EP3318479B1 - Flüssigkeitführungsvorrichtung für azimutalpropeller - Google Patents

Flüssigkeitführungsvorrichtung für azimutalpropeller Download PDF

Info

Publication number
EP3318479B1
EP3318479B1 EP16196916.7A EP16196916A EP3318479B1 EP 3318479 B1 EP3318479 B1 EP 3318479B1 EP 16196916 A EP16196916 A EP 16196916A EP 3318479 B1 EP3318479 B1 EP 3318479B1
Authority
EP
European Patent Office
Prior art keywords
ring member
channel
inner ring
shaft housing
guiding device
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.)
Not-in-force
Application number
EP16196916.7A
Other languages
English (en)
French (fr)
Other versions
EP3318479A1 (de
Inventor
Veronica JONSSON
Niklas Lagesson
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.)
Caterpillar Propulsion Production AB
Original Assignee
Caterpillar Propulsion Production AB
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 Caterpillar Propulsion Production AB filed Critical Caterpillar Propulsion Production AB
Priority to EP16196916.7A priority Critical patent/EP3318479B1/de
Priority to DK16196916T priority patent/DK3318479T3/da
Publication of EP3318479A1 publication Critical patent/EP3318479A1/de
Application granted granted Critical
Publication of EP3318479B1 publication Critical patent/EP3318479B1/de
Not-in-force 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
    • B63H21/00—Use of propulsion power plant or units on vessels
    • B63H21/38—Apparatus or methods specially adapted for use on marine vessels, for handling power plant or unit liquids, e.g. lubricants, coolants, fuels or the like
    • B63H21/386—Apparatus or methods specially adapted for use on marine vessels, for handling power plant or unit liquids, e.g. lubricants, coolants, fuels or the like for handling lubrication liquids
    • 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
    • B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
    • B63H2005/1254—Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis
    • 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
    • B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
    • B63H2005/1254—Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis
    • B63H2005/1256—Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis with mechanical power transmission to propellers

Definitions

  • the present disclosure relates to an azimuth thruster.
  • the present disclosure relates to a fluid guiding device for an azimuth thruster, and an azimuth thruster including the fluid guiding device.
  • Azimuth thrusters are commonly used as propulsion devices for marine vessels.
  • Azimuth thrusters are at least partly arranged beneath a hull of a marine vessel and typically comprise an upper gear unit, an azimuth unit and a lower gear unit.
  • the upper gear unit is connected to a horizontal drive shaft via an upper gear crown wheel and configured to mechanically drive a vertical input shaft of the azimuth thruster.
  • the azimuth unit is connected to the upper gear unit via a slewing bearing.
  • the azimuth unit has an outer azimuth stem and an inner azimuth stem.
  • the slewing bearing allows a relative rotation between the outer azimuth stem and the inner azimuth stem so that the azimuth thruster can be slewed for maneuvering the vessel.
  • the lower gear unit includes one or more propellers connected to the vertical input shaft for providing thrust to the marine vessel.
  • the propeller may be a variable pitch propeller which allows to vary a pitch of the propeller blades.
  • the pitch may be varied by a piston moving under the influence of a pressure of a hydraulic fluid selectively supplied to the propeller.
  • NL 8 005 590 A shows an azimuth thruster with a fluid guiding device configured to guide lubricating oil for lubricating a lower gear unit from an upper compartment into a lower compartment of the azimuth thruster.
  • WO 2013/072549 A1 discloses the lubrication of a steerable thruster of a marine vessel.
  • the lubrication is based on splash-type lubrication at the pod and full bath lubrication in the stembox and in the shank.
  • the lubrication oil enters the pod both from the stembox and the shank via a constriction and directly from an oil tank. The oil is further circulated from the pod to the oil tank by means of pumps.
  • the present disclosure is directed, at least in part, to improving or overcoming one or more aspects of prior systems.
  • the present disclosure relates to a fluid guiding device for an azimuth thruster.
  • the fluid guiding device comprises an inner ring member extending circumferentially about a longitudinal axis, and including a first inner ring member channel.
  • the fluid guiding device further comprises an outer ring member arranged coaxial around the inner ring member, and including a first outer ring member channel fluidly connected to the first inner ring member channel.
  • the inner ring member and the outer ring member are movable with respect to each other in a radial direction of the longitudinal axis. Further, the inner ring member is sealingly engaged with the outer ring member and the inner ring member is rotatable with respect to the outer ring member.
  • an azimuth thruster comprises a variable pitch propeller, and a fluid guiding device according to the above aspect or any embodiment as disclosed herein.
  • the first inner ring member channel and the first outer ring member channel are fluidly connected to the variable pitch propeller for varying a pitch.
  • an azimuth thruster comprises an upper gear housing accommodating an upper gear unit, and rotatable inner azimuth stem for slewing the azimuth thruster.
  • the azimuth thruster further comprises a fluid guiding device according to the above aspect or any embodiment as disclosed herein, wherein a shaft housing is connected to the upper gear housing, and the outer ring member is connected to the inner stem so that the outer ring member rotates relative to the shaft housing when the inner stem is rotated about the longitudinal axis.
  • a fluid guiding device for an azimuth thruster with a drive shaft comprises a shaft housing extending along a longitudinal axis and configured to support the drive shaft of the azimuth thruster.
  • the shaft housing includes a first shaft housing channel.
  • the fluid guiding device comprises an outer ring member arranged coaxial around the shaft housing and including a first outer ring member channel.
  • the fluid guiding device comprises an inner ring member arranged coaxial around the shaft housing between the shaft housing and the outer ring member.
  • the inner ring member includes a first inner ring member channel fluidly interconnected between the first shaft housing channel and the outer ring member channel.
  • the inner ring member and the outer ring member are movable with respect to each other in a radial direction of the longitudinal axis.
  • a swivel assembly may be integrated into an azimuth thruster for guiding a hydraulic fluid from a stationary component to a lower gear unit and a propeller, which are rotatable relative to the stationary component about a longitudinal axis of a vertical drive shaft of the azimuth thruster.
  • the swivel assembly may include a rotatable inner ring member and a rotatable outer ring member, wherein the ring members are arranged and configured to allow a movement between both ring members in a radial direction of the longitudinal axis. Said configuration allows to accommodate a radial movement resulting from a thrust force of the propeller which may slightly bend and/or displace the drive shaft.
  • a rotatable inner ring member for a fluid guiding device of an azimuth thruster.
  • the inner ring member includes at least one inner ring member channel.
  • the inner ring member includes a stepped outer circumferential face.
  • the inner ring member may include at least one first annular sealing face extending in a radial direction of a longitudinal axis of the inner ring member and including at least one first annular groove accommodating at least one first seal ring.
  • the inner ring member may include a second annular sealing face extending parallel to the longitudinal axis, the second sealing face including at least one second annular accommodating at least one second seal ring.
  • Fig. 1 shows a schematic drawing of an exemplary azimuth thruster 100 for a marine vessel.
  • the azimuth thruster 100 includes an upper gear unit 102, an azimuth unit 104 and a lower gear unit 106.
  • the upper gear unit 102 includes a substantially horizontal drive shaft 108 for connecting to a drive source.
  • the drive shaft 108 terminates to an upper gear pinion wheel 110.
  • the upper gear pinion wheel 110 includes an upper gear pinion wheel extension 112 configured to rotatably support the horizontal drive shaft 108 within an upper gear housing 114.
  • the upper gear pinion wheel 110 is configured to transmit power from the horizontal drive shaft 108 to an upper gear crown wheel 116.
  • the upper gear crown wheel 116 is mounted on top of a substantially vertical drive shaft 118.
  • the vertical drive shaft 118 includes an upper crown wheel shaft 120, an intermediate shaft 122, and a lower pinion shaft 124.
  • the upper crown wheel shaft 120 is drivably connected to the intermediate shaft 122 via a first connection 126.
  • the lower pinion shaft 124 is drivably connected to the intermediate shaft 122 via a second connection 128.
  • the first and second connections 126, 128 may be splined connections, flexible shaft couplings and/or floating shaft couplings.
  • the vertical input shaft 118 terminates to a lower gear pinion wheel 130 formed on the lower pinion shaft 124.
  • the lower gear pinion wheel 130 extends into the lower gear unit 106 and transmits the power to a lower gear crown wheel 132.
  • the lower gear crown wheel 132 is connected to a propeller shaft 134.
  • the propeller shaft 134 extends substantially horizontal and is provided with a propeller 136 for providing thrust to the azimuth thruster 100.
  • the propeller 136 may be any type of propeller 136 known to a person skilled in the art, for example a variable or fixed pitch propeller.
  • the propeller 136 is surrounded by a nozzle 138.
  • the nozzle 138 is fixedly connected to the lower gear unit 106 and may be any type of nozzle known to a person skilled in the art.
  • the nozzle 138 is configured to increase a thrust of the propeller 136 and to protect the propeller 136 against, for example, debris.
  • the azimuth thruster 100 may not include the nozzle 138.
  • the lower gear unit 106 including the propeller 136 and the nozzle 138 need to be rotated (slewed) around the vertical input shaft 118.
  • the upper gear unit 102 needs to be stationary, e.g. non-rotatable, whereas the lower gear unit 106 needs to be rotatable.
  • the azimuth thruster 100 includes the azimuth unit 104.
  • the azimuth unit 104 is connected to the upper gear unit 102 via a separation plate 140.
  • the separation plate 140 includes an opening 142 configured to at least partially accommodate the upper crown wheel shaft 120.
  • the separation plate 140 at least partially separates the azimuth unit 104 from the upper gear unit 102.
  • An upper crown wheel shaft housing (not shown in Fig. 1 ) may be connected to the separation plate 140 and may protrude through the opening 142 for rotatably supporting the upper crown wheel shaft 120 via suitable bearings.
  • the azimuth unit 104 further includes an azimuth stem 144 with an inner azimuth stem 146 and an outer azimuth stem 148.
  • the outer azimuth stem 148 is connected to the separation plate 140 via a ring body 152.
  • the ring body 152 is fixedly connected to an annular flange 150 of the outer azimuth stem 148.
  • the annular flange 150 is fixedly connected to a hull structure (foundation) of the marine vessel.
  • the outer azimuth stem 148 including the separation plate 140 and the upper gear unit 102 are stationary, e.g. non-rotatable, with respect to the marine vessel.
  • a ring-shaped gearwheel 154 is rotatable relative to the outer ring body 152 via a bearing 153.
  • the ring-shaped gearwheel 154 is fixedly connected to the inner azimuth stem 146.
  • the outer ring body 152 and the ring-shaped gearwheel 154 together form a slewing bearing 156.
  • the outer ring body 152 forms an outer race of the slewing bearing 156
  • the ring-shaped gearwheel 154 forms an inner race of the slewing bearing 156.
  • the slewing bearing 156 is configured to allow a rotation of the inner azimuth stem 146 relative to the outer azimuth stem 148 (relative rotation between the ring-shaped gearwheel 154 and the outer ring body 152).
  • the ring-shaped gearwheel 154 includes teeth on an inner circumferential face.
  • a slewing drive including at least one drive gearwheel (both not shown) is arranged to rotate the ring-shaped gearwheel 154. Specifically, teeth on an outer circumferential face of the at least one drive gearwheel engage with the teeth on the inner circumferential face of the ring-shaped gearwheel 154.
  • the slewing drive rotates the at least one drive gearwheel which in turn rotates the ring-shaped gearwheel 154 relative to the outer ring body 152.
  • the inner azimuth stem 146 is connected at its lower part to a vertical shaft housing 158.
  • the vertical shaft housing 158 surrounds the vertical input shaft 118 and connects the inner azimuth stem 146 with the lower gear unit 106.
  • the vertical shaft housing 158 is fixedly connected to a lower gear housing 159.
  • the lower gear housing 159 surrounds the lower gear transmission of the lower gear unit 106.
  • the lower gear unit 106 is rotatable relative to the upper gear unit 102 via the slewing bearing 156.
  • Lubricant compartment 160 is disposed to accommodate lubricant for bath lubricating the slewing bearing 156.
  • Lubricant may be any type of lubricant known to a person skilled in the art.
  • the lubricant may be oil.
  • the lubricant compartment 160 is formed by an annular space surrounding the vertical input shaft 118.
  • the lubricant compartment 160 is filled with lubricant such that the slewing bearing 156 is immersed in lubricant for arranging a full bath lubrication of the slewing bearing 156.
  • a radial shaft seal 157 is arranged between a lower end of the outer azimuth stem 148 and a lower end of inner azimuth stem 146.
  • the lubricant compartment 160 accommodates a volume of lubricant in a range between about 0.5 m 3 and about 3 m 3 , depending on the type and size of the azimuth thruster 100 and the inner azimuth stem 146.
  • the drive shaft 118 is supported by a shaft housing (not shown in Fig. 1 ), which surrounds the upper crown wheel shaft 120.
  • said shaft housing is depicted together with further components constituting a fluid guiding device for guiding a fluid from an upper region of the azimuth thruster 100 to the propeller 136.
  • Figs. 2 and 3 show vertical cross-sections of the fluid guiding device 200 at different circumferential positions.
  • the fluid guiding device 200 comprises a shaft housing 202, and a swivel assembly 204 including an inner ring member 206 and an outer ring member 208.
  • the shaft housing 202 is configured to rotatably support the drive shaft 118 (see Fig. 1 ) at an upper region thereof via suitable bearings not shown in further detail here.
  • the shaft housing 202 extends along a longitudinal axis A, which coincides with a longitudinal axis of the drive shaft 118.
  • the shaft housing 202 includes an annular mounting portion 210 at an upper end.
  • the mounting portion 210 is fastened to the separation plate 140, for example an inner circumferential edge portion of the separation plate 140, which defines the opening 142 (see Fig. 1 ).
  • the mounting portion 210 may be fastened to the upper gear housing 114.
  • the shaft housing 202 further includes a substantially hollow cylindrical portion 212, through which the drive shaft 118 (see Fig. 1 ) extends in an assembled state.
  • a first shaft housing channel 214 (see Fig. 2 ) and a second shaft housing channel 216 (see Fig. 3 ) extend through the shaft housing 202.
  • the first and second shaft housing channels 214 and 216 extend through the shaft housing 202 at different circumferential positions of the shaft housing 202 with respect to the longitudinal axis A.
  • the first and second shaft housing channels 214 and 216 include an arcuate (curved) shape along their extension.
  • the first shaft housing channel 214 extends between an opening 220 in a circumferential outer face 218 of the mounting portion 210, and an opening 222 in a bottom region of the substantially hollow cylindrical portion 212.
  • the same may extend until an opening in an annular end face 223 of the substantially hollow cylindrical portion 212, which is sealed (for example, by a plug) after machining so that fluid can be guided in the first shaft housing channel 214 between the openings 220 and 222.
  • the second shaft housing channel 216 extends between an opening 224 in a circumferential outer face 218 of the mounting portion 210, and an opening 226 in a bottom region of the substantially hollow cylindrical portion 212. Similar to the first shaft housing channel 214, the second shaft housing channel 216 may extend until an opening in the annular end face 223, which is sealed after machining so that fluid can be guided in the second shaft housing channel 216 between the openings 224 and 226.
  • the opening 220 of the first shaft housing channel 214 and the opening 224 of the second shaft housing channel 216 are arranged to overlap with respect to a longitudinal position (height position) along the longitudinal axis A.
  • the opening 220 and the opening 224 are arranged to be spaced apart with respect to a circumferential position about the longitudinal axis A.
  • the opening 222 of the first shaft housing channel 214 and the opening 226 of the second shaft housing channel 216 are arranged to be spaced apart with respect to a longitudinal position along the longitudinal axis A.
  • the opening 222 and the opening 226 of the second shaft housing channel 216 are arranged to be spaced apart with respect to a circumferential position about the longitudinal axis A.
  • the openings 220-226 may be arranged in any other fashion allowing to fluidly isolate the first shaft housing channel 214 and the second shaft housing channel 216.
  • a hydraulic fluid system not shown in further detail may be connected to the openings 220 and 224 for supplying and drawing hydraulic fluid as desired.
  • the hydraulic fluid system may be configured to control a pitch of the variable pitch propeller 136 ( Fig. 1 ) as described in greater detail later on.
  • a lubrication oil system not shown in further detail may be connected to the openings 220 and/or 224.
  • the inner ring member 206 is arranged coaxial around the shaft housing 202 to surround a bottom region of the substantially hollow cylindrical portion 212.
  • the inner ring member 206 may be made of a low-friction material such as bronze.
  • the inner ring member 206 includes an inner circumferential face 228 and a stepped outer circumferential face 230.
  • the inner circumferential face 228 of the inner ring member 206 and an outer circumferential face 232 define a first inner annular channel 234 and a second inner annular channel 236.
  • the first inner annular channel 234 and the second inner annular channel 236 are fluidly isolated to each other by an inner intermediate seal ring 238.
  • the first and second inner annular channels 234, 236 extend coaxial between the inner ring member 206 and the shaft housing 202.
  • the inner annular channels 234, 236 are arranged spaced apart with respect to a longitudinal position along the longitudinal axis A.
  • the first shaft housing channel 214 is fluidly connected to the first inner annular channel 234 via the opening 222.
  • the second shaft housing channel 216 is fluidly connected to the second inner annular channel 236 via the opening 226.
  • the inner ring member 206 and the shaft housing 202 are rotatable with respect to each other. Additionally, the inner ring member 206 is connected to the shaft housing 202 to follow a radial movement of the shaft housing 202 with respect to the longitudinal axis A. Said radial movement may result from a thrust force of the propeller 136 which may slightly bend and/or displace the drive shaft 118 supported by the shaft housing 202 in a radial direction of the longitudinal axis A. Said radial movement is oppositely directed to the water jet generated by the propeller 136.
  • the inner ring member 206 is sealingly engaged with the shaft housing 202 via an inner upper seal ring 240, the inner intermediate seal ring 238, and an inner lower seal ring 242.
  • the inner upper seal ring 240 seals between the first inner annular channel 234 and an exterior of the swivel assembly 204.
  • the inner intermediate seal ring 238 seals between the first inner annular channel 234 and the second inner annular channel 236.
  • the inner lower seal ring 242 seals between the second inner annular channel 236 and an exterior of the swivel assembly 204.
  • the seal rings 238-242 are accommodated in corresponding grooves extending in the inner circumferential face 228 of the inner ring member 206.
  • the seal rings 238-242 may be accommodated in corresponding grooves extending in the outer circumferential face 232 of the shaft housing 202.
  • the seal rings 238-242 may be formed by flexible outer ring bodies connected (glued etc.) to low-friction inner ring bodies, for example, made up of Teflon.
  • the flexible outer ring bodies may press the low-friction inner ring bodies against the outer circumferential face 232 of the shaft housing 202 for obtaining a sealing effect while allowing a rotational movement between the inner ring member 206 and the shaft housing 202.
  • the at least one first inner ring member channel 244 extends through a first portion 245 of the inner ring member 206, and the at least one second inner ring member channel 246 extends through a second portion 247 of the inner ring member 206.
  • the first portion 245 has a greater thickness then the second portion 247 in a radial direction of the longitudinal axis A.
  • the at least one first inner ring member channel 244 and the at least one second inner ring member channel 246 are arranged spaced apart with respect to a longitudinal position along the longitudinal axis A. In other words, the at least one first inner ring member channel 244 is arranged above the at least one second inner ring member channel 246 in a vertical direction.
  • the inner ring member 206 includes at least one first inner ring member channel 244 and at least one second inner ring member channel 246.
  • the at least one first inner ring member channel 244 extends between the first inner annular channel 234 and a first outer annular channel 248.
  • the at least one second inner ring member channel 246 extends between the second inner annular channel 236 and a second outer annular channel 250.
  • the at least one first inner ring member channel 244 and the at least one second inner ring member channel 246 extend in a radial direction with respect to the longitudinal axis A.
  • the first and second outer annular channels 248, 250 are defined by the outer circumferential face 230 of the inner ring member 206 and a stepped inner circumferential face 252 of the outer ring member 208.
  • the first and second outer annular channels 248, 250 extend coaxial between the inner ring member 206 and the outer ring member 208.
  • the first and second outer annular channels 248, 250 are fluidly isolated from each other by an outer intermediate seal ring 254.
  • the outer intermediate seal ring 254 is accommodated in an annular groove 256 of a sealing face 258 of the inner ring member 206.
  • the sealing face 258 extends in a radial direction of the longitudinal axis A so that a sealing effect is obtained by the outer intermediate seal ring 254 even if a slight radial movement between the inner ring member 206 and outer ring member 208 occurs.
  • the outer intermediate seal ring 254 may be accommodated in an annular groove of a radially extending sealing face of the outer ring member 208.
  • the inner ring member 206 is sealingly engaged with the outer ring member 208 via first and second outer upper seal rings 260, 262, the outer intermediate seal ring 254, and an outer lower seal ring 264.
  • the first and second outer upper seal rings 240 seal between the first outer annular channel 248 and an annular plate 266 mounted on top of the outer ring member 208.
  • the inner intermediate seal ring 254 seals between the first outer annular channel 248 and the second outer annular channel 250.
  • the outer lower seal ring 264 seals the second outer annular channel 250.
  • the outer ring member 208 of the swivel assembly 204 is arranged coaxial around the shaft housing 202 and the inner ring member 206.
  • the inner ring member 206 and the outer ring member 208 are movable with respect to each other in a radial direction of the longitudinal axis A while maintaining a sealing engagement of the seal rings 254, 260-264, which seal against radially extending sealing faces.
  • the inner ring member 206 is rotatable with respect to the shaft housing 202 and the outer ring member 208.
  • the outer ring member 208 includes a first portion 268 and a second portion 270.
  • the first portion 268 has a smaller thickness than the second portion 270 in a radial direction of the longitudinal axis A.
  • the first portion 268 and the second portion 270 are connected to one another.
  • the first portion 268 of the outer ring member 208 is positioned to substantially overlap the first portion 245 of the inner ring member 206 viewed in a radial direction of the longitudinal axis A.
  • the second portion 270 of the outer ring member 208 is positioned to substantially overlap the second portion 247 of the inner ring member 206 viewed in a radial direction of the longitudinal axis A.
  • a first outer ring member channel 272 extends through the first and second portions 268 and 270 to fluidly interconnect the first outer annular channel 248 and a first hydraulic fluid tube 274 connected to a variable pitch mechanism of the propeller 136.
  • a second outer ring member channel 276 extends through the second portion 270 to fluidly interconnect the second outer annular channel 250 and a second hydraulic fluid tube 278 connected to the variable pitch mechanism.
  • outer ring member channels 272, 276, may extend until an opening in an outer circumferential face 280 of outer ring member 208, which are sealed after machining (for example, by inserting a plug) so that fluid can be guided in the first and second outer ring member channels 272 and 276 between first and second outer annular channels 248 and 250, and the first and second hydraulic fluid tubes 274 and 278, respectively.
  • the first and second outer ring member channels 272 and 276 are spaced apart from each other with respect to a circumferential position around the longitudinal axis A.
  • the outer ring member 208 is fastened to the inner azimuth stem 146 (see Fig. 1 ) via a plurality of radially extending supports 282 so that the outer ring member 208 rotates together with the inner azimuth stem 146 (and the lower gear unit 106) when rotating the azimuth thruster 100 is rotated about the longitudinal axis A.
  • first shaft housing channel 214, the first inner annular channel 234, the first inner ring member channel 244, the first outer annular channel 248, and the first outer ring member channel 272 together define a first fluid passage for guiding a hydraulic fluid.
  • second shaft housing channel 216, the second inner annular channel 236, the second inner ring member channel 246, the second outer annular channel 250, and the second outer ring member channel 276 together define a second fluid passage.
  • the first fluid passage and the second fluid passage are fluidly isolated from each other.
  • the first fluid passage and the second fluid passage as noted above may be used to supply a hydraulic fluid to a variable pitch mechanism of the propeller 136.
  • hydraulic fluid may be supplied via the first fluid passage to a first chamber to displace a piston of the variable pitch mechanism for varying the pitch. While increasing a volume of the first chamber, the piston pushes hydraulic fluid out of a second chamber and into the second fluid passage.
  • hydraulic fluid may be supplied via the second fluid passage to the second chamber to displace the piston to vary the pitch, and simultaneously pushing hydraulic fluid from the first chamber into the first fluid passage.
  • one of the first and the second fluid passages may be sufficient for varying the pitch depending on the specific variable pitch mechanism.
  • the first fluid passage and/or the second fluid passage may be used to supply any other fluid to the lower gear unit 106.
  • the first fluid passage and/or the second fluid passage may be used to supply a lubricant to the lower gear unit 106 and/or the propeller 136 for providing a point lubrication.
  • one of the first fluid passage and the second fluid passage may be omitted.
  • the inner ring member 206 is arranged in a floating manner between the outer ring member 208 and the shaft housing 202. That is, the inner ring member 206 is arranged to follow the radial movement of the shaft housing 202 to radially move relative to the outer ring member 208.
  • the inner and outer ring members 206 and 208 may be dimensioned so that a radial movement greater than 0 mm between the inner and outer ring members 206 and 208 can be accommodated.
  • a clearance gap between the inner and outer ring members 206 and 208 may be within a range between about 0,5 mm and 10 mm, or even greater.
  • the stepped configuration of the inner ring member 206 (outer circumferential face 230) and the outer ring member 208 (inner circumferential face 252) together with the seal rings 254, and 260 to 264, which are disposed in sealing faces extending in a radial direction of the longitudinal axis A, allows a relative radial movement between the inner ring member 206 and outer ring member 208 while maintaining a sealing engagement.
  • the outer ring member 208 rotates together with the inner stem 146.
  • the inner ring member 206 typically tends to at least partially rotate together with the outer ring member 208 due to the higher friction caused by the outer seal rings 254, 262 and 264 relative to the low-friction inner seal rings 238-242. As a result, the inner ring member 206 rotates relative to the shaft housing 202.
  • the fluid guiding device as disclosed herein is applicable for integration in an azimuth thruster for providing thrust to a marine vessel.
  • the fluid guiding device allows to guide a fluid in fluidly isolated channels from a fixed shaft housing for a drive shaft of the azimuth thruster and a rotatable swivel assembly, which is rotatable together with the inner azimuth stem, the lower gear unit, and the propeller about a longitudinal axis of the drive shaft.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Details Of Gearings (AREA)

Claims (14)

  1. Fluidführungsvorrichtung (200) für einen Azimutantrieb (100), umfassend:
    ein inneres Ringelement (206), das sich in Umfangsrichtung um eine Längsachse (A) erstreckt und einen ersten inneren Ringelementkanal (244) aufweist; und
    ein äußeres Ringelement (208), das koaxial um das innere Ringelement (206) angeordnet ist und einen ersten äußeren Ringelementkanal (272) aufweist, der mit dem ersten inneren Ringelementkanal (244) fluidisch verbunden ist;
    wobei das innere Ringelement (206) abdichtend mit dem äußeren Ringelement (208) in Eingriff steht;
    wobei das innere Ringelement (206) in Bezug auf das äußere Ringelement (208) drehbar ist; und
    wobei das innere Ringelement (206) und das äußere Ringelement (208) in radialer Richtung der Längsachse (A) zueinander beweglich sind.
  2. Fluidführungsvorrichtung (200) nach Anspruch 1, ferner umfassend:
    ein Wellengehäuse (202), das sich entlang der Längsachse (A) erstreckt und so konfiguriert ist, dass es eine Antriebswelle (118) des Azimutantriebs (100) trägt, wobei das Wellengehäuse (202) einen ersten Wellengehäusekanal (214) aufweist, der fluidisch mit dem ersten inneren Ringelementkanal (244) verbunden ist.
  3. Fluidführungsvorrichtung (200) nach Anspruch 2, wobei das innere Ringelement (206) mit dem Wellengehäuse (202) verbunden ist, um einer Radialbewegung des Wellengehäuses (202) in Bezug auf die Längsachse (A) zu folgen.
  4. Fluidführungsvorrichtung (200) nach einem der Ansprüche 2 oder 3, wobei:
    das innere Ringelement (206) abdichtend mit dem Wellengehäuse (202) in Eingriff steht; und/oder
    das innere Ringelement (206) in Bezug auf das Wellengehäuse (202) drehbar ist.
  5. Fluidführungsvorrichtung (200) nach einem der vorhergehenden Ansprüche, wobei eine äußere Umfangsfläche (230) des inneren Ringelements (206) und eine innere Umfangsfläche (252) des äußeren Ringelements (208) so konfiguriert sind, dass sie einen ersten äußeren Ringkanal (248) definieren, der den ersten inneren Ringelementkanal (244) und den ersten äußeren Ringelementkanal (272) fluidisch verbindet.
  6. Fluidführungsvorrichtung (200) nach einem der Ansprüche 2 bis 5, wobei eine innere Umfangsfläche (228) des inneren Ringelements (206) und eine äußere Umfangsfläche (232) des Wellengehäuses (202) so konfiguriert sind, dass sie einen ersten inneren Ringkanal (234) definieren, der den ersten Wellengehäusekanal (214) und den ersten inneren Ringelementkanal (244) fluidisch verbindet.
  7. Fluidführungsvorrichtung (200) nach einem der Ansprüche 2 bis 6, wobei:
    das Wellengehäuse (202) einen zweiten Wellengehäusekanal (216) aufweist;
    das äußere Ringelement (208) einen zweiten äußeren Ringelementkanal (276) aufweist; und
    das innere Ringelement (206) einen zweiten inneren Ringelementkanal (246) aufweist, der zwischen dem zweiten Wellengehäusekanal (216) und dem zweiten äußeren Ringelementkanal (276) fluidisch verbunden ist.
  8. Fluidführungsvorrichtung (200) nach Anspruch 7, wobei:
    eine innere Umfangsfläche (228) des inneren Ringelements (206) und eine äußere Umfangsfläche (232) des Wellengehäuses (202) so konfiguriert sind, dass sie einen zweiten inneren Ringkanal (236) definieren, der den zweiten Wellengehäusekanal (216) und den zweiten inneren Ringelementkanal (246) fluidisch verbindet, und/oder
    eine äußere Umfangsfläche (230) des inneren Ringelements (206) und eine innere Umfangsfläche (252) des äußeren Ringelements (208) so konfiguriert sind, dass sie einen zweiten äußeren Ringkanal (250) definieren, der den zweiten inneren Ringelementkanal (246) und den zweiten äußeren Ringelementkanal (276) fluidisch verbindet.
  9. Fluidführungsvorrichtung (200) nach Anspruch 8, wobei
    der erste Wellengehäusekanal (214), der erste innere Ringkanal (234), der erste innere Ringelementkanal (244), der erste äußere Ringkanal (248) und der erste äußere Ringelementkanal (272) zusammen einen ersten Fluiddurchgang definieren;
    der zweite Wellengehäusekanal (216), der zweite innere Ringkanal (236), der zweite innere Ringelementkanal (246), der zweite äußere Ringkanal (250) und der zweite äußere Ringelementkanal (276) zusammen einen zweiten Fluiddurchgang definieren; und
    der erste Fluidkanal und der zweite Fluidkanal fluidisch voneinander isoliert sind.
  10. Fluidführungsvorrichtung (200) nach einem der vorhergehenden Ansprüche, wobei mindestens eines der inneren Ringelemente (206) und das äußere Ringelement (208) mindestens eine erste ringförmige Dichtfläche (258) aufweist, die sich in einer radialen Richtung der Längsachse (A) erstreckt und mindestens eine erste Ringnut (256) aufweist, die mindestens einen ersten Dichtring (254) zum Abdichten zwischen dem inneren Ringelement (206) und dem äußeren Ringelement (208) aufnimmt.
  11. Fluidführungsvorrichtung (200) nach einem der Ansprüche 2 bis 10, wobei mindestens eines der inneren Ringelemente (206) und das Wellengehäuse (202) eine zweite ringförmige Dichtfläche (228) aufweist, die sich parallel zur Längsachse (A) erstreckt, wobei die zweite Dichtfläche (228) mindestens eine zweite Ringnut (239) aufweist, die mindestens einen zweiten Dichtungsring (238) zum Abdichten zwischen dem inneren Ringelement (206) und dem Wellengehäuse (202) aufnimmt.
  12. Fluidführungsvorrichtung (200) nach einem der vorstehenden Ansprüche, wobei das innere Ringelement (206) aus Bronze hergestellt ist.
  13. Azimutantrieb (100), umfassend
    einen Verstellpropeller (136); und
    eine Fluidführungsvorrichtung (200) nach einem der Ansprüche 1 bis 12, wobei der erste innere Ringelementkanal (244) und der erste äußere Ringelementkanal (272) mit dem Verstellpropeller (136) zum Variieren einer Steigung fluidisch verbunden sind.
  14. Azimutantrieb (100), umfassend
    ein oberes Getriebegehäuse (114), das ein oberes Getriebe (102) aufnimmt;
    einen drehbaren inneren Azimutschaft (146) zum Schwenken des Azimutantriebs (100); und
    eine Fluidführungsvorrichtung (200) nach einem der Ansprüche 2 bis 12, wobei das Wellengehäuse (202) mit dem oberen Getriebegehäuse (114) verbunden ist und das äußere Ringelement (208) mit dem inneren Schaft (146) verbunden ist, sodass sich das äußere Ringelement (208) in Bezug auf das Wellengehäuse (202) dreht, wenn der innere Schaft (146) um die Längsachse (A) gedreht wird.
EP16196916.7A 2016-11-02 2016-11-02 Flüssigkeitführungsvorrichtung für azimutalpropeller Not-in-force EP3318479B1 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP16196916.7A EP3318479B1 (de) 2016-11-02 2016-11-02 Flüssigkeitführungsvorrichtung für azimutalpropeller
DK16196916T DK3318479T3 (da) 2016-11-02 2016-11-02 Fluidstyreindretning til azimutfremdrivningsmotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP16196916.7A EP3318479B1 (de) 2016-11-02 2016-11-02 Flüssigkeitführungsvorrichtung für azimutalpropeller

Publications (2)

Publication Number Publication Date
EP3318479A1 EP3318479A1 (de) 2018-05-09
EP3318479B1 true EP3318479B1 (de) 2019-07-31

Family

ID=57233326

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16196916.7A Not-in-force EP3318479B1 (de) 2016-11-02 2016-11-02 Flüssigkeitführungsvorrichtung für azimutalpropeller

Country Status (2)

Country Link
EP (1) EP3318479B1 (de)
DK (1) DK3318479T3 (de)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8005590A (nl) * 1980-10-09 1982-05-03 Ishikawajima Ship & Chem Voortstuw-stuurinrichting van het z-type.
IT1222924B (it) * 1987-10-15 1990-09-12 Mauro Salvetti Gruppo produlsore retrattile migliorato per imbracazioni
EP2780224B1 (de) * 2011-11-18 2016-01-13 Wärtsilä Finland Oy Verfahren zur anordnung der schmierung eines lenkbaren strahlruders eines wasserfahrzeugs und schmierungsanordnung dafür

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP3318479A1 (de) 2018-05-09
DK3318479T3 (da) 2019-10-28

Similar Documents

Publication Publication Date Title
US7641526B1 (en) Vessel and underwater mountable azimuthing thruster
US9611929B2 (en) Gearbox lubrication
EP3236111B1 (de) Ölübertragungseinheit zur übertragung von öl zwischen einem stehenden teil und einem sich drehenden teil
EP2230172A1 (de) Schifssantrieb mit gegendrehungspropeller
KR20120135341A (ko) 애지머스 추진기
JP2872866B2 (ja) 舶用二重反転プロペラ軸用軸受装置
EP3187414B1 (de) Öltransferanordnung zur zuführung von öl in ein drehendes und verschiebbares rohr
EP3318479B1 (de) Flüssigkeitführungsvorrichtung für azimutalpropeller
EP3279079B1 (de) Schmiersystem für azimuttriebwerk
US20180029680A1 (en) Method of arranging the lubrication of a controllable pitch propeller arrangement of a marine vessel and a lubrication arrangement therefor
KR100836637B1 (ko) 가변피치프로펠러 유압분배기(ｏｄ) 박스
US9751603B2 (en) Propulsion device for ship and ship comprising the same
KR100305260B1 (ko) 선미관베어링시스템
US8926466B2 (en) Vessel propulsion apparatus
US4142835A (en) Pitch controlling device of a marine propeller
JP2016211638A (ja) 動力伝達装置およびモータグレーダ
CN113382920A (zh) 摆线船用推进单元和配备有其的船舶
EP2716540B1 (de) Schiffsantriebsvorrichtung und schiff damit
JP2015147540A (ja) 船舶推進機
KR101422491B1 (ko) 선박용 추진장치 및 이를 포함하는 선박
JP6940368B2 (ja) 湿式多板クラッチ及び舶用推進装置
KR101444330B1 (ko) 선박용 추진장치 및 이를 갖춘 선박
EP3088296B1 (de) Trennplatte für ein azimuttriebwerk
KR102090935B1 (ko) 선박용 추진기 밀폐장치
JP4208943B1 (ja) 舶用スラスタの上部ギヤボックス構造

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

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

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

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

AX Request for extension of the european patent

Extension state: BA ME

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20181102

RBV Designated contracting states (corrected)

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

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: 20190211

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

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: CH

Ref legal event code: EP

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1160606

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190815

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602016017640

Country of ref document: DE

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

Effective date: 20191025

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NO

Ref legal event code: T2

Effective date: 20190731

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1160606

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190731

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

Ref country code: BG

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: 20191031

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: 20190731

Ref country code: HR

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: 20190731

Ref country code: FI

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: 20190731

Ref country code: PT

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: 20191202

Ref country code: AT

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: 20190731

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

Ref country code: SE

Payment date: 20191025

Year of fee payment: 4

Ref country code: NO

Payment date: 20191025

Year of fee payment: 4

Ref country code: NL

Payment date: 20191025

Year of fee payment: 4

Ref country code: DE

Payment date: 20191021

Year of fee payment: 4

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

Ref country code: ES

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: 20190731

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: 20190731

Ref country code: LV

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: 20190731

Ref country code: GR

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: 20191101

Ref country code: IS

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: 20191130

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: 20190731

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

Ref country code: DK

Payment date: 20191025

Year of fee payment: 4

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: 20190731

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

Ref country code: RO

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: 20190731

Ref country code: PL

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: 20190731

Ref country code: IT

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: 20190731

Ref country code: EE

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: 20190731

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

Ref country code: IS

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: 20200224

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: 20190731

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: 20190731

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: 20190731

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602016017640

Country of ref document: DE

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

PG2D Information on lapse in contracting state deleted

Ref country code: IS

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

Ref country code: LI

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

Effective date: 20191130

Ref country code: CH

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

Effective date: 20191130

Ref country code: MC

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: 20190731

Ref country code: LU

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

Effective date: 20191102

Ref country code: IS

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: 20191030

26N No opposition filed

Effective date: 20200603

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20191130

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

Ref country code: SI

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: 20190731

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

Ref country code: FR

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

Effective date: 20191130

Ref country code: IE

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

Effective date: 20191102

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

Ref country code: BE

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

Effective date: 20191130

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: 20190731

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602016017640

Country of ref document: DE

REG Reference to a national code

Ref country code: NO

Ref legal event code: MMEP

Ref country code: DK

Ref legal event code: EBP

Effective date: 20201130

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

REG Reference to a national code

Ref country code: NL

Ref legal event code: MM

Effective date: 20201201

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20201102

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

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: 20190731

Ref country code: HU

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

Effective date: 20161102

Ref country code: NO

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

Effective date: 20201130

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

Ref country code: SE

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

Effective date: 20201103

Ref country code: NL

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

Effective date: 20201201

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

Ref country code: DE

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

Effective date: 20210601

Ref country code: DK

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

Effective date: 20201130

Ref country code: GB

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

Effective date: 20201102

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: 20190731