Patents Assigned to Thermodyn
  • Patent number: 11248630
    Abstract: This liquid/gas separator for centrifugal motor compressor includes a sump internally equipped with at least one gas separator stage suitable to separate a gaseous phase from a liquid phase accepted in the sump entry. The sump internally includes a compartment in which the gaseous phase is separated by a separator stage, and in which is assembled by a compressor stage of the motor compressor.
    Type: Grant
    Filed: March 4, 2016
    Date of Patent: February 15, 2022
    Assignee: Thermodyn SAS
    Inventors: Thomas Alban, Yoann Vidalenc, Julien Renaud, Tiziano Pellegrini, Sebastien Condom
  • Patent number: 10774839
    Abstract: An impeller wheel assembly for a radial rotating machine, comprises a bladed hub portion of an impeller wheel, with a first radially outward facing, fluid deflecting surface having a curvature profile designed to deflect an axial fluid flow into a radial centrifugal flow, and comprising a deflector portion with a second radially outward facing, fluid deflecting surface. The second radially outward facing surface has a curvature profile designed to deflect a radial centripetal fluid flow into an axial fluid flow.
    Type: Grant
    Filed: December 18, 2013
    Date of Patent: September 15, 2020
    Assignee: THERMODYN SAS
    Inventors: Thomas Alban, Sylvain Guillemin, Manuele Bigi, Guiseppe Iurisci, Stefano Falomi
  • Patent number: 10718382
    Abstract: Embodiments of the present invention provide a magnetic bearing system comprising an axial bearing rotating flywheel arranged so as to magnetically interact with at least one fixed axial stop. The system includes a cooling fluid path configured so as to send the flow to the flywheel in a direction of flow being in a substantially radial plane relative to the axis of rotation of the flywheel.
    Type: Grant
    Filed: June 25, 2015
    Date of Patent: July 21, 2020
    Assignee: Thermodyn SAS
    Inventor: Denis Guillaume Guenard
  • Patent number: 10711792
    Abstract: An auxiliary turbomachinery shaft-support system including a first assembly configured to axially support the shaft, the first assembly including a rotating disc having a part shaped to be torsionally coupled to the shaft, and a stator including at least one pad including at least one elastic component coupled with the pads and urging it in the direction of a disc sliding surface.
    Type: Grant
    Filed: September 28, 2016
    Date of Patent: July 14, 2020
    Assignee: THERMODYN SAS
    Inventors: Yoann Vidalenc, Thomas Alban
  • Patent number: 10280938
    Abstract: A motorcompressor unit includes a first motor driving the rotation of a rotor and a compression stage including a bladed impeller mounted on a driven shaft, the rotation of which is driven by the rotor. Also, common casing is gastight with respect to fluid handled by the motorcompressor unit, where the compression stage and the first motor are mounted in the common casing. The compression stage also includes a regulating member that regulates the angle at which the fluid flows to or from the bladed impeller, and a second motor that controls the regulating member, the second motor being mounted in the common casing.
    Type: Grant
    Filed: December 29, 2011
    Date of Patent: May 7, 2019
    Assignee: THERMODYN
    Inventor: Gilles Nawrocki
  • Patent number: 9970461
    Abstract: A compressor unit is disclosed comprising at least a first motor driving in rotation at least one impeller of a compression stage, having at the outlet of the impeller a diffuser designed to centrifugally channel the gases coming from the impeller, and having a centripetal return channel downstream of the diffuser. The return channel includes at least one movable blade portion that, when moved, can vary a tangential component of the speed of the gases coming from the return channel.
    Type: Grant
    Filed: January 13, 2014
    Date of Patent: May 15, 2018
    Assignee: Thermodyn SAS
    Inventors: Gilles Nawrocki, Pascal Gaudez
  • Patent number: 9938983
    Abstract: A compressor for a motor-compressor set, comprising, on a rotating shaft, a balancing piston, a set of bladed wheels, a rear cavity of the piston adjacent to the balancing piston on a side opposite to the set of bladed wheels, a regulation valve suitable for coupling the rear cavity to the input of the set of bladed wheels, a suction pressure chamber coupled to the input of the set of bladed wheels, the rear cavity being arranged between the balancing piston and the suction pressure chamber. The compressor comprises a discharge pressure chamber arranged between the rear cavity of the piston and the suction pressure chamber, the discharge pressure chamber being coupled via a discharge line to a discharge area between the set of bladed wheels and the balancing piston.
    Type: Grant
    Filed: November 5, 2013
    Date of Patent: April 10, 2018
    Assignee: Thermodyn SAS
    Inventors: Benjamin Stalder, Thomas Alban
  • Patent number: 9689401
    Abstract: An impeller designed to be mounted on a rotary shaft includes: a basic rim provided with blades protruding on one surface of the basic rim, and a hub capable of being coupled to the basic rim and to the rotary shaft. In certain embodiments, the impeller includes an annular plate and the hub, where the annular plate and the basic rim are configured to interact together so as to hold the basic rim axially and to maintain a freedom of radial deformation of the basic rim relative to the hub and to the annular plate.
    Type: Grant
    Filed: February 21, 2013
    Date of Patent: June 27, 2017
    Assignee: Thermodyn
    Inventors: Sylvain Guillemin, Vittorio Michelassi, Douglas Carl Hofer
  • Patent number: 9644633
    Abstract: A centrifugal compressor unit includes a driving means for rotatably driving a rotor, and at least one compressor including a statoric body and an arrangement of blade wheels mounted on a shaft which is rotatably driven by the rotor in the statoric body. The group formed by the motor and/or each compressor being mounted in a common housing is sealed from the gas used by the compressor. The compressor unit also includes an arrangement of active bearings for axially and radially guiding the rotor and the driven shaft, and a means for cooling the driving means and the guiding bearings by withdrawing the gas used by the compressor at the outlet of a first compression stage. The cooling means includes a set of internal conduits for supplying the driving means and the bearings with cooling gas. The cooling gas flow in the motor and the cooling gas flow in the bearing is separated and then converge upstream of the first compression stage.
    Type: Grant
    Filed: April 11, 2003
    Date of Patent: May 9, 2017
    Assignee: Thermodyn
    Inventors: Pierre Laboube, Patrick Friez, Jean-Marc Pugnet, Patrice Bonnefoi
  • Patent number: 9631494
    Abstract: A rotor structure is provided. The rotor structure includes a plurality of wheels, a main axial tie rod passing through the plurality of wheels and a first shaft and a second shaft each attached to one extremity of the main tie rod, wherein the main tie rod and the bore of an end wheel in contact with one of the first and second shafts delimit a hydraulic chamber configured to receive a hydraulic fluid, and wherein the main tie rod, the hydraulic chamber and the end wheel form an internal hydraulic tension device configured to preload the main tie rod.
    Type: Grant
    Filed: June 15, 2012
    Date of Patent: April 25, 2017
    Assignee: Thermodyn
    Inventor: Denis Guenard
  • Patent number: 9447784
    Abstract: A diaphragm for the compression stage of a compressor includes least one set of through passages extending between two mutually opposite faces of the diaphragm, so as to create a flow of gas between the opposite faces depending on a pressure difference prevailing on either side of the diaphragm.
    Type: Grant
    Filed: April 11, 2013
    Date of Patent: September 20, 2016
    Assignee: Thermodyn
    Inventor: Gilles Nawrocki
  • Patent number: 9222481
    Abstract: A motor compressor unit (1) comprises a motor (3) and a compressor (2) which are mounted in a common housing (4) sealed against the gas to be compressed. The motor (3) comprises a rotor (39) rotatably connected to a rotor (38) of the compressor (2). The rotor (38) of the compressor comprises a main shaft (11) and a connecting shaft (21) coaxial with the main shaft, the connecting shaft being placed at least partly inside the main shaft (11) so as to be radially spaced from the main shaft (11) and comprising a coupling zone (15) for coupling with the main shaft (11).
    Type: Grant
    Filed: December 20, 2011
    Date of Patent: December 29, 2015
    Assignee: Thermodyn
    Inventor: Thomas Alban
  • Publication number: 20150354599
    Abstract: A compressor unit is disclosed comprising at least a first motor driving in rotation at least one impeller of a compression stage, having at the outlet of the impeller a diffuser designed to centrifugally channel the gases coming from the impeller, and having a centripetal return channel downstream of the diffuser. The return channel includes at least one movable blade portion that, when moved, can vary a tangential component of the speed of the gases coming from the return channel.
    Type: Application
    Filed: January 13, 2014
    Publication date: December 10, 2015
    Applicant: Thermodyn Sas
    Inventors: Gilles NAWROCKI, Pascal GAUDEZ
  • Patent number: 8899945
    Abstract: One aspect of the invention provides a centrifugal compressor unit (1) comprising a first motor (3), at least one compressor (2) comprising a drive shaft (9) driven by the rotor (12) of the first motor (3) and a set of impellers (5, 6, 7, 8) mounted on the drive shaft (9). The first motor (3) and the compressor (2) are mounted in a gas-tight common housing (26) operated by the compressor unit (1). The rotor (12) of the first motor (3) and the drive shaft (9) are connected by a flexible coupling (24) placed in the housing (26). The compressor unit includes a second motor (4) that is placed in the housing and of which the rotor (13) is connected to the drive shaft (9) by a second flexible coupling (25).
    Type: Grant
    Filed: October 24, 2011
    Date of Patent: December 2, 2014
    Assignee: Thermodyn
    Inventor: Pierre Laboube
  • Publication number: 20130216393
    Abstract: The invention provides an impeller designed to be mounted on a rotary shaft. The impeller comprises a basic rim provided with blades protruding on one surface of the basic rim, and a hub capable of being coupled to the basic rim and to the rotary shaft. In certain embodiments, the impeller comprises an annular plate and the hub, the plate and the basic rim are configured to interact together so as to hold the basic rim axially and to maintain a freedom of radial deformation of the basic rim relative to the hub and to the plate.
    Type: Application
    Filed: February 21, 2013
    Publication date: August 22, 2013
    Applicant: Thermodyn
    Inventor: Thermodyn
  • Publication number: 20120171056
    Abstract: This motorcompressor unit comprises at least one motor driving the rotation of a rotor and at least one compression stage comprising a set of bladed impellers mounted on a driven shaft the rotation of which is driven by the rotor, the assembly consisting of the motor and the or each compressor being mounted in a common casing that is gastight with respect to the gas handled by the compressor unit. At least one of the compression members comprises at least one aerodynamic member (13) for regulating the angle at which the gas handled by the said stage flows and a motor (16) for controlling the regulating member (13) mounted in the common casing.
    Type: Application
    Filed: December 29, 2011
    Publication date: July 5, 2012
    Applicant: THERMODYN
    Inventor: Gilles Nawrocki
  • Publication number: 20120164005
    Abstract: A motor compressor unit (1) comprises a motor (3) and a compressor (2) which are mounted in a common housing (4) sealed against the gas to be compressed. The motor (3) comprises a rotor (39) rotatably connected to a rotor (38) of the compressor (2). The rotor (38) of the compressor comprises a main shaft (11) and a connecting shaft (21) coaxial with the main shaft, the connecting shaft being placed at least partly inside the main shaft (11) so as to be radially spaced from the main shaft (11) and comprising a coupling zone (15) for coupling with the main shaft (11).
    Type: Application
    Filed: December 20, 2011
    Publication date: June 28, 2012
    Applicant: Thermodyn
    Inventor: Thomas Alban
  • Publication number: 20120100017
    Abstract: Centrifugal compressor unit (1) comprising a first motor (3), at least one compressor (2) comprising a drive shaft (9) driven by the rotor (12) of the first motor (3) and a set of impellers (5, 6, 7, 8) mounted on the drive shaft (9), the assembly consisting of the motor (3) and the compressor (2) being mounted in a gas-tight common housing (26) operated by the compressor unit (1), the rotor (12) of the first motor (3) and the drive shaft (9) being connected by a flexible coupling (24) placed in the housing (26). The compressor unit comprises a second motor (4) which is placed in the housing and of which the rotor (13) is connected to the drive shaft (9) by a second flexible coupling (25).
    Type: Application
    Filed: October 24, 2011
    Publication date: April 26, 2012
    Applicant: THERMODYN
    Inventor: Pierre La Boube
  • Patent number: 7144226
    Abstract: This compressor unit comprises a motor (34) and at least one compressor (44) comprising a driven shaft (54) driven by the rotor of the motor and bladed wheels fitted on the driven shaft (54), the assembly composed of the motor and the compressor being installed in a common casing (55) leak tight to the gas manipulated by the compressor unit. The rotor and the driven shaft are connected through a flexible coupling (72) placed in the casing.
    Type: Grant
    Filed: April 11, 2003
    Date of Patent: December 5, 2006
    Assignee: Thermodyn
    Inventors: Jean-Marc Pugnet, Patrick Friez, Pierre Laboube
  • Patent number: 6959929
    Abstract: A seal for a rotary compressor comprises a casing, at least one assembly having a rotating seal face ring which rotates as one with a sleeve intended to be mounted on a shaft of the compressor and of a stationary seal face ring mounted on the casing, the seal face rings being urged to press against one another via their rubbing face. The seal design further incorporates fluid circulation for heating leaks of compressible fluid conveyed by the compressor that occur between the seal face rings, this fluid circulation being formed in the casing and extending at least partially downstream of the seal face rings with respect to the direction of flow of the fluid stream.
    Type: Grant
    Filed: July 26, 2002
    Date of Patent: November 1, 2005
    Assignee: Thermodyn
    Inventors: Jean-Marc Pugnet, Daniel Bolusset, Patrick Friez