EP4585504A1 - Method and arrangement for sealing a propeller shaft of a marine vessel - Google Patents

Method and arrangement for sealing a propeller shaft of a marine vessel

Info

Publication number
EP4585504A1
EP4585504A1 EP24151399.3A EP24151399A EP4585504A1 EP 4585504 A1 EP4585504 A1 EP 4585504A1 EP 24151399 A EP24151399 A EP 24151399A EP 4585504 A1 EP4585504 A1 EP 4585504A1
Authority
EP
European Patent Office
Prior art keywords
lubricant
seal chamber
arrangement
line part
line
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.)
Pending
Application number
EP24151399.3A
Other languages
German (de)
French (fr)
Inventor
Petri Pellinen
Tuomas Kekki
Sakari Siipilehto
Tuomas Herranen
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.)
ABB Oy
Original Assignee
ABB Oy
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 ABB Oy filed Critical ABB Oy
Priority to EP24151399.3A priority Critical patent/EP4585504A1/en
Priority to US19/010,454 priority patent/US20250229884A1/en
Priority to CA3261587A priority patent/CA3261587A1/en
Priority to JP2025003913A priority patent/JP2025109194A/en
Priority to CN202510043943.0A priority patent/CN120288226A/en
Priority to KR1020250003865A priority patent/KR20250110160A/en
Publication of EP4585504A1 publication Critical patent/EP4585504A1/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/321Bearings or seals specially adapted for propeller shafts
    • B63H23/326Water lubricated bearings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/321Bearings or seals specially adapted for propeller shafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/36Shaft tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/321Bearings or seals specially adapted for propeller shafts
    • B63H2023/327Sealings specially adapted for propeller shafts or stern tubes

Definitions

  • a problem with the above presented method and arrangement is the heating of the seal rings delimiting the lubricant seal chamber with leads to wear and reduced service-life of the seal rings.
  • the seal rings are heated due to the friction between the propeller shaft and the seal rings, because the seal rings engage the outer circumference of the rotating propeller shaft.
  • a propeller 5 is attached to a driving end 6 of the propeller shaft 1, wherein the driving end 6 projects out of the pod 3.
  • the propeller shaft 1 can additionally have a second driving end (not illustrated) that projects out of an opposite end of the pod 3 i.e. so that the propeller projects through the pod and so that a second propeller (not illustrated) is provided as the second driving end.
  • the propeller shaft 1 is rotatably supported with a bearing arrangement 8 inside the pod 3.
  • At least two seal rings 9 are provided axially spaced apart from each other in an axial direction of the propeller shaft 1 and engaging the outer circumference of the propeller shaft 1 such that at least one lubricant chamber 10 is delimited between adjacent seal rings 9.
  • the propeller shaft 1 can comprise a liner 20 that at least partly forms the outermost part of the propeller shaft 1.
  • the liner 20 forms the outermost part of the propeller shaft 1 at least in the region of the seal rings 11.
  • the bearing arrangement comprises a lubrication arrangement 11 comprising a lubricant circulation line 12 for conducting lubricant to said bearing arrangement 8 and for conducting lubricant from said bearing arrangement 8, and a lubricant circulator 13 configured to create a flow of lubricant in the lubricant circulation line 12 and in the bearing arrangement 8.
  • the method comprises providing the lubrication arrangement 11 with an additional lubrication circulation line 14 comprising a first line part 15 for conducting a part of said flow of lubricant to said at least one lubricant seal chamber 10 and comprising a second line part 16 for conducting said part of said flow of lubricant from said at least one lubricant seal chamber 10.
  • Said flow of lubricant in said at least one lubricant seal chamber 10 will lower the temperature in said at least one lubricant seal chamber 10 and consequently lower the temperature of the seal rings 9 delimiting said at least one lubricant seal chamber 10. This reduces wearing of the seal rings 9 and extends the service-life of the seal rings 9.
  • the height or the second line part 16 By adjusting the height or the second line part 16 can the pressure in said at least one lubricant seal chamber 10 be adjusted.
  • a higher height or the second line part 16 results in a higher lubricant level and into a higher pressure in in said at least one lubricant seal chamber 10 and this seals said at least one lubricant seal chamber 10 better and prevents thus leakage.
  • a higher pressure also extends the service-life of said at least two seal rings 9. Because said at least one lubricant seal chamber 10 will be full with lubricant, said at least two seal rings 9 will have a longer service-life.
  • the fourth embodiment illustrated in figure 4 comprises connecting the first line part 15 in fluid connection with a bottom of the bearing arrangement 8, and connecting the first line part 15 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the bottom of the bearing arrangement 8 into the bottom of said at least one lubricant seal chamber 10 in the first line part 15, and connecting the second line part 16 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13 and conducting said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12 in the second line part 16.
  • the method comprises preferably, but not necessarily, conducting thermal energy from lubricant circulating in the lubricant circulation line 12 with a cooler 17 provided in thermal contact with the lubricant circulation line 12. This additionally promotes cooling of said at least two seal rings 9.
  • the cooler 17 can be arranged within the pod 3 as illustrated in figures 1 to 4 or outside the pod and within the hull 4 of the marine vessel 2 as illustrated in figure 5 .
  • the method comprises preferably, but not necessarily, regulating the flow of lubricant in the first line part 15 by means of a throttle means 18 provided in the first line part 15.
  • a throttle means 18 can another type of flow regulating means be used.
  • the propeller shaft 1 is arranged at a pod 3 that is suspended at a hull 4 of the marine vessel 2.
  • the propeller shaft 1 is rotatably supported with a bearing arrangement 8 inside the pod 3.
  • At least two seal rings 9 are provided axially spaced apart from each other in an axial direction of the propeller shaft 1 and engaging the outer circumference of the propeller shaft 1 such that at least one lubricant seal chamber 10 is delimited between adjacent seal rings 9.
  • the lubrication arrangement comprises an additional lubrication circulation line 14 for conducting a part of said flow of lubricant to said at least one lubricant seal chamber 10 and for conducting said part of said flow of lubricant from said at least one lubricant seal chamber 10 and the lubrication arrangement being additionally configured to create a flow of lubricant in the additional lubricant circulation line 14 and in said at least one lubricant seal chamber 10.
  • Said flow of lubricant in said at least one lubricant seal chamber 10 will lower the temperature in said at least one lubricant seal chamber 10 and consequently lower the temperature of the seal rings 9 delimiting said at least one lubricant seal chamber 10. This reduces wearing of the seal rings 9 and extends the service-life of the seal rings 9.
  • the first line part 15 can be in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 into the bottom of said at least one lubricant seal chamber 10.
  • the second line part 16 can be in fluid connection with a top of said at least one lubricant seal chamber 10 and in fluid connection with the bearing arrangement 8, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the top of said at least one lubricant seal chamber 10 into the bearing arrangement 8.
  • the second line part 16 can be in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12.
  • the first line part 15 is in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 to said at least one lubricant seal chamber 10, and the second line part 16 is formed by an equalizing channel between said at least one lubricant seal chamber 10 and the bearing arrangement 8, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from said at least one lubricant seal chamber 10 to the bearing arrangement 8.
  • the first line part 15 is in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 into the bottom of said at least one lubricant seal chamber 10, and the second line part 16 is in fluid connection with a top of said at least one lubricant seal chamber 10 and in fluid connection with the bearing arrangement 8, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the top of said at least one lubricant seal chamber 10 into the bearing arrangement 8.
  • the first line part 15 is in fluid connection with a bottom of the bearing arrangement, and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the bottom of the bearing arrangement 8 into the bottom of said at least one lubricant seal chamber 10, and the second line part 16 is in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12.
  • the arrangement comprises preferably, but not necessarily, a throttle means 18 provided in the first line part 15, which throttle means 18 is configured to regulate the flow of lubricant in the first line part 15.
  • a throttle means 18 can another type of flow regulating means be used.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Sealing Of Bearings (AREA)
  • Sealing Devices (AREA)
  • Rolling Contact Bearings (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Sealing With Elastic Sealing Lips (AREA)

Abstract

Presented is a method and an arrangement for sealing a propeller shaft (1). The propeller shaft (1) is rotatably supported with a bearing arrangement (8) inside a pod (3) that is suspended at a hull (4) of the marine vessel (2). The bearing arrangement (8) comprising at least two seal rings (9) axially spaced apart from each other such that at least one lubricant seal chamber (10) is delimited. The arrangement comprises a lubrication arrangement (11) for conducting lubricant to and from said bearing arrangement (8). The lubrication arrangement comprises an additional lubrication circulation line (14) for conducting a part of said flow of lubricant to and from said at least one lubricant seal chamber (10). The lubrication arrangement being additionally configured to create a flow of lubricant in the additional lubricant circulation line (14) and in said at least one lubricant seal chamber (10).

Description

    Field
  • The invention relates to a method for sealing a propeller shaft of a marine vessel as defined in the preamble of independent claim 1, wherein the propeller shaft is arranged at a pod that is suspended at a hull of the marine vessel, wherein a propeller is attached to a driving end of the propeller shaft, wherein the driving end projects out of the pod, wherein the propeller shaft is rotatably supported with a bearing arrangement inside the pod, wherein at least two seal rings are provided axially spaced apart from each other in an axial direction of the propeller shaft and engaging the outer circumference of the propeller shaft such that at least one lubricant seal chamber is delimited between adjacent seal rings, and wherein the bearing arrangement comprises a lubrication arrangement comprising a lubricant circulation line for conducting lubricant to said bearing arrangement and for conducting lubricant from said bearing arrangement, and a lubricant circulator configured to create a flow of lubricant in the lubricant circulation line and in the bearing arrangement.
  • The invention also relates to an arrangement for sealing a propeller shaft of a marine vessel as defined in the preamble of independent claim 9 , wherein the propeller shaft is arranged at a pod that is suspended at a hull of the marine vessel, wherein a propeller is attached to a driving end of the propeller shaft, wherein the driving end projects out of the pod, wherein the propeller shaft is rotatably supported with a bearing arrangement inside the pod, wherein at least two seal rings are provided axially spaced apart from each other in an axial direction of the propeller shaft and engaging the outer circumference of the propeller shaft such that at least one lubricant seal chamber is delimited between adjacent seal rings, and wherein the arrangement comprises a lubrication arrangement comprising a lubricant circulation line for conducting lubricant to said bearing arrangement and for conducting lubricant from said bearing arrangement, and a lubricant circulator configured to create a flow of lubricant in the lubricant circulation line and in the bearing arrangement.
  • A problem with the above presented method and arrangement is the heating of the seal rings delimiting the lubricant seal chamber with leads to wear and reduced service-life of the seal rings. The seal rings are heated due to the friction between the propeller shaft and the seal rings, because the seal rings engage the outer circumference of the rotating propeller shaft.
  • Objective
  • The object of the invention is to provide a method and an arrangement for sealing a propeller shaft of a marine vessel to solve the mentioned problem.
  • Short description
  • The method is characterized by the definitions of independent claim 1.
  • Preferred embodiments of the method are defined in the dependent claims 2 to 8.
  • The arrangement is correspondingly characterized by the definitions of independent claim 9.
  • Preferred embodiments of the arrangement are defined in the dependent claims 10 to 16.
  • List of figures
  • In the following the invention will described in more detail by referring to the figures, which
    • Figure 1 illustrates a first embodiment of the arrangement,
    • Figure 2 illustrates a second embodiment of the arrangement,
    • Figure 3 illustrates a third embodiment of the arrangement,
    • Figure 4 illustrates a fourth embodiment of the arrangement, and
    • Figure 5 illustrates a fifth embodiment of the arrangement.
    Detailed description of the invention
  • First the method for sealing a propeller shaft 1 of a marine vessel 2 and some embodiments and variants of the method will be described in greater detail.
  • In the method the propeller shaft 1 is arranged at a pod 3 that is suspended at a hull 4 of the marine vessel 2.
  • The pod 3 can be fixedly suspended at the hull 4 of the marine vessel 2. It is also possible that the pod 3 is pivotable about a pivot axis (not illustrated) suspended at the hull 4 of the marine vessel 2. Inside the pod 3 can an electric motor (not illustrated) be provided for rotating the propeller shaft 1. It is also possible that the pod comprises a mechanical power transmission arrangement for rotating the propeller shaft 1 by means of a motor arranged as housed by the hull 4 of the marine vessel 1.
  • In the method a propeller 5 is attached to a driving end 6 of the propeller shaft 1, wherein the driving end 6 projects out of the pod 3. The propeller shaft 1 can additionally have a second driving end (not illustrated) that projects out of an opposite end of the pod 3 i.e. so that the propeller projects through the pod and so that a second propeller (not illustrated) is provided as the second driving end.
  • In the method the propeller shaft 1 can have a non-driving section 7 that is inside the pod 3,
  • In the method the propeller shaft 1 is rotatably supported with a bearing arrangement 8 inside the pod 3.
  • In the method at least two seal rings 9 are provided axially spaced apart from each other in an axial direction of the propeller shaft 1 and engaging the outer circumference of the propeller shaft 1 such that at least one lubricant chamber 10 is delimited between adjacent seal rings 9.
  • The propeller shaft 1 can comprise a liner 20 that at least partly forms the outermost part of the propeller shaft 1. In the figures, the liner 20 forms the outermost part of the propeller shaft 1 at least in the region of the seal rings 11.
  • In the method the bearing arrangement comprises a lubrication arrangement 11 comprising a lubricant circulation line 12 for conducting lubricant to said bearing arrangement 8 and for conducting lubricant from said bearing arrangement 8, and a lubricant circulator 13 configured to create a flow of lubricant in the lubricant circulation line 12 and in the bearing arrangement 8.
  • The method comprises providing the lubrication arrangement 11 with an additional lubrication circulation line 14 comprising a first line part 15 for conducting a part of said flow of lubricant to said at least one lubricant seal chamber 10 and comprising a second line part 16 for conducting said part of said flow of lubricant from said at least one lubricant seal chamber 10.
  • The method comprises creating a flow of lubricant in the first line part 15 and in the second line part 16 of the additional lubrication circulation line 14 and in said at least one lubricant seal chamber 10.
  • The method can comprise creating by means of the lubricant circulator 13 the flow of lubricant in the first line part 15 and in the second line part 16 of the additional lubrication circulation line 14 and in said at least one lubricant seal chamber 10.
  • It is also possible that the first line part 15 and/or the second line part 16 of the additional lubrication circulation line comprises or is provided with an additional lubricant circulator (not illustrated in the figures) configured to create the flow of lubricant in the first line part 15 and in the second line part 16 of the additional lubrication circulation line 14 and in said at least one lubricant seal chamber 10.
  • Said flow of lubricant in said at least one lubricant seal chamber 10 will lower the temperature in said at least one lubricant seal chamber 10 and consequently lower the temperature of the seal rings 9 delimiting said at least one lubricant seal chamber 10. This reduces wearing of the seal rings 9 and extends the service-life of the seal rings 9. One reason for the temperature being lower is that because the temperature of the lubricant that is circulated in said at least one lubricant seal chamber 10 is lower than the temperature resulting from the friction between the outer circumference of the rotating propeller shaft 1 and said seal rings 9, thermal energy will be conducted from the seal rings 9 to the lubricant that is circulated in said at least one lubricant seal chamber 10 and in the second line part 16 away from said at least one lubricant seal chamber 10.
  • The method can comprise connecting the first line part 15 in fluid connection with the 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10, and connecting the first line part 15 in fluid connection with said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the lubricant circulation line 12 to said at least one lubricant seal chamber 10 in the first line part 15.
  • The method can comprise connecting the first line part 15 in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10, and connecting the first line part 15 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the lubricant circulation line 12 into the bottom of said at least one lubricant seal chamber 10 in the first line part 15.
  • The method can comprise connecting the first line part 15 in fluid connection with a bottom of the bearing arrangement 8 and connecting the first line part 15 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the bottom of the bearing arrangement 8 into the bottom of said at least one lubricant seal chamber 10 in the first line part 15.
  • The method can comprise providing the second line part 16 by means an equalizing channel between said at least one lubricant seal chamber 10 and the bearing arrangement 8 and conducting said part of said flow of lubricant from said at least one lubricant seal chamber 10 to the bearing arrangement 8 in the second line part 16.
  • The method can comprise connecting the second line part 16 in fluid connection with a top of said at least one lubricant seal chamber 10 and in fluid connection with the bearing arrangement 8 and conducting said part of said flow of lubricant from the top of said at least one lubricant seal chamber 10 into the bearing arrangement 8 in the second line part 16.
  • The method can comprise connecting the second line part 16 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13 and conducting said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12 in the second line part 16.
  • The second embodiment illustrated in figure 2 comprises connecting the first line part 15 in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10, and connecting the first line part 15 in fluid connection with said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the lubricant circulation line 12 to said at least one lubricant seal chamber 10 in the first line part 15, and providing the second line part 16 by means an equalizing channel between said at least one lubricant seal chamber 10 and the bearing arrangement 8 and conducting said part of said flow of lubricant from said at least one lubricant seal chamber 10 to the bearing arrangement 8 in the second line part 16.
  • The third embodiment illustrated in figure 3 comprises connecting the first line part 15 in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10, and connecting the first line part 15 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the lubricant circulation line 12 into the bottom of said at least one lubricant seal chamber 10 in the first line part 15, and connecting the second line part 16 in fluid connection with a top of said at least one lubricant seal chamber 10 and in fluid connection with the bearing arrangement 8 and conducting said part of said flow of lubricant from the top of said at least one lubricant seal chamber 10 into the bearing arrangement 8 in the second line part 16. By adjusting the height or the second line part 16 can the pressure in said at least one lubricant seal chamber 10 be adjusted. A higher height or the second line part 16 results in a higher lubricant level and into a higher pressure in in said at least one lubricant seal chamber 10 and this seals said at least one lubricant seal chamber 10 better and prevents thus leakage. A higher pressure also extends the service-life of said at least two seal rings 9. Because said at least one lubricant seal chamber 10 will be full with lubricant, said at least two seal rings 9 will have a longer service-life.
  • The fourth embodiment illustrated in figure 4 comprises connecting the first line part 15 in fluid connection with a bottom of the bearing arrangement 8, and connecting the first line part 15 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and conducting said part of said flow of lubricant from the bottom of the bearing arrangement 8 into the bottom of said at least one lubricant seal chamber 10 in the first line part 15, and connecting the second line part 16 in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13 and conducting said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12 in the second line part 16.
  • The method comprises preferably, but not necessarily, conducting thermal energy from lubricant circulating in the lubricant circulation line 12 with a cooler 17 provided in thermal contact with the lubricant circulation line 12. This additionally promotes cooling of said at least two seal rings 9. The cooler 17 can be arranged within the pod 3 as illustrated in figures 1 to 4 or outside the pod and within the hull 4 of the marine vessel 2 as illustrated in figure 5.
  • The method comprises preferably, but not necessarily, regulating the flow of lubricant in the first line part 15 by means of a throttle means 18 provided in the first line part 15. Instead of a throttle means 18 can another type of flow regulating means be used.
  • Next the arrangement for sealing a propeller shaft 1 of a marine vessel 2 and some embodiments and variants of the method will be described in greater detail.
  • The propeller shaft 1 is arranged at a pod 3 that is suspended at a hull 4 of the marine vessel 2.
  • The pod 3 can be fixedly suspended at the hull 4 of the marine vessel 2. It is also possible that the pod 3 is pivotable about a pivot axis (not illustrated) suspended at the hull 4 of the marine vessel 2. Inside the pod 3 can an electric motor (not illustrated) be provided for rotating the propeller shaft 1. It is also possible that the pod comprises a mechanical power transmission arrangement for rotating the propeller shaft 1 by means of a motor arranged as housed by the hull 4 of the marine vessel 1.
  • A propeller 5 is attached to a driving end 6 of the propeller shaft 1, wherein the driving end 6 projects out of the pod 3. The propeller shaft 1 can have a non-driving section 7 that is inside the pod 3. The propeller shaft 1 can additionally have a second driving end (not illustrated) that projects out of an opposite end of the pod 3 i.e. so that the propeller projects through the pod and so that a second propeller (not illustrated) is provided as the second driving end.
  • The propeller shaft 1 is rotatably supported with a bearing arrangement 8 inside the pod 3.
  • At least two seal rings 9 are provided axially spaced apart from each other in an axial direction of the propeller shaft 1 and engaging the outer circumference of the propeller shaft 1 such that at least one lubricant seal chamber 10 is delimited between adjacent seal rings 9.
  • The propeller shaft 1 can comprise a liner 20 that at least partly forms the outermost part of the propeller shaft 1. In the figures, the liner 20 forms the outermost part of the propeller shaft 1 at least in the region of the seal rings 11.
  • The arrangement comprises a lubrication arrangement 11 comprising a lubricant circulation line 12 for conducting lubricant to said bearing arrangement 8 and for conducting lubricant from said bearing arrangement 8, and a lubricant circulator 13 configured to create a flow of lubricant in the lubricant circulation line 12 and in the bearing arrangement 8.
  • In the arrangement the lubrication arrangement comprises an additional lubrication circulation line 14 for conducting a part of said flow of lubricant to said at least one lubricant seal chamber 10 and for conducting said part of said flow of lubricant from said at least one lubricant seal chamber 10 and the lubrication arrangement being additionally configured to create a flow of lubricant in the additional lubricant circulation line 14 and in said at least one lubricant seal chamber 10.
  • In the arrangement the lubricant circulator 13 of the lubrication arrangement is preferably, but not necessarily, additionally configured to create the flow of lubricant in the additional lubricant circulation line 14 and in said at least one lubricant seal chamber 10.
  • In the arrangement it is also possible that the additional lubricant circulation line 14 is provided with an additional lubricant circulator (not illustrated in the figures) configured to create the flow of lubricant in the additional lubricant circulation line 14 and in said at least one lubricant seal chamber 10.
  • Said flow of lubricant in said at least one lubricant seal chamber 10 will lower the temperature in said at least one lubricant seal chamber 10 and consequently lower the temperature of the seal rings 9 delimiting said at least one lubricant seal chamber 10. This reduces wearing of the seal rings 9 and extends the service-life of the seal rings 9. One reason for the temperature being lower is that because the temperature of the lubricant that is circulated in said at least one lubricant seal chamber 10 is lower than the temperature resulting from the friction between the outer circumference of the rotating propeller shaft 1 and said seal rings 9, thermal energy will be conducted from the seal rings 9 to the lubricant that is circulated in said at least one lubricant seal chamber 10 and in the second line part 16 away from said at least one lubricant seal chamber 10..
  • In the arrangement the first line part 15 can be in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 to said at least one lubricant seal chamber 10.
  • In the arrangement the first line part 15 can be in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 into the bottom of said at least one lubricant seal chamber 10.
  • In the arrangement the first line part 15 can be in fluid connection with a bottom of the bearing arrangement, and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the bottom of the bearing arrangement 8 into the bottom of said at least one lubricant seal chamber 10.
  • In the arrangement the second line part 16 can be formed by an equalizing channel between said at least one lubricant seal chamber 10 and the bearing arrangement 8, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from said at least one lubricant seal chamber 10 to the bearing arrangement 8.
  • In the arrangement the second line part 16 can be in fluid connection with a top of said at least one lubricant seal chamber 10 and in fluid connection with the bearing arrangement 8, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the top of said at least one lubricant seal chamber 10 into the bearing arrangement 8.
  • In the arrangement the second line part 16 can be in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12.
  • In the second embodiment of the arrangement illustrated in figure 2, the first line part 15 is in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 to said at least one lubricant seal chamber 10, and the second line part 16 is formed by an equalizing channel between said at least one lubricant seal chamber 10 and the bearing arrangement 8, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from said at least one lubricant seal chamber 10 to the bearing arrangement 8.
  • In the third embodiment of the arrangement illustrated in figure 3, the first line part 15 is in fluid connection with the lubricant circulation line 12 at a point downstream of the lubricant circulator 13 and upstream of said at least one lubricant seal chamber 10 and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the lubricant circulation line 12 into the bottom of said at least one lubricant seal chamber 10, and the second line part 16 is in fluid connection with a top of said at least one lubricant seal chamber 10 and in fluid connection with the bearing arrangement 8, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the top of said at least one lubricant seal chamber 10 into the bearing arrangement 8. By adjusting the height or the second line part 16 can the pressure in said at least one lubricant seal chamber 10 be adjusted. A higher height or the second line part 16 results in a higher lubricant level and into a higher pressure in in said at least one lubricant seal chamber 10 and this seals said at least one lubricant seal chamber 10 better and prevents thus leakage. A higher pressure also extends the service-life of said at least two seal rings 9. Because said at least one lubricant seal chamber 10 will be full with lubricant, said at least two seal rings 9 will have a longer service-life.
  • In the fourth embodiment of the arrangement illustrated in figure 4, the first line part 15 is in fluid connection with a bottom of the bearing arrangement, and in fluid connection with a bottom of said at least one lubricant seal chamber 10, wherein the first line part 15 being configured to conduct said part of said flow of lubricant from the bottom of the bearing arrangement 8 into the bottom of said at least one lubricant seal chamber 10, and the second line part 16 is in fluid connection with a bottom of said at least one lubricant seal chamber 10 and in fluid connection with the lubricant circulation line 12 at a point downstream of the bearing arrangement 8 and upstream of the lubricant circulator 13, wherein the second line part 16 being configured to conduct said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber 10 into the lubricant circulation line 12.
  • The arrangement comprises preferably, but not necessarily, a cooler 17 provided in thermal contact with the lubricant circulation line 12, which cooler 17 is configured to conduct thermal energy from lubricant circulating in the lubricant circulation line 12. This additionally promotes cooling of said at least two seal rings 9. The cooler 17 can be arranged within the pod 3 as illustrated in figures 1 to 4 or outside the pod and within the hull 4 of the marine vessel 2 as illustrated in figure 5.
  • The arrangement comprises preferably, but not necessarily, a throttle means 18 provided in the first line part 15, which throttle means 18 is configured to regulate the flow of lubricant in the first line part 15. Instead of a throttle means 18 can another type of flow regulating means be used.
  • It is apparent to a person skilled in the art that as technology advanced, the basic idea of the invention can be implemented in various ways. The invention and its embodiments are therefore not restricted to the above examples, but they may vary within the scope of the claims.

Claims (16)

  1. A method for sealing a propeller shaft (1) of a marine vessel (2),
    wherein the propeller shaft (1) is arranged at a pod (3) that is suspended at a hull (4) of the marine vessel (2),
    wherein a propeller (5) is attached to a driving end (6) of the propeller shaft (1), wherein the driving end (6) projects out of the pod (3),
    wherein the propeller shaft (1) is rotatably supported with a bearing arrangement (8) inside the pod (3),
    wherein at least two seal rings (9) are provided axially spaced apart from each other in an axial direction of the propeller shaft (1) and engaging the outer circumference of the propeller shaft (1) such that at least one lubricant seal chamber (10) is delimited between adjacent seal rings (9), and
    wherein the bearing arrangement (8) comprises a lubrication arrangement (11) comprising a lubricant circulation line (12) for conducting lubricant to said bearing arrangement (8) and for conducting lubricant from said bearing arrangement (8), and a lubricant circulator (13) configured to create a flow of lubricant in the lubricant circulation line (12) and in the bearing arrangement (8),
    characterized
    by providing the lubrication arrangement (11) with an additional lubrication circulation line (14) comprising a first line part (15) for conducting a part of said flow of lubricant to said at least one lubricant seal chamber (10) and comprising a second line part (16) for conducting said part of said flow of lubricant from said at least one lubricant seal chamber (10), and
    by creating a flow of lubricant in the first line part (15) and in the second line part (16) of the additional lubricant circulation line (14) and in said at least one lubricant seal chamber (10).
  2. The method according to claim 1, characterized
    by creating the flow of lubricant in the first line part (15) and in the second line part (16) of the additional lubricant circulation line (14) and in said at least one lubricant seal chamber (10) by means of the lubricant circulator (13).
  3. The method according to claim 1 or 2, characterized
    by connecting the first line part (15) in fluid connection with the lubricant circulation line (12) at a point downstream of the lubricant circulator (13) and upstream of said at least one lubricant seal chamber (10), and connecting the first line part (15) in fluid connection with said at least one lubricant seal chamber (10), and
    by conducting said part of said flow of lubricant from the lubricant circulation line (12) to said at least one lubricant seal chamber (10) in the first line part (15).
  4. The method according to claim 1 or 2, characterized
    by connecting the first line part (15) in fluid connection with the lubricant circulation line (12) at a point downstream of the lubricant circulator (13) and upstream of said at least one lubricant seal chamber (10), and connecting the first line part (15) in fluid connection with a bottom of said at least one lubricant seal chamber (10), and
    by conducting said part of said flow of lubricant from the lubricant circulation line (12) into the bottom of said at least one lubricant seal chamber (10) in the first line part (15).
  5. The method according to claim 1 or 2, characterized
    by connecting the first line part (15) in fluid connection with a bottom of the bearing arrangement (8), and connecting the first line part (15) in fluid connection with a bottom of said at least one lubricant seal chamber (10), and
    by conducting said part of said flow of lubricant from the bottom of the bearing arrangement (8) into the bottom of said at least one lubricant seal chamber (10) in the first line part (15).
  6. The method according to any of the claims 1 to 5, characterized
    by providing the second line part (16) by means an equalizing channel between said at least one lubricant seal chamber (10) and the bearing arrangement (8), and
    by conducting said part of said flow of lubricant from said at least one lubricant seal chamber (10) to the bearing arrangement (8) in the second line part (16).
  7. The method according to any of the claims 1 to 5, characterized
    by connecting the second line part (16) in fluid connection with a top of said at least one lubricant seal chamber (10) and in fluid connection with the bearing arrangement (8), and
    by conducting said part of said flow of lubricant from the top of said at least one lubricant seal chamber (10) into the bearing arrangement (8) in the second line part (16).
  8. The method according to any of the claims 1 to 5, characterized
    by connecting the second line part (16) in fluid connection with a bottom of said at least one lubricant seal chamber (10) and in fluid connection with the lubricant circulation line (12) at a point downstream of the bearing arrangement (8) and upstream of the lubricant circulator (13), and
    by conducting said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber (10) into the lubricant circulation line (12) in the second line part (16).
    line part (15) by means of a throttle means (18) provided in the first line part (15).
  9. An arrangement for sealing a propeller shaft (1) of a marine vessel (2),
    wherein the propeller shaft (1) is arranged at a pod (3) that is suspended at a hull (4) of the marine vessel (2),
    wherein a propeller (5) is attached to a driving end (6) of the propeller shaft (1), wherein the driving end (6) projects out of the pod (3),
    wherein the propeller shaft (1) is rotatably supported with a bearing arrangement (8) inside the pod (3),
    wherein at least two seal rings (9) are provided axially spaced apart from each other in the axial direction of the propeller shaft (1) and engaging the outer circumference of the propeller shaft (1) such that at least one lubricant seal chamber (10) is delimited between adjacent seal rings (9), and
    wherein the bearing arrangement (8) comprises a lubrication arrangement (11) comprising a lubricant circulation line (12) for conducting lubricant to said bearing arrangement (8) and for conducting lubricant from said bearing arrangement (8), and a lubricant circulator (13) configured to create a flow of lubricant in the lubricant circulation line (12) and in the bearing arrangement (8),
    characterized
    by the lubrication arrangement comprises an additional lubrication circulation line (14) for conducting a part of said flow of lubricant to said at least one lubricant seal chamber (10) and for conducting said part of said flow of lubricant from said at least one lubricant seal chamber (10), and
    by the lubrication arrangement being additionally configured to create a flow of lubricant in the additional lubricant circulation line (14) and in said at least one lubricant seal chamber (10).
  10. The arrangement according to claim 9, characterized
    by the lubricant circulator (13) of the lubrication arrangement being additionally configured to create a flow of lubricant in the additional lubricant circulation line (14) and in said at least one lubricant seal chamber (10).
  11. The arrangement according to claim 9 or 10, characterized
    by the first line part (15) being in fluid connection with the lubricant circulation line (12) at a point downstream of the lubricant circulator (13) and upstream of said at least one lubricant seal chamber (10) and in fluid connection with said at least one lubricant seal chamber (10), wherein the first line part (15) being configured to conduct said part of said flow of lubricant from the lubricant circulation line (12) to said at least one lubricant seal chamber (10).
  12. The arrangement according to claim 9 or 10, characterized
    by the first line part (15) being in fluid connection with the lubricant circulation line (12) at a point downstream of the lubricant circulator (13) and upstream of said at least one lubricant seal chamber (10) and in fluid connection with a bottom of said at least one lubricant seal chamber (10), wherein the first line part (15) being configured to conduct said part of said flow of lubricant from the lubricant circulation line (12) into the bottom of said at least one lubricant seal chamber (10).
  13. The arrangement according to claim 9 or 10, characterized
    by the first line part (15) being in fluid connection with a bottom of the bearing arrangement, and in fluid connection with a bottom of said at least one lubricant seal chamber (10), wherein the first line part (15) being configured to conduct said part of said flow of lubricant from the bottom of the bearing arrangement (8) into the bottom of said at least one lubricant seal chamber (10).
  14. The arrangement according to any of the claims 9 to 13, characterized
    by the second line part (16) being formed by an equalizing channel between said at least one lubricant seal chamber (10) and the bearing arrangement (8), wherein the first line part (15) being configured to conduct said part of said flow of lubricant from said at least one lubricant seal chamber (10) to the bearing arrangement (8).
  15. The arrangement according to any of the claims 9 to 13, characterized
    by the second line part (16) being in fluid connection with a top of said at least one lubricant seal chamber (10) and in fluid connection with the bearing arrangement (8), wherein the second line part (16) being configured to conduct said part of said flow of lubricant from the top of said at least one lubricant seal chamber (10) into the bearing arrangement (8).
  16. The arrangement according to any of the claims 9 to 13, characterized
    by the second line part (16) being in fluid connection with a bottom of said at least one lubricant seal chamber (10) and in fluid connection with the lubricant circulation line (12) at a point downstream of the bearing arrangement (8) and upstream of the lubricant circulator (13), wherein the second line part (16) being configured to conduct said part of said flow of lubricant from the bottom of said at least one lubricant seal chamber (10) into the lubricant circulation line (12).
EP24151399.3A 2024-01-11 2024-01-11 Method and arrangement for sealing a propeller shaft of a marine vessel Pending EP4585504A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP24151399.3A EP4585504A1 (en) 2024-01-11 2024-01-11 Method and arrangement for sealing a propeller shaft of a marine vessel
US19/010,454 US20250229884A1 (en) 2024-01-11 2025-01-06 Method and Arrangement for Sealing a Propeller Shaft of a Marine Vessel
CA3261587A CA3261587A1 (en) 2024-01-11 2025-01-08 Method and arrangement for sealing a propeller shaft of a marine vessel
JP2025003913A JP2025109194A (en) 2024-01-11 2025-01-10 Method and apparatus for sealing a marine propeller shaft - Patents.com
CN202510043943.0A CN120288226A (en) 2024-01-11 2025-01-10 Method and device for sealing a propeller shaft of a vessel
KR1020250003865A KR20250110160A (en) 2024-01-11 2025-01-10 Method and arrangement for sealing a propeller shaft of a marine vessel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP24151399.3A EP4585504A1 (en) 2024-01-11 2024-01-11 Method and arrangement for sealing a propeller shaft of a marine vessel

Publications (1)

Publication Number Publication Date
EP4585504A1 true EP4585504A1 (en) 2025-07-16

Family

ID=89619176

Family Applications (1)

Application Number Title Priority Date Filing Date
EP24151399.3A Pending EP4585504A1 (en) 2024-01-11 2024-01-11 Method and arrangement for sealing a propeller shaft of a marine vessel

Country Status (6)

Country Link
US (1) US20250229884A1 (en)
EP (1) EP4585504A1 (en)
JP (1) JP2025109194A (en)
KR (1) KR20250110160A (en)
CN (1) CN120288226A (en)
CA (1) CA3261587A1 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62181998A (en) * 1986-02-07 1987-08-10 Eagle Ind Co Ltd Method for feeding lubricating oil to stern tube
JPS62268798A (en) * 1986-05-15 1987-11-21 Mitsubishi Heavy Ind Ltd Bearing lubrication device for ship's contra-rotating propeller
JP2006234101A (en) * 2005-02-25 2006-09-07 Nippon Marine Techno Kk Shaft seal device for marine propulsion shaft
CN109027654A (en) * 2018-09-11 2018-12-18 上海和创船舶工程有限公司 A kind of tail pipe oil system applied to polar region ship

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2550929Y2 (en) * 1990-05-02 1997-10-15 日本マリンテクノ株式会社 Stern tube sealing device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62181998A (en) * 1986-02-07 1987-08-10 Eagle Ind Co Ltd Method for feeding lubricating oil to stern tube
JPS62268798A (en) * 1986-05-15 1987-11-21 Mitsubishi Heavy Ind Ltd Bearing lubrication device for ship's contra-rotating propeller
JP2006234101A (en) * 2005-02-25 2006-09-07 Nippon Marine Techno Kk Shaft seal device for marine propulsion shaft
CN109027654A (en) * 2018-09-11 2018-12-18 上海和创船舶工程有限公司 A kind of tail pipe oil system applied to polar region ship

Also Published As

Publication number Publication date
US20250229884A1 (en) 2025-07-17
CA3261587A1 (en) 2025-10-30
JP2025109194A (en) 2025-07-24
KR20250110160A (en) 2025-07-18
CN120288226A (en) 2025-07-11

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