Patents by Inventor Mark Rudkin

Mark Rudkin 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: 10533899
    Abstract: The present invention provides a thermocouple probe (10). The probe includes a first pair of thermocouple wires (50) joined to form a first thermocouple junction (56) at a sensing tip (14) of the thermocouple probe and a cooling arrangement (20) defining a cooling pathway (34) adjacent to a cooled portion of the probe. The sensing tip projects beyond the cooling arrangement and is cooled during use by conduction to the cooled portion of the probe. The probe further includes a second pair of thermocouple wires (54) joined to form a second thermocouple junction (52) in the cooled portion of the probe and adjacent to the sensing tip. The present invention also provides a method and a system for determining the gas temperature (Tg) in a high temperature environment, such as a jet engine.
    Type: Grant
    Filed: July 26, 2016
    Date of Patent: January 14, 2020
    Assignee: WESTON AEROSPACE LIMITED
    Inventor: Mark Rudkin
  • Publication number: 20170030779
    Abstract: The present invention provides a thermocouple probe (10). The probe includes a first pair of thermocouple wires (50) joined to form a first thermocouple junction (56) at a sensing tip (14) of the thermocouple probe and a cooling arrangement (20) defining a cooling pathway (34) adjacent to a cooled portion of the probe. The sensing tip projects beyond the cooling arrangement and is cooled during use by conduction to the cooled portion of the probe. The probe further includes a second pair of thermocouple wires (54) joined to form a second thermocouple junction (52) in the cooled portion of the probe and adjacent to the sensing tip. The present invention also provides a method and a system for determining the gas temperature (Tg) in a high temperature environment, such as a jet engine.
    Type: Application
    Filed: July 26, 2016
    Publication date: February 2, 2017
    Inventor: Mark Rudkin
  • Patent number: 8947071
    Abstract: A system and method for measuring frequency which reduces the impact of noise. The system and method includes the steps of sampling a signal train over a first signal portion of the signal train, determining a first average period for the first signal portion (t1) of the signal train, sampling the signal train over a second signal portion (t2) of the signal train, wherein, the second portion of the signal train overlaps with the first signal portion, determining a second average period for the second signal portion (t2) of the output signal train, and then determining the average of the determined average periods.
    Type: Grant
    Filed: March 2, 2012
    Date of Patent: February 3, 2015
    Assignee: Weston Aerospace Limited
    Inventors: Mark Rudkin, Anthony Palmer
  • Publication number: 20130063127
    Abstract: A system and method for measuring frequency which reduces the impact of noise. The system and method includes the steps of sampling a signal train (2) over a first signal portion (t1) of the signal train, determining a first average period for the first signal portion (t1) of the signal train, sampling the signal train over a second signal portion (t2) of the signal train, wherein, the second portion of the signal train overlaps with the first signal portion, determining a second average period for the second signal portion (t2) of the output signal train, and then determining the average of the determined average periods.
    Type: Application
    Filed: March 2, 2012
    Publication date: March 14, 2013
    Applicant: WESTON AEROSPACE LIMITED
    Inventors: Mark Rudkin, Anthony Palmer
  • Publication number: 20110252884
    Abstract: The invention provides a vibrating cylinder transducer for measuring the pressure or density of a fluid medium comprising: a cylindrical vibrator, in use having at least one surface coupled to a fluid medium to be measured; a drive means for vibrating the cylindrical vibrator; a sensor for detecting the resonant frequency of the cylindrical vibrator; and an output coupled to the sensor, the output configured to provide an output signal indicative of the pressure and/or the density of the fluid medium; wherein the surface coupled to the fluid medium is coated in a corrosion resistant polymer layer. Preferably the corrosion resistant polymer layer is formed from parylene.
    Type: Application
    Filed: April 14, 2011
    Publication date: October 20, 2011
    Applicant: WESTON AEROSPACE LIMITED
    Inventors: Paul Hanscombe, Mark Rudkin
  • Publication number: 20050268721
    Abstract: A pressure measuring device (2) comprises a vibrating ferromagnetic cylinder (4) and mechanically located within a casing (6). A diaphragm (24) is directly connected to the cylinder and forms a pressure measurement surface. Pressure on the diaphragm (24) results in a force and stresses in the cylinder (4) which change the resonant frequency of the vibrating cylinder.
    Type: Application
    Filed: May 19, 2005
    Publication date: December 8, 2005
    Applicant: Weston Aerospace Limited
    Inventor: Mark Rudkin