Patents by Inventor Mark Loweth

Mark Loweth 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: 7146849
    Abstract: A leakage drain is used to provide an indication that leakage of a fluid has occurred within an engine. Previously, such leakage was detected by visual inspection of a retained drop at the outlet of a drain. With the present invention, a sensor arrangement comprising electrodes is located within or about the leakage drain whereby leakage fluid creates a film across those electrodes. Relative presence or absence or thickness of film causes variation in a detected electrical response (capacitance, reactance, resistance or impedance) and this variation is utilized in order to determine whether fluid leakage has occurred. Additionally, by time of flight analysis using electrostatic sensors it is possible to determine fluid flow rate. By analysis at different incident frequencies, a characteristic response for a particular type of leakage fluid is obtained. Thus, it is possible to deduce the type of leakage fluid as well as the rate of leakage.
    Type: Grant
    Filed: February 3, 2005
    Date of Patent: December 12, 2006
    Assignee: Rolls-Royce, PLC.
    Inventors: Ian C D Care, Mark Loweth
  • Publication number: 20050204802
    Abstract: A leakage drain (30) is used to provide an indication that leakage of a fluid has occurred within an engine. Previously such leakage was detected by visual inspection of a retained drop at the outlet of a drain. With the present invention a sensor arrangement comprising electrodes (33, 34; 133, 134) is located within or about the leakage drain (30) whereby leakage fluid creates a film across those electrodes. Relative presence or absence or thickness of film causes variation in a detected electrical response (capacitance, reactance, resistance or impedance) and this variation is utilised in order to determine whether fluid leakage has occurred. Additionally by time of flight analysis using electrostatic sensors (35, 36; 135, 136) it is possible to determine fluid flow rate. By analysis at different incident frequencies a characteristic response for a particular type of leakage fluid is obtained. Thus, it is possible to deduce the type of leakage fluid as well as the rate of leakage.
    Type: Application
    Filed: February 3, 2005
    Publication date: September 22, 2005
    Applicant: ROLLS-ROYCE PLC
    Inventors: Ian Care, Mark Loweth