispin David Bolgar
  • Patent number: 8402767
    Abstract: At least one solid mass of oxidizing-species-releasing material (ORM), selected as a solid oxidizer (SO), and/or as oxidizing-species-releasing burning substance (ORBS) is used as a device for enhancing the starting process of a turbine engine under various ambient conditions. The ORM is introduced into the combustion chamber of the turbine engine and the starting process of the turbine engine is initiated, by help of the igniter and in association with the ORM to enhance the starting process. In operation, an ORM selected as an SO releases gaseous oxygen when heated to decompose, while an ORM chosen as an ORBS discharges oxidizing species when ignited to burn. An ORM such as an SO or an ORBS may operate alone or in various combinations of both. The ORM is configured to release a predetermined mass flow rate of oxidizing species or of gaseous oxygen.
    Type: Grant
    Filed: May 29, 2009
    Date of Patent: March 26, 2013
    Assignee: Rafael-Advanced Defense Systems, Ltd.
    Inventors: Amichay H. Gross, Savely Khosid, Arie Peretz
  • Publication number: 20100043444
    Abstract: A method for implementing a system and a device for enhancing the starting process of a turbine engine by use of at least one solid mass of oxidizing-species-releasing material, ORM, selected as a solid oxidizer, or SO, and/or as an oxidizing-species-releasing burning substance, or ORBS. The ORM is introduced into the combustion chamber of the turbine engine and the starting process of the turbine engine is initiated, by help of the igniter and in association with the mass of ORM, to enhance the starting process. In operation, an ORM selected as an SO releases gaseous oxygen when heated to decompose, while an ORM chosen as an ORBS discharges oxidizing species when ignited to burn. An ORM such as an SO or an ORBS may operate alone or in various combinations of both. The ORM is configured to release a predetermined mass flow rate of oxidizing species or of gaseous oxygen.
    Type: Application
    Filed: May 29, 2009
    Publication date: February 25, 2010
    Applicant: RAFAEL ADVANCED DEFENSE SYSTEMS LTD.
    Inventors: Amichay H. Gross, Savely Khosid, Arie Peretz
  • Patent number: 6993915
    Abstract: An emergency power system comprising a plurality of solid propellant gas generators each having a gas outlet in fluid communication with a turbine wheel rotationally disposed within a gas turbine housing, the turbine wheel being in rotational communication with an electric generator input shaft, a fluid pump input shaft, or both. A method of producing power from such an emergency power system is also disclosed.
    Type: Grant
    Filed: February 26, 2004
    Date of Patent: February 7, 2006
    Assignee: Honeywell International Inc.
    Inventors: Ru-Li Kung, Scott J. Goldberg, Alex Morando, Tom Iles