Patents by Inventor Stan Wood

Stan Wood 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: 7574894
    Abstract: A gas measuring method, apparatus and system for measuring a concentration of a gas of interest is disclosed. The gas concentration is based on a propagation delay of a sonic or ultrasonic wave as the wave travels through the gas. The propagation delay is measured such that delay contributions from sources other than the gas itself are canceled. A sensor in accordance with the invention includes an sonic or ultrasonic transmitter and receiver, and a control module for performing calculations. The sensor can be used in various applications, including on-board inert gas generating systems (OBIGGS).
    Type: Grant
    Filed: April 25, 2006
    Date of Patent: August 18, 2009
    Assignee: Parker-Hannifin Corporation
    Inventors: Howard Austerlitz, Lenard Hirshman, Ronald Bueter, Stan Wood
  • Publication number: 20070245802
    Abstract: A gas measuring method, apparatus and system for measuring a concentration of a gas of interest is disclosed. The gas concentration is based on a propagation delay of a sonic or ultrasonic wave as the wave travels through the gas. The propagation delay is measured such that delay contributions from sources other than the gas itself are canceled. A sensor in accordance with the invention includes an sonic or ultrasonic transmitter and receiver, and a control module for performing calculations. The sensor can be used in various applications, including on-board inert gas generating systems (OBIGGS).
    Type: Application
    Filed: April 25, 2006
    Publication date: October 25, 2007
    Inventors: Howard Austerlitz, Lenard Hirshman, Ronald Bueter, Stan Wood
  • Patent number: 6915987
    Abstract: The invention relates to a method of providing a seal between an aircraft structure (14) and a removable panel (26) mountable on the structure to close an opening (12) therein. According to the invention, the method comprises applying a sealant compound (28) for example a polysulphide rubber compound, to one of the structure and the panel, forming a rebate (46) in the sealant compound, and providing a sealant tape (48) to fit within the rebate. Subsequently, the panel is fastened to the structure with the seal (50) comprising the sealant compound and the sealant tape being sandwiched between the structure and the panel and encircling the opening.
    Type: Grant
    Filed: September 11, 2002
    Date of Patent: July 12, 2005
    Assignee: BAE Systems plc.
    Inventors: David Fisher, Raja S. Abbas, John S. Robbens, Stan Wood
  • Publication number: 20030015278
    Abstract: The invention relates to a method of providing a seal between an aircraft structure (14) and a removable panel (26) mountable on the structure to close an opening (12) therein. According to the invention, the method comprises applying a sealant compound (28) for example a polysulphide rubber compound, to one of the structure and the panel, forming a rebate (46) in the sealant compound, and providing a sealant tape (48) to fit within the rebate. Subsequently, the panel is fastened to the structure with the seal (50) comprising the sealant compound and the sealant tape being sandwiched between the structure and the panel and encircling the opening.
    Type: Application
    Filed: September 11, 2002
    Publication date: January 23, 2003
    Applicant: BAE Systems plc
    Inventors: David Fisher, Raja S. Abbas, John S. Robbens, Stan Wood
  • Patent number: 6461458
    Abstract: The invention relates to a method of providing a seal between an aircraft structure (14) and a removable panel (26) mountable on the structure to close an opening (12) therein. According to the invention, the method comprises applying a sealant compound (28) for example a polysulphide rubber compound, to one of the structure and the panel, forming a rebate (46) in the sealant compound, and providing a sealant tape (48) to fit within the rebate. Subsequently, the panel is fastened to the structure with the seal (50) comprising the sealant compound and the sealant tape being sandwiched between the structure and the panel and encircling the opening.
    Type: Grant
    Filed: June 2, 2000
    Date of Patent: October 8, 2002
    Assignee: BAE Systems plc
    Inventors: David Fisher, Raja S. Abbas, John S. Robbens, Stan Wood