EP2613999B1 - Antrieb - Google Patents

Antrieb Download PDF

Info

Publication number
EP2613999B1
EP2613999B1 EP11758389.8A EP11758389A EP2613999B1 EP 2613999 B1 EP2613999 B1 EP 2613999B1 EP 11758389 A EP11758389 A EP 11758389A EP 2613999 B1 EP2613999 B1 EP 2613999B1
Authority
EP
European Patent Office
Prior art keywords
rotary element
drive
radius
outflow
rotary
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP11758389.8A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2613999A1 (de
Inventor
Siegfried Lais
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Reintrieb GmbH
Original Assignee
Reintrieb GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Reintrieb GmbH filed Critical Reintrieb GmbH
Priority to SI201131751T priority Critical patent/SI2613999T1/sl
Priority to PL11758389T priority patent/PL2613999T4/pl
Publication of EP2613999A1 publication Critical patent/EP2613999A1/de
Application granted granted Critical
Publication of EP2613999B1 publication Critical patent/EP2613999B1/de
Priority to HRP20191184TT priority patent/HRP20191184T1/hr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08—Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller

Definitions

  • the object of the invention is to propose a drive that allows reducing the draft and in which the propulsion is increased.
  • the drive according to the invention basically two possible uses are conceivable.
  • the use as a force-transmitting device is conceivable in which energy is transmitted by the energy device to the rotary machines and thereby a movement of the water vehicle is initiated.
  • the use as a regenerative device is conceivable in which energy is transferred from a flow to the centrifugal machines and the energy device acts as a generator.
  • the centrifugal machines are turbines.
  • the first rotary machine and / or the second rotary machine comprises axially, semi-axially or radially arranged blades. hereby In each case, different discharge directions can be set without the gyroscope having to be turned on with respect to a direction of movement.
  • the blades of the first rotary machine and the blades of the second rotary machine have the same or different lengths. In this case, it is possible that the first rotary machine and the second rotary machine are the same size. Moreover, it is conceivable that the first rotary machine is larger than the second rotary machine and vice versa.
  • a gyroscope has blades of different sizes.
  • the pusher in one embodiment it is conceivable for the pusher to form a transverse jet installation in which at least one first rotary machine and / or at least one second rotary machine is provided.
  • centrifugal machines can deviate from each other in the employment of the blades with respect to the axial flow.
  • one of the at least one first rotary machine has a first radius which is the maximum radial extent of the first rotary machine with respect to its axis of rotation
  • one of the at least one second gyroscope has a second radius comprising the maximum radial extent of the second gyroscope with respect to its axis of rotation
  • the close spacing of the first gyroscope and the second gyroscope is less than or equal to each other by 2 x first radius + second radius) or (first radius + 2 x second radius), preferably (3/2 x first radius + second radius) or (first radius + 3/2 x second radius), preferably (5/4 x first radius + second radius) or (first radius + 5/4 x second radius), definable or defined.
  • the first and second axes of rotation have at least a distance of about 10 mm to 20 mm.
  • the tips of the blades of the rotary machines it is possible for the tips of the blades of the rotary machines to have a maximum distance from a radius length of the blades of the first rotary machine or of the second rotary machine relative to one another.
  • at least one of the at least one first rotary machine and at least one of the at least one second rotary machine are arranged at least partially intermeshing.
  • the first rotary machine and the second rotary machine may overlap 10% to 40% with respect to the first radius of the first rotary machine or the second radius of the second rotary machine.
  • the first drive can be made particularly compact.
  • angles ⁇ 1 and / or ⁇ 1 of the first gyroscope and / or the angles ⁇ 2 and / or ⁇ 2 of the second gyroscope are adjustable during operation of the first drive.
  • the first drive can be individually adapted by a user.
  • the transmission is preferably arranged such that it drives the first rotary machine and / or the second rotary machine at the axial height. As a result, it is upstream of the two centrifugal machines in the flow direction and, like the centrifugal machines, also arranged in the fluid.
  • two or more second rotary machines are assigned to a first rotary machine or that two or more first rotary machines are assigned to a second rotary machine.
  • the first rotary machine has a larger radius than the two second rotary machines.
  • an optimal size difference is achieved by the.
  • the First rotary machine generated propulsion corresponds to the propulsion, which is generated by the two centrifugal machines.
  • first rotary machine and the second rotary machine have a common suction surface.
  • first rotary machine and the second rotary machine have suction surfaces which are separable from one another. This ensures that the respective axial flow of the individual rotor machine is substantially free of twist.
  • the first rotary machine and the second rotary machine each have a radiating surface.
  • the invention provides that the first rotary machine and the second rotary machine have a common radiating surface.
  • the pusher may be formed only by the first gyroscope and / or the second gyroscope. Further, the pusher may have a nozzle or jacket.
  • the invention provides that the exhaust nozzle before the first rotary machine and / or the second rotary machine has an inlet.
  • the inlet can be configured in such a way that the first rotary machine and the second rotary machine are flowed together via the inlet or else can be flowed on separately through the inlet.
  • the nozzle may be arranged in the drive according to the invention such that it surrounds the first rotary machine and the second rotary machine or be arranged downstream of the rotary machines. In the latter case, the rotary machines are freely running in the radial direction with respect to the environment.
  • the process is characterized by the step: Diverting the swirl components of the swirling first outflow by colliding with the swirl-related second outflow by designing the drive according to the invention.
  • the pusher can build smaller, whereby it is achieved that the draft of the ship is reduced. As a result, waters with low water depth are passable.
  • the drive can be designed to save space, since an energy device can be assigned to several centrifugal machines.
  • the figures show an overall drive provided with the reference numeral 2, in particular for a watercraft, which has an energy device 4 and a vortriebin pusher 6.
  • the energy device can be designed in particular as an internal combustion engine or electric machine. If the energy device 4 is an electric machine, it can be driven by both a motor and a generator.
  • the thrust generating device 6, as shown in the figures, has a first rotary machine 8 and a second rotary machine 10. Both the first centrifugal machine 8 and the second rotary machine 10 are essentially flowed through by an axial flow. During operation of the drive 2, the axial flow is then respectively subjected to swirl during passage through the rotary machine 8 or the rotary machine 10 and deflected into a first outflow direction or second outflow direction. In the case of the first centrifugal machine 8, the axial flow is deflected as a first outflow into a first outflow direction 12, in the case of the second rotary machine 10 as a second outflow in a second outflow direction 14. In the case of the drives 2 shown in the figures, in each case one energy device 4 is assigned a first rotary machine 8 and a second rotary machine 10.
  • FIG. 1 shows a schematic arrangement of the first gyroscope 8 and the second gyro 10. These have with respect to a direction of movement 16, viewed in a horizontal plane, an angle ⁇ 1 and an angle ⁇ 2 on. The angles ⁇ 1 and ⁇ 2 are adjustable during operation of the drive 2.
  • the centrifugal machines 8, 10 are equipped with blades 18 which are the same in the first rotary machine 8 and the second rotary machine 10. In principle, however, it is also conceivable that the blade 18 of the first rotary machine 8 differ from the blades 18 of the second rotary machine 10 in length, contour, arrangement and employment.
  • the first rotary machine 8 and the second rotary machine 10 a close distance from each other, with respect to their axes of rotation, on. This distance is defined below over the radii of the rotary machines 8, 10:
  • the first rotary machine 8 has a first radius, which includes the maximum radial extent of the first rotary machine 8 with respect to its axis of rotation.
  • the second gyroscope 10 has a second radius, which includes the maximum radial extent of the second gyroscope 10 with respect to its axis of rotation.
  • FIG. 2 shows a second embodiment of the drive 2 according to the invention, in which the first rotary machine 8 and the second rotary machine 10 are arranged partially interlocking or overlapping each other.
  • the two rotary machines 10, 8 with a synchronization device 20 (in FIG. 2 not shown) connected such that the rotational movement of the first gyroscope 8 is synchronized with the rotational movement of the second gyroscope 10 such that the blades 18 of the first gyroscope engage in gaps of the second gyroscope 10 and vice versa.
  • damage to the drive 2 is prevented by unsynchronized movement of the rotary machines 8, 10.
  • FIG. 3 shows a schematic side view of the drive 2.
  • the energy device 4 is provided in a watercraft 22.
  • the energy device 4 is connected by means of a first shaft 24 with a gear 26, in particular transfer case.
  • the gear 26 Via the gear 26, the drive energy provided by the energy device 4 is transmitted by means of two second shafts 28 to the first rotary machine 8 and to the second rotary machine 10, respectively.
  • the gear 26 in this case implements the synchronization device 20.
  • the first rotary machine 8 is arranged parallel to the water surface.
  • the angle ⁇ 1 in a considered vertical plane, the angle between the water surface and the first gyroscope spans, is 0 ° in such case.
  • FIG. 4 shows a plan view of the schematic representation according to FIG. 3 ,
  • the gearbox 26 is designed in such a way that the energy provided by the energy device 4 is transmitted to the first rotary machine 8 and to the second rotary machine 10 in such a way that both rotary machines 8, 10 rotate in opposite directions with respect to each other.
  • FIG. 5 also shows a plan view of a schematic arrangement of the embodiment according to FIG. 3 in which the first rotary machine 8 is inclined with respect to the direction of movement 16 at an angle ⁇ 1 and the second rotary machine 10 at an angle ⁇ 2 with respect to the direction of movement 16 with respect to each other.
  • An optimum angle by varying the angles ⁇ 1 and ⁇ 2, depending on the power which is to project beyond the centrifugal machine 8, 10, be adjusted in order to recover maximum propulsion from the swirling outflow.
  • FIG. 7 shows an embodiment of the drive 2 according to the invention, in which the pusher in addition to the previous, not belonging to the invention examples, a nozzle 32 has.
  • suction surfaces 34 of the nozzle 32 are separated from each other by means of a wall 36 from each other.
  • FIG. 8 An alternative design of the nozzle 32 of the drive of the pusher 6 of the drive 2 shows FIG. 8 in which the first rotary machine 8 and the second rotary machine 10 have a common suction surface 34.
  • FIGS. 9 and 10 show different types of casing or nozzle 32 of the thruster 6 of the drive 2.
  • the nozzle 32 may have an essentially oval shape.
  • the nozzle 32 may also have an 8-shaped cross-section.
  • FIGS. 11 and 12 show an embodiment of the drive 2, in which the first rotary machine 8 and the second rotary machine 10 transverse to the direction of movement 16 of a watercraft 22 work.
  • the first rotary machine 8 and the second rotary machine 10 jointly convey fluid into a pressure chamber 38 which is enclosed.
  • the medium conveyed into the pressure chamber is emitted via a jacket or nozzle 32.
  • the drive 2 according to the invention is designed as a water jet drive.
  • FIG. 13 shows a perspective sectional view of the drive 2 with a first centrifugal machine 8 and a second centrifugal machine 10, downstream of which a nozzle 32 is connected downstream.
  • First rotary machine 8 and second rotary machine 10 are arranged in parallel at the same axial height and spaced from each other.
  • the nozzle 32 surrounds the first rotary machine 8 and the second rotary machine 10 and tapers in the direction of the outflow.
  • FIG. 14 shows a perspective view of the drive 2, which forms a transverse jet drive.
  • a first rotary machine 8 and a second rotary machine 10 are arranged transversely to the direction of travel of the watercraft.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Hydraulic Turbines (AREA)
  • Surgical Instruments (AREA)
  • Valve Device For Special Equipments (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
EP11758389.8A 2010-09-06 2011-09-06 Antrieb Active EP2613999B1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
SI201131751T SI2613999T1 (sl) 2010-09-06 2011-09-06 Pogon
PL11758389T PL2613999T4 (pl) 2010-09-06 2011-09-06 Napęd
HRP20191184TT HRP20191184T1 (hr) 2010-09-06 2019-07-01 Pogon

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010044435A DE102010044435A1 (de) 2010-09-06 2010-09-06 Antrieb
PCT/EP2011/004478 WO2012031740A1 (de) 2010-09-06 2011-09-06 Antrieb

Publications (2)

Publication Number Publication Date
EP2613999A1 EP2613999A1 (de) 2013-07-17
EP2613999B1 true EP2613999B1 (de) 2019-04-03

Family

ID=44658691

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11758389.8A Active EP2613999B1 (de) 2010-09-06 2011-09-06 Antrieb

Country Status (11)

Country Link
EP (1) EP2613999B1 (hu)
DE (1) DE102010044435A1 (hu)
DK (1) DK2613999T3 (hu)
ES (1) ES2743312T3 (hu)
HR (1) HRP20191184T1 (hu)
HU (1) HUE044175T2 (hu)
LT (1) LT2613999T (hu)
PL (1) PL2613999T4 (hu)
PT (1) PT2613999T (hu)
SI (1) SI2613999T1 (hu)
WO (1) WO2012031740A1 (hu)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105197216A (zh) * 2015-10-30 2015-12-30 佛山市神风航空科技有限公司 一种斜桨船
CN105173045A (zh) * 2015-10-30 2015-12-23 佛山市神风航空科技有限公司 一种双桨方管船舶推进装置
CN105270589B (zh) * 2015-10-30 2018-05-01 佛山市神风航空科技有限公司 一种船舶用双级推进器
CN105197181A (zh) * 2015-10-30 2015-12-30 佛山市神风航空科技有限公司 一种双体斜桨船
CN105197215B (zh) * 2015-10-30 2018-08-03 佛山市神风航空科技有限公司 一种双推电动船
CN105197219A (zh) * 2015-10-30 2015-12-30 佛山市神风航空科技有限公司 一种双桨方管船舶推进器
CN105270588A (zh) * 2015-10-30 2016-01-27 佛山市神风航空科技有限公司 一种船舶用对称型双级推进装置
CN105217002B (zh) * 2015-10-30 2018-12-04 孙永锋 一种气动小型船
CN105584586A (zh) * 2016-03-08 2016-05-18 上海船舶研究设计院 一种小型lng运输船双全回转拉式桨推进的尾部结构
DE102018102289A1 (de) * 2018-02-01 2019-08-01 Ellergon Antriebstechnik Gesellschaft M.B.H. Hydrofoil

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2407799A1 (de) * 1974-02-19 1975-08-28 Berndt Martens Querstrahl-steueranlage fuer wasserfahrzeuge
DE3937327A1 (de) * 1988-11-14 1990-05-17 Kawasaki Heavy Ind Ltd Schiffsantriebseinrichtung
DE4206720A1 (de) * 1991-03-11 1992-09-17 Kawasaki Heavy Ind Ltd Schiffsantriebseinrichtung
EP1892183A1 (en) * 2005-03-11 2008-02-27 Kabushiki Kaisha Kawasaki Zosen Stern structure of ship

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1270603A (en) * 1917-06-23 1918-06-25 Robert William Davis Propulsion of vessels.
DE490526C (de) * 1926-01-06 1930-01-30 Christian Andresen Dipl Ing Luft- und Wasserschraubenanordnung mit vor, hinter oder um die Schraube fest oder umlaufend angeordnetem Ringmantel
US1864857A (en) * 1931-08-28 1932-06-28 Ranke Gisbert Boat propelling device
US2162058A (en) * 1936-01-23 1939-06-13 Alanson P Brush Boat
US3416480A (en) * 1967-01-31 1968-12-17 Navy Usa Ship's stern and propeller arrangement
JPS4737316B1 (hu) * 1968-10-26 1972-09-20
GB1197850A (en) * 1968-12-03 1970-07-08 Satterthwaite James G Peripheral Journal Propeller Drive
US3662702A (en) * 1970-06-16 1972-05-16 David John Doust Multiple propeller ducted system
US3745963A (en) * 1970-08-14 1973-07-17 W Fisher Boat structure
DD96911A1 (hu) * 1972-05-23 1973-04-12
DE2356508A1 (de) * 1973-11-13 1975-05-15 Tt Linie Gmbh & Co Schiffsantrieb
US4057027A (en) * 1974-08-08 1977-11-08 Foster Daniel S Boat propulsion with surface-running propeller drive
DE2516426A1 (de) * 1975-04-15 1976-10-28 Schottel Werft Strahl-steueranlage fuer wasserfahrzeuge
DE3005682C2 (de) * 1980-01-28 1982-11-11 Escher Wyss Gmbh, 7980 Ravensburg Schiffantriebsanlage
US4550673A (en) * 1983-06-02 1985-11-05 Sigurdur Ingvason Hull construction for seagoing vessels
JPS61178294A (ja) * 1985-01-31 1986-08-09 Mitsubishi Heavy Ind Ltd 魚雷形没水体付き２軸型高速艇
SE470285B (sv) * 1992-05-22 1994-01-10 Volvo Penta Ab Drivaggregat för fartyg
US6213824B1 (en) * 2000-02-11 2001-04-10 Power Vent Technologies, Inc. Method for reducing vessel draft
US6361387B1 (en) * 2001-01-19 2002-03-26 Brunswick Corporation Marine propulsion apparatus with dual driveshafts extending from a forward end of an engine
NO317226B1 (no) * 2002-05-08 2004-09-20 Moss Maritime As Propell akselarrangement
US7070469B2 (en) * 2004-09-15 2006-07-04 James Stallings Dual propeller surface drive propulsion system for boats
JP4220970B2 (ja) * 2005-01-31 2009-02-04 有限会社アークシステム 船舶推進構造および船舶駆動装置
DE102005050640B4 (de) * 2005-10-20 2009-08-27 Voith Turbo Gmbh & Co. Kg Schiffsantrieb

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2407799A1 (de) * 1974-02-19 1975-08-28 Berndt Martens Querstrahl-steueranlage fuer wasserfahrzeuge
DE3937327A1 (de) * 1988-11-14 1990-05-17 Kawasaki Heavy Ind Ltd Schiffsantriebseinrichtung
DE4206720A1 (de) * 1991-03-11 1992-09-17 Kawasaki Heavy Ind Ltd Schiffsantriebseinrichtung
EP1892183A1 (en) * 2005-03-11 2008-02-27 Kabushiki Kaisha Kawasaki Zosen Stern structure of ship

Also Published As

Publication number Publication date
WO2012031740A1 (de) 2012-03-15
EP2613999A1 (de) 2013-07-17
LT2613999T (lt) 2019-11-11
PL2613999T3 (pl) 2019-09-30
SI2613999T1 (sl) 2019-08-30
DE102010044435A1 (de) 2012-03-08
PL2613999T4 (pl) 2019-09-30
ES2743312T3 (es) 2020-02-18
PT2613999T (pt) 2019-07-25
HUE044175T2 (hu) 2019-10-28
HRP20191184T1 (hr) 2019-10-04
DK2613999T3 (da) 2019-07-15

Similar Documents

Publication Publication Date Title
EP2613999B1 (de) Antrieb
DE60019264T2 (de) Abgasmischvorrichtung und gerät mit einer solchen vorrichtung
DE102009040471B4 (de) Mechanisch angetriebener Schiffpropulsor mit hohem Wirkungsgrad
EP2279112B1 (de) Strömungsmaschine mit zumindest zwei kontrarotierbaren rotoren und mechanischem momentenausgleich
EP2591994B1 (de) Vorrichtung zur Verringerung des Antriebsleistungsbedarfs eines Wasserfahrzeuges
DE9013099U1 (de) Rotor
EP2597030B1 (de) Vordüse für ein Antriebssystem eines Wasserfahrzeuges zur Verbesserung der Energieeffizienz
DE3530769A1 (de) Stromlinienkoerper fuer turbinentriebwerke
DE2439484A1 (de) Druckgasmaschine
EP2994379A1 (de) Vorrichtung zur verringerung des antriebsleistungsbedarfs eines wasserfahrzeuges
EP0790921B1 (de) Schiffsantrieb mit einem ruderpropeller
EP1445193A1 (de) Turbopropantrieb mit zwei mitläufigen und axial versetzten Propeller
EP1964774A2 (de) Fluggerät mit rotierenden Zylindern zur Erzeugung von Auftrieb und/oder Vortrieb
DE102015010239B4 (de) Torus-Turbinen-Rotorantrieb für Helikopter, Multikopter oder für Turbo-Fan Flugzeuge
EP2223853A1 (de) Strömungsdynamische Fläche mit einer von einer durch die angeströmte Fläche induzierten Strömung angetriebenen Turbine
DE3508203A1 (de) Schiffsantrieb
EP2519739A2 (de) Geometrische anordnung von teilen eines energiewandlers und turbinenanordnung zur umwandlung von in einer strömung eines fluids enthaltener energie in elektrische energie
CH714302A2 (de) Aerodynamisch optimiertes Rotorblatt.
EP2730772B1 (de) Düse mit Leitvorrichtungen
EP1306301B1 (de) Vorrichtung zur Entgegenwirkung von im Nabenbereich von Propellern und/oder Propellerantrieben im umgebenden Fluid erzeugten Strömungswirbeln
AT523720B1 (de) Turbine für eine Windenergieanlage und eine Windenergieanlage
WO2002020347A2 (de) Ausserhalb des rumpfes angeordneter antrieb für ein wasserfahrzeug
DE10334900A1 (de) Schiffsantrieb
DE102022129372A1 (de) Düsenpropeller für Propulsionssysteme
DE102013018146B4 (de) Einspritzelement für eine Raketenbrennkammer

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20130311

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: LAIS, SIEGFRIED

17Q First examination report despatched

Effective date: 20160614

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20180704

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: REINTRIEB GMBH

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 1115409

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190415

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502011015560

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: HR

Ref legal event code: TUEP

Ref document number: P20191184

Country of ref document: HR

REG Reference to a national code

Ref country code: RO

Ref legal event code: EPE

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: PATENTANWAELTE SCHAAD, BALASS, MENZL AND PARTN, CH

Ref country code: DK

Ref legal event code: T3

Effective date: 20190708

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: PT

Ref legal event code: SC4A

Ref document number: 2613999

Country of ref document: PT

Date of ref document: 20190725

Kind code of ref document: T

Free format text: AVAILABILITY OF NATIONAL TRANSLATION

Effective date: 20190718

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: EE

Ref legal event code: FG4A

Ref document number: E017770

Country of ref document: EE

Effective date: 20190715

REG Reference to a national code

Ref country code: HR

Ref legal event code: ODRP

Ref document number: P20191184

Country of ref document: HR

Payment date: 20190827

Year of fee payment: 9

REG Reference to a national code

Ref country code: NO

Ref legal event code: T2

Effective date: 20190403

REG Reference to a national code

Ref country code: HR

Ref legal event code: T1PR

Ref document number: P20191184

Country of ref document: HR

REG Reference to a national code

Ref country code: GR

Ref legal event code: EP

Ref document number: 20190402013

Country of ref document: GR

Effective date: 20191016

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E044175

Country of ref document: HU

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: EE

Payment date: 20190902

Year of fee payment: 9

Ref country code: IE

Payment date: 20190910

Year of fee payment: 9

Ref country code: FI

Payment date: 20190909

Year of fee payment: 9

Ref country code: DK

Payment date: 20190910

Year of fee payment: 9

Ref country code: MC

Payment date: 20190828

Year of fee payment: 9

Ref country code: SI

Payment date: 20190829

Year of fee payment: 9

Ref country code: PT

Payment date: 20190820

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: HR

Payment date: 20190827

Year of fee payment: 9

Ref country code: BE

Payment date: 20190827

Year of fee payment: 9

Ref country code: BG

Payment date: 20190829

Year of fee payment: 9

Ref country code: GR

Payment date: 20190829

Year of fee payment: 9

Ref country code: HU

Payment date: 20190905

Year of fee payment: 9

Ref country code: LV

Payment date: 20190830

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IS

Payment date: 20190827

Year of fee payment: 9

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502011015560

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20190913

Year of fee payment: 9

Ref country code: LT

Payment date: 20191016

Year of fee payment: 9

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2743312

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20200218

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

26N No opposition filed

Effective date: 20200106

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190906

REG Reference to a national code

Ref country code: HR

Ref legal event code: PBON

Ref document number: P20191184

Country of ref document: HR

Effective date: 20200906

REG Reference to a national code

Ref country code: EE

Ref legal event code: MM4A

Ref document number: E017770

Country of ref document: EE

Effective date: 20200930

Ref country code: FI

Ref legal event code: MAE

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

Effective date: 20200930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200930

Ref country code: FI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200906

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

Ref country code: LV

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200906

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20200930

REG Reference to a national code

Ref country code: LT

Ref legal event code: MM4D

Effective date: 20200906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200930

Ref country code: BG

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210331

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

Ref country code: HR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200906

Ref country code: GR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210406

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200906

Ref country code: PT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210409

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200930

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200930

Ref country code: SI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200907

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200930

Ref country code: HU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200907

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200906

REG Reference to a national code

Ref country code: SI

Ref legal event code: KO00

Effective date: 20210812

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190403

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: RO

Payment date: 20230823

Year of fee payment: 13

Ref country code: NO

Payment date: 20230911

Year of fee payment: 13

Ref country code: NL

Payment date: 20230915

Year of fee payment: 13

Ref country code: IT

Payment date: 20230829

Year of fee payment: 13

Ref country code: GB

Payment date: 20230824

Year of fee payment: 13

Ref country code: AT

Payment date: 20230825

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20230830

Year of fee payment: 13

Ref country code: PL

Payment date: 20230829

Year of fee payment: 13

Ref country code: FR

Payment date: 20230911

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20231009

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20231006

Year of fee payment: 13

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20240129