Patents by Inventor Tuyen Trong Hoang

Tuyen Trong Hoang 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: 9200572
    Abstract: Methods and devices for anticipating a surge in a gas turbine engine. Controlled pressure signal(s) may be compared with reference pressure signal(s), each of the controlled pressure signal(s) and reference pressure signal(s) having an associated time value. If the controlled pressure signal(s) are less than the reference pressure signal(s), a controlled pressure curve may be fitted through a predetermined number of points based on the controlled pressure value(s) and associated time value(s). A reference pressure curve may be fitted through the predetermined number of points based on the reference pressure value(s) and associated time value(s). A time to compressor surge may be estimated based on an intersection of the controlled pressure curve and the reference pressure curve.
    Type: Grant
    Filed: September 13, 2012
    Date of Patent: December 1, 2015
    Assignee: PRATT & WHITNEY CANADA CORP.
    Inventor: Tuyen Trong Hoang
  • Publication number: 20140069105
    Abstract: Methods and devices for anticipating a surge in a gas turbine engine. Controlled pressure signal(s) may be compared with reference pressure signal(s), each of the controlled pressure signal(s) and reference pressure signal(s) having an associated time value. If the controlled pressure signal(s) are less than the reference pressure signal(s), a controlled pressure curve may be fitted through a predetermined number of points based on the controlled pressure value(s) and associated time value(s). A reference pressure curve may be fitted through the predetermined number of points based on the reference pressure value(s) and associated time value(s). A time to compressor surge may be estimated based on an intersection of the controlled pressure curve and the reference pressure curve.
    Type: Application
    Filed: September 13, 2012
    Publication date: March 13, 2014
    Applicant: PRATT & WHITNEY CANADA CORP.
    Inventor: Tuyen Trong HOANG
  • Patent number: 8312969
    Abstract: A lubrication system for an aircraft engine includes a lubrication fluid tank and a fluid passage communicating with the tank to define an entry of the passage inside the tank. The entry is positioned in a location submerged in the lubrication fluid for delivery of the lubrication fluid under a pressure differential, from the tank to the lubrication system regardless of the tank or aircraft attitude.
    Type: Grant
    Filed: June 29, 2010
    Date of Patent: November 20, 2012
    Assignee: Pratt & Whitney Canada Corp.
    Inventor: Tuyen Trong Hoang
  • Publication number: 20110315484
    Abstract: A lubrication system for an aircraft engine includes a lubrication fluid tank and a fluid passage communicating with the tank to define an entry of the passage inside the tank. The entry is positioned in a location submerged in the lubrication fluid for delivery of the lubrication fluid under a pressure differential, from the tank to the lubrication system regardless of the tank or aircraft attitude.
    Type: Application
    Filed: June 29, 2010
    Publication date: December 29, 2011
    Applicant: PRATT & WHITNEY CANADA CORP.
    Inventor: Tuyen Trong HOANG
  • Patent number: 7530430
    Abstract: A gravity controlled lubrication system for aircraft engines to supply a lubricant from a tank to a circulating system permitting lubricant to flow when the aircraft changes to an inverted flight condition.
    Type: Grant
    Filed: November 4, 2004
    Date of Patent: May 12, 2009
    Assignee: Pratt & Whitney Canada Corp.
    Inventors: Tuyen Trong Hoang, Constantin Catanu, Daniel Grigore