Patents by Inventor Philippe Alphonse Louis Ernens

Philippe Alphonse Louis Ernens 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: 9062549
    Abstract: Fluid-injected screw-type compressor element comprising two co-operating rotors (2 and 3) which are radially and axially bearing-mounted in a housing (1), whereby this housing confines a rotor chamber (4) in which the rotors (2 and 3) are situated and in which a fluid circuit (11) for the injection of a fluid discharges, characterized in that the radial bearing of at least one rotor is formed by the contact of the rotor concerned with the part of the wall of the housing opposite the radial perimeter of the rotor concerned and/or the co-operation with the other rotor and by maximally one additional radial bearing.
    Type: Grant
    Filed: May 15, 2009
    Date of Patent: June 23, 2015
    Assignee: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Raphael Henri Maria Pauwels, Philippe Alphonse Louis Ernens
  • Patent number: 8197227
    Abstract: An improved multi-stage compressor device for compressing gas, which compressor device (1) mainly consists of at least two compressor elements (2-5-28) placed in series one after the other, at least one of which (5-28) is driven by a motor (9), characterized in that at least one other compressor element (2) is driven separately, in other words without any mechanical link with said motor (9), by means of an expander (18) of a closed power cycle (12) with a circulating medium inside which is heated by the compressed gas.
    Type: Grant
    Filed: June 1, 2007
    Date of Patent: June 12, 2012
    Assignee: Atlas Copco Airpower, Naamloze Vennootschap
    Inventor: Philippe Alphonse Louis Ernens
  • Publication number: 20110014079
    Abstract: Fluid-injected screw-type compressor element comprising two co-operating rotors (2 and 3) which are radially and axially bearing-mounted in a housing (1), whereby this housing confines a rotor chamber (4) in which the rotors (2 and 3) are situated and in which a fluid circuit (11) for the injection of a fluid discharges, characterised in that the radial bearing of at least one rotor is formed by the contact of the rotor concerned with the part of the wall of the housing opposite the radial perimeter of the rotor concerned and/or the co-operation with the other rotor and by maximally one additional radial bearing.
    Type: Application
    Filed: May 15, 2009
    Publication date: January 20, 2011
    Inventors: Raphael Henri Maria Pauwels, Philippe Alphonse Louis Ernens
  • Publication number: 20090257902
    Abstract: An improved multi-stage compressor device for compressing gas, which compressor device (1) mainly consists of at least two compressor elements (2-5-28) placed in series one after the other, at least one of which (5-28) is driven by a motor (9), characterized in that at least one other compressor element (2) is driven separately, in other words without any mechanical link with said motor (9), by means of an expander (18) of a closed power cycle (12) with a circulating medium inside which is heated by the compressed gas.
    Type: Application
    Filed: June 1, 2007
    Publication date: October 15, 2009
    Inventor: Philippe Alphonse Louis Ernens