Patents Assigned to Atlas Copco Airpower, naamloze vennootschap
  • Publication number: 20180347567
    Abstract: A Method for controlling the liquid injection of a compressor device or expander device. This compressor device includes at least one compressor element or expander element, whereby the element comprises a housing that comprises a rotor chamber in which at least one rotor is rotatably affixed by means of bearings, whereby liquid is injected into the element. The method comprises the step of providing two independent separated liquid supplies to the element, whereby one liquid supply is injected into the rotor chamber and the other liquid supply is injected at the location of the bearings. The separated liquid supplies are realised by means of a modular channelling piece of an injection module.
    Type: Application
    Filed: September 12, 2016
    Publication date: December 6, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Sofie DEPREZ, Christian SCHMITZ, Johan Julia J. DOM, Aleksandr PULNIKOV, Benjamin MOENS
  • Patent number: 10145485
    Abstract: Compressor device that comprises a compressor element that is equipped with a compression chamber with at least one coolant inlet, and which furthermore comprises a gas outlet, a gas/coolant separation tank connected to it, and, a cooling circuit with a cooler that extends between the separation tank and the coolant inlet, and which is equipped with control means to adjust the temperature of the coolant flow supplied to the compressor element, whereby the aforementioned control means comprise a first and a second sub-controller, each with a different target parameter, whereby the control means also comprise switching means to place one of the two sub-controllers in an activated state and the other sub-controller in a deactivated state.
    Type: Grant
    Filed: February 22, 2013
    Date of Patent: December 4, 2018
    Assignee: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Kristof Adrien Laura Martens
  • Publication number: 20180311601
    Abstract: A device for separating liquid from a gas stream within a liquid injected vacuum pump or compressor, said device comprising: two communicating vessels having a common section extending over at least a part of the height; an inlet opening positioned on the opposite side of the common section; at least two bucket shaped vessels, each provided within one of the two communicating vessels; a lid comprising an outlet opening; wherein at least one of the two bucket shaped vessels forms a fluid passage between the wall of the communicating vessel and the wall of the bucket shaped vessel for allowing a fluid to pass there through.
    Type: Application
    Filed: April 13, 2016
    Publication date: November 1, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Niels GORREBEECK, Andries Jan F. DESIRON, Rudolf Jozef M. BEUCKELAERS, Tomasz MIRECKI, Ruben Pieter VYVEY, Johan Gustaaf K. AERTS, Willem EVERAERT
  • Publication number: 20180306189
    Abstract: An oil circuit for lubrication and cooling of an oil-free compressor with an oil reservoir and a rotary oil pump to drive oil to the compressor element and/or the motor via an oil pipe. The rotary oil pump has a rotor mounted on a rotation shaft, and is driven by the motor of the compressor. The oil circuit is provided with a bypass pipe and a pressure-actuated bypass valve which guide a portion of the oil back to the oil reservoir without this portion of the oil passing through the compressor element and/or the motor during its way back to the oil reservoir. The oil circuit is further provided with an oil cooler in the bypass pipe. The bypass valve is in the oil pipe.
    Type: Application
    Filed: April 20, 2018
    Publication date: October 25, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Thomas DE BONTRIDDER, Wim MEEUSEN, Edwin ROSKAM
  • Publication number: 20180298904
    Abstract: A compressor element of a screw compressor inlet side and an outlet side and two helical rotors, respectively a male rotor with a drive for the male rotor and a female rotor that is driven by the male rotor by means of synchronisation gearwheels with at least one synchronisation gearwheel on the male rotor, wherein the drive and synchronisation gearwheels of the male rotor are chosen such that, upon being driven with acceleration of the rotors without gas forces, the resulting mechanical drive force that is exerted by this drive and by this synchronisation gearwheel on the male rotor has an axial component that is directed from the outlet side to the inlet side and that the movement of the male rotor in the axial direction from the outlet side to the inlet side is fixed by means of a single axial single-acting or double-acting bearing.
    Type: Application
    Filed: April 12, 2016
    Publication date: October 18, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Simon Peter G. DE BOCK, Johan NACHTERGAELE, Dieter Manille L. BERTELS
  • Publication number: 20180283379
    Abstract: A method for controlling the speed of a compressor with a controller as a function of the available gas flow comprising the following steps: setting a desired value for the inlet pressure; determining the inlet pressure; determining the speed; controlling the speed of the compressor by reducing or increasing it depending on whether the inlet pressure is less than or greater than the set desired value until the inlet pressure is equal to the set desired value; providing the characteristic data of the compressor relating to the efficiency and/or the Specific Energy Requirement (SER) as a function of the speed and the inlet pressure; adjusting the desired value of the inlet pressure on the basis of the aforementioned characteristic data and in such a way that the efficiency of the compressor is a maximum or the SER is a minimum.
    Type: Application
    Filed: August 11, 2016
    Publication date: October 4, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Hans Theo MAGITS, Subodh Sharadchandra PATWARDHAN
  • Publication number: 20180283380
    Abstract: Device for controlling the oil temperature of an oil-injected compressor installation (1) with a compressor element (2) that is provided with a gas inlet (3) and an outlet (5) for compressed gas that is connected to an oil separator (8) that is connected by means of an injection pipe (12) to the aforementioned compressor element (2), and whereby a cooler (17) is affixed in a part (19) of the injection pipe (12) that can be bypassed by means of a bypass pipe (18), characterised in that the device (20) is provided with an extra pipe (21) that is intended to be connected in parallel with the bypass pipe (18) and the cooler (17), and in which an energy recovery system (22) can be connected, and that the device (20) is provided with flow distribution means (23) through the cooler (17), the bypass pipe (18) and the extra pipe (21), and a controller (28) for controlling these temperature (Tout) control means at the aforementioned outlet (5) of the compressor element (2).
    Type: Application
    Filed: February 3, 2016
    Publication date: October 4, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Kenneth DE VOCHT, Andries Jan F. DESIRON
  • Patent number: 10087944
    Abstract: A method for controlling a compressor that includes a compressor element, whereby during a transition from full load or partial load to zero load, a process A is followed that involves: (1) reducing the inlet pressure; and (2) reducing the speed and/or the drive torque. During a transition from zero load to part load or full load, a process B is followed that involves: (3) increasing of the speed or drive; and (4) increasing the inlet pressure.
    Type: Grant
    Filed: April 8, 2011
    Date of Patent: October 2, 2018
    Assignee: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Filip Gustaaf M. Huberland, Uwe Pahner, Filip Petrus I Beyens, Stijn Jozef Rita Johanna Janssens
  • Publication number: 20180274713
    Abstract: A housing for a compressor or expander installation, vacuum pump, generator or similar, whereby this housing is made of metal plates, wherein at least one of the aforementioned metal plates is provided with one or more reinforcing profiles, respectively longitudinal profiles that extend in a certain longitudinal direction and transverse profiles that extend along a transverse direction that forms an angle to the aforementioned longitudinal direction, whereby the various metal plates and longitudinal profiles and/or transverse profiles are joined together solely by means of mechanical fasteners.
    Type: Application
    Filed: January 5, 2016
    Publication date: September 27, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Ronny Antoine J. COOLS
  • Publication number: 20180274541
    Abstract: An oil-injected vacuum pump element, whereby two mating helical rotors are rotatably provided in a housing, whereby this housing comprises an inlet port and an outlet end face with an outlet port, whereby compression chambers are formed between the helical rotors and the housing, wherein the vacuum pump element is provided with a connection that extends from a first compression chamber to a second smaller compression chamber at the outlet end face, whereby this first compression chamber is at a lower pressure than the second compression chamber and whereby this second compression chamber can make connection with the outlet port upon rotation of the helical rotors, whereby the connection is such that a flow from the second compression chamber to the first compression chamber is possible, whereby the connection is not directly connected to the outlet port.
    Type: Application
    Filed: January 7, 2016
    Publication date: September 27, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Jens BOECKX, Jozef Maria SEGERS
  • Publication number: 20180266561
    Abstract: Method for installing a transmission between a drive with a driveshaft and a load with a driven shaft, whereby this transmission includes a housing and at least a drive gear and a driven gear, wherein the method consists of first affixing the transmission over the driveshaft and fastening the housing of the transmission to the housing of the drive and then affixing a shaft seal over the driveshaft.
    Type: Application
    Filed: September 27, 2016
    Publication date: September 20, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Stephan Willem VAN PRAET
  • Publication number: 20180266534
    Abstract: Transmission between a combustion engine with a crankshaft and a compressor element with driven shaft, whereby this transmission includes a housing and at least one driven gear and driveshaft with a drive gear, wherein the driveshaft of the transmission is connected to the crankshaft of the combustion engine by means of a rigid coupling, and the distance between the driveshaft and the driven shaft is greater than a sum of the radii of a plurality of pitch circles of the drive gear and the driven gear.
    Type: Application
    Filed: September 27, 2016
    Publication date: September 20, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Ivo DANIELS, Stephan Willem VAN PRAET
  • Publication number: 20180266421
    Abstract: An inlet valve for regulating the pressure at the inlet channel of a vacuum pump comprising: a first chamber defined by a housing having at least one inlet channel connected to a first supply of a fluid, comprising a movable element defining two cavities fluidly sealed from each-other and means for exerting a force on the movable element; a second chamber separated from the first chamber by a wall and defined by a housing, being in direct communication with a process channel of a second supply of a fluid; a valve body slidably mounted in the wall to prevent a fluid flow between the second chamber and the second cavity of the first chamber, the valve body having a distal end and a proximal end, wherein the valve body comprises a fluid channel extending through the valve body allowing a fluid flow between the first cavity and the inlet channel.
    Type: Application
    Filed: January 7, 2016
    Publication date: September 20, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Joeri COECKELBERGS, Niels GORREBEECK, Dries GIELIS, Andries DE BOCK, Glenn VINCK, Andries DESIRON
  • Publication number: 20180258952
    Abstract: A compressor module for compressing gas composed of a compressor element with a housing with integrated compressor element cooler; a motor and a gas cooler for cooling the compressed gas originating from the compressor element. The gas cooler includes a primary section through which the gas to be cooled can be guided and a secondary section that is in heat-exchanging contact with the primary section. A first cooling circuit can guide a coolant through the secondary section of the gas cooler or through a section thereof and a second cooling circuit can guide a coolant through the compressor element cooler. The first cooling circuit and the second cooling circuit are joined together in series or in parallel and are guided to a common output.
    Type: Application
    Filed: February 28, 2018
    Publication date: September 13, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: WIM MEEUSEN, THOMAS DE BONTRIDDER
  • Publication number: 20180252120
    Abstract: An Organic Rankine Cycle (ORC) device and method for transforming heat from a heat source into mechanical energy. The ORC includes a closed circuit containing a two phase working fluid. The circuit comprises a liquid pump for circulating the working fluid consecutively through an evaporator which is configured to be placed in thermal contact with the heat source; through an expander for transforming the thermal energy of the working fluid into mechanical energy; and through a condenser which is in thermal contact with a cooling element. The expander is situated above the evaporator. The fluid outlet of the evaporator is connected to the fluid inlet of the expander by a raiser column which is filled with a mixture of liquid working fluid and of gaseous bubbles of the working fluid, which mixture is supplied to the expander.
    Type: Application
    Filed: August 18, 2016
    Publication date: September 6, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Henrik OHMAN
  • Publication number: 20180243686
    Abstract: An adsorption device for compressed gas, is provided with a vessel with an inlet for the supply of a compressed gas to be treated, and an outlet for treated gas and an adsorption element is affixed in the vessel. The adsorption element extends along the flow direction of the compressed gas to be treated, between the inlet and the outlet. The adsorption element has a monolithic supporting structure that is at least partially provided with a coating that contains an adsorbent.
    Type: Application
    Filed: June 14, 2016
    Publication date: August 30, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventors: Carlo Lambert J. Lammers, Hans Hermans, Geert Van Rompaey
  • Publication number: 20180245788
    Abstract: An Organic Rankine Cycle (ORC) device and method for transforming waste heat from a heat source containing compressed gas into mechanical energy. The ORC includes a closed circuit containing a two-phase working fluid, the circuit including a liquid pump for circulating the working fluid in the circuit consecutively through an evaporator which is in thermal contact with the heat source; through an expander like a turbine for transforming the thermal energy of the working fluid into mechanical energy; and through a condenser which is in thermal contact with a cooling element. The ORC determines the mechanical energy generated by the expander. A control device regulates the fraction of the working fluid entering the expander based on the determined mechanical energy such that the mechanical energy generated by the expander is maximum.
    Type: Application
    Filed: August 18, 2016
    Publication date: August 30, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Henrik OHMAN
  • Publication number: 20180245599
    Abstract: A compressor device comprising a compressor element with a housing with, an inlet and an outlet. At least one rotor is affixed in the housing that is provided with a drive. The compressor device is provided with an oil circuit for injecting oil into the housing. The oil circuit only comprises one pump for driving the oil around in the oil circuit. This pump is coupled to a first shaft via a first disengageable coupling, more specifically a shaft of the aforementioned drive on the one hand, and to a second shaft via a second disengageable coupling, more specifically a shaft of a secondary drive on the other hand. The first and second disengageable couplings between the pump and the first shaft and between the pump and the second shaft are such that the pump is only driven by the shaft of these two shafts that has the highest speed.
    Type: Application
    Filed: February 1, 2016
    Publication date: August 30, 2018
    Applicant: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Kurt PEETERS
  • Patent number: 10060663
    Abstract: A cooling circuit is equipped with a coolant, a compressor, a condenser and evaporator expansion valve combinations, whereby the outlets of the evaporators are connected to a collection pipe connected to the compressor. The cooling circuit comprises a control unit connected to a temperature sensor and a pressure sensor affixed in the collection pipe and connected to the expansion valves for the control of them. The control unit is provided with an algorithm for controlling the expansion valves on the basis of the temperature sensor and pressure sensor to control the superheating in the collection pipe.
    Type: Grant
    Filed: December 18, 2017
    Date of Patent: August 28, 2018
    Assignee: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Frits Cornelis A. Baltus
  • Patent number: D826242
    Type: Grant
    Filed: May 26, 2017
    Date of Patent: August 21, 2018
    Assignee: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
    Inventor: Roel Adriaensen