EP2813421A2 - Ship propulsion system - Google Patents

Ship propulsion system Download PDF

Info

Publication number
EP2813421A2
EP2813421A2 EP14167837.5A EP14167837A EP2813421A2 EP 2813421 A2 EP2813421 A2 EP 2813421A2 EP 14167837 A EP14167837 A EP 14167837A EP 2813421 A2 EP2813421 A2 EP 2813421A2
Authority
EP
European Patent Office
Prior art keywords
valve
fluid
propeller shaft
propulsion system
ship propulsion
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.)
Withdrawn
Application number
EP14167837.5A
Other languages
German (de)
French (fr)
Other versions
EP2813421A3 (en
Inventor
Kurt Plough
Arne Flemming Pedersen
Kenneth Boesen
Mads Hvoldal
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.)
MAN Energy Solutions Filial af MAN Energy Solutions SE
Original Assignee
MAN Energy Solutions Filial af MAN Energy Solutions SE
MAN Diesel and Turbo Filial af MAN Diesel and Turbo SE
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 MAN Energy Solutions Filial af MAN Energy Solutions SE , MAN Diesel and Turbo Filial af MAN Diesel and Turbo SE filed Critical MAN Energy Solutions Filial af MAN Energy Solutions SE
Publication of EP2813421A2 publication Critical patent/EP2813421A2/en
Publication of EP2813421A3 publication Critical patent/EP2813421A3/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H3/00Propeller-blade pitch changing
    • B63H3/06Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical
    • B63H3/08Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid
    • B63H3/081Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid actuated by control element coaxial with the propeller shaft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H3/00Propeller-blade pitch changing
    • B63H3/06Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical
    • B63H3/08Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid
    • B63H2003/088Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid characterised by supply of fluid actuating medium to control element, e.g. of hydraulic fluid to actuator co-rotating with the propeller
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/02Transmitting power from propulsion power plant to propulsive elements with mechanical gearing

Definitions

  • the present invention relates to a ship propulsion system comprising a propeller arrangement having at least one adjustable propeller blade connected to a hub housing a hydraulic cylinder arrangement comprising a first pressure chamber and a second pressure chamber separated by a piston connected to and operating a regulating device for the at least one adjustable propeller blade and a propeller shaft located between the hub and a torque transmission unit where the propeller shaft comprises a valve arrangement provided with a fluid from a hydraulic power unit and having a number of valve fluid channels connected to a number of check valves for controlling a flow of fluid through a first duct to the first pressure chamber and through a second duct from the second pressure chamber or vice versa.
  • Ship propulsion systems of the above-mentioned kind are well known for adjusting propeller blades on controllable pitch propellers. It is known to arrange an oil distribution arrangement, comprising a stationary oil distribution ring and a valve box, on the input shaft side of a gearbox where an external hydraulic power unit supplies servo oil to two hydraulic inlet ports connected to the stationary oil distribution ring which encloses the valve box. Usually a number of check valves are mounted in the valve box for holding the oil pressure in the two servo oil chambers in a propeller hub to lock a piston when no change in pitch is desired. The piston is connected to and operates an adjusting device for the propeller blade.
  • An oil distribution arrangement of this type is disclosed in the Korean patent application 20120003058 .
  • a disadvantage with such a ship propulsion system is that the check valves, which regularly require service and maintenance, are difficult to access as they are located in the valve box which is enclosed by the stationary oil distribution ring and housing. This means that service and maintenance of the check valves will require much dismantling which is time-consuming and thus costly.
  • a further disadvantage relating to this oil distribution arrangement is that the rotating motion between the stationary oil distribution ring and the rotating valve box will induce some leakage between these elements.
  • the oil distribution arrangement is located between the gearbox and the engine as the space in that area is very narrow and thus difficult to access for service and maintenance.
  • valve arrangement comprises at least one check valve arranged in a valve housing being mounted on an outside surface of the propeller shaft and rotating together with the propeller shaft.
  • valve housings are located on the outside surface of the propeller shaft which is open to the environment in the engine room.
  • No cover or surrounding oil distribution ring for the valve housings is needed, thus, service and maintenance can be carried out quickly without much dismantling resulting in less downtime and reduced costs.
  • no leakage caused by such movement will occur in the arrangement.
  • valve arrangement is provided with fluid from the hydraulic power unit via a number of central fluid channels located inside the propeller shaft. This ensures that at very compact design can be obtained.
  • the check valves are arranged in at least two separate valve housings distributed on the circumference of the propeller shaft. In this way the needed amount of fluid can be directed via several check valves meaning that the size of the individual check valves may be reduced and, furthermore, in case of failure of a single check valve in a valve housing the other check valves will still be able to provide enough fluid to the pressure chambers in the hydraulic cylinder arrangement for moving the piston which adjusts the propeller blades.
  • valve housings may be fixed to the propeller shaft by any suitable means e.g. by means of welding, gluing or any kind of mechanically locking arrangements.
  • at least one valve housing is fixed to the propeller shaft by means of demountable fastening means, such as screwed connections.
  • At least one valve housing is configured as a sleeve or ring enclosing the propeller shaft.
  • a sleeve or ring may be shrink-fitted to the propeller shaft.
  • one or more valve housings may be integrated in a single sleeve.
  • the sleeve may be divided into two half sections, or more sections, for easy assembling around the propeller shaft.
  • the valve arrangement comprises an outer tube enclosing at least a portion of a inner tube device configured for axial movement and comprising a first pipe portion, an intermediate solid portion and a second pipe portion where the inner tube device is configured for directing fluid through the number of check valves to or from the hydraulic cylinder arrangement and where the first pipe portion and the second pipe portion each are provided with a radial fluid channel connected to a first intermediate fluid chamber and a second intermediate fluid chamber, respectively, provided between a portion of the outer tube and a portion of the inner tube device and where the intermediate fluid chambers are located separately from each other and connected to the number of check valves via the valve fluid channels.
  • the valve arrangement can be made very compact as the fluid from the hydraulic power unit may be supplied via a number of central fluid channels located inside the propeller shaft.
  • the first and second intermediate fluid chambers may comprise a first recess and a second recess, respectively, provided internally in the outer tube or provided on the circumference of a portion of the inner tube device.
  • sealing means configured to allow axial movements between the inner tube device and the outer tube are provided at both ends of each intermediate fluid chamber. This will effectively seal the intermediate fluid chambers from each other even when the inner tube device moves axially relative to the outer tube.
  • the sealing means are preferably also suitable for rotatable movements between the outer tube and the inner tube device.
  • the inner tube device is connected to the piston at a first end and connected to means indicating the position of the piston at a second end.
  • the means for indicating the position of the piston may in principle be constituted by any means as long as it is possible to read off the position of the piston.
  • the means comprise a ring surrounding the propeller shaft and being connected to the inner tube device via a rod through a longitudinal hole in the propeller shaft.
  • the ring interacts with feed-back means for on-line control and regulation of the position of the propeller blades.
  • each intermediate fluid chamber should preferably at least be equal to the length of the stroke of the piston to ensure that the intermediate fluid chambers at the maximum and minimum position of the piston are located within the outer tube.
  • the fluid may in principle be any kind of fluid as long as it is suitable for the hydraulic operation of the components in the ship propulsion system.
  • the fluid is an oil.
  • the engine powering the ship propulsion system may be a two-stroke internal combustion engine, e.g. a large low speed turbocharged crosshead engine, or a four-stroke internal combustion engine.
  • the engine may be connected directly to the propeller shaft or connected to the propeller shaft via a gear.
  • the in the introduction mentioned torque transmission unit is preferably the gear or the engine itself when the propeller is directly connected to the engine.
  • the valve arrangement 10 comprises an outer tube 21 arranged inside the propeller shaft 5 and enclosing a portion of an inner tube device configured for axial and rotational movement in relation to the outer tube 21 and comprising a first pipe 22 portion, an intermediate solid portion 23 and a second pipe portion 24.
  • the inner tube device is configured for directing fluid through the check valve 16 to or from the first pressure chamber 7 (see Fig. 1 ).
  • the first pipe portion 22 is provided with a first radial fluid channel 26 and the second pipe portion 24 is provided with a second radial fluid channel 25 which, respectively, are connected to a first recess 27 and a second recess 28 provided in the outer tube 21.
  • the recesses 27,28 are provided on the inside of the outer tube 21 and located separately from each other and connected to the check valve 15 via the valve fluid channels 17,18. Sealing and stearing means 29 configured to allow axial movements between the inner tube device and the outer tube 21 are provided at both ends of each recess 27, 28.
  • a directional valve on the hydraulic power unit 11 directs fluid into a first central fluid channel comprising the first pipe portion 22 so as to make the fluid flow through the first radial fluid channel 26, the first recess 27, the first valve fluid channel 17, the check valve 16, the second valve fluid channel 18, the second recess 28, the second radial fluid channel 25, the second pipe portion 24, the first duct 13 and into the first pressure chamber 7 (see Fig. 1 ) thereby moving the piston 9 axially towards the gear 4 and thus via the regulating device adjusting the pitch of the propeller blades 3.
  • the movement of the piston 9 will force an amount of fluid, equivalent to the movement of piston, to flow out of the second pressure chamber 8 and through the second duct 14, the third valve fluid channel 19, the check valve 15, the fourth valve fluid channel 20 and through a second central fluid channel 30 comprising the space between the outer circumference of the outer tube 21 and a hollow portion of the propeller shaft 5 and back to the tank of the hydraulic power unit 11.
  • the check valves 15,16 are preferably pilot controlled check valves where an increase in pressure on the engine side of a pilot controlled check valve will force a pilot opening of the check valve controlling the return flow.
  • the pilot fluid channels are not shown.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Actuator (AREA)
  • Check Valves (AREA)

Abstract

Described is a ship propulsion system (1) comprising a propeller arrangement (2) having at least one adjustable propeller blade (3) connected to a hub (6) housing a hydraulic cylinder arrangement comprising a first pressure chamber (7) and a second pressure chamber (8) separated by a piston (9) connected to and operating an regulating device for the at least one adjustable propeller blade (3) and a propeller shaft (5) located between the hub (6) and a torque transmission unit (4) where the propeller shaft (5) comprises a valve arrangement (10) provided with fluid from a hydraulic power unit (11) and having a number of valve fluid channels (17,18,19,20) connected to a number of check valves (15,16) for controlling a flow of fluid through a first duct (13) and a second duct (14) to the first pressure chamber (7) and from the second pressure chamber (7), respectively, or vice versa. The ship propulsion system is characterized in that the valve arrangement (10) comprises at least one check valve (15,16) arranged in a valve housing (12) being mounted to an outside surface of the propeller shaft (5) and rotating together with the propeller shaft (5).

Description

    FIELD OF THE INVENTION
  • The present invention relates to a ship propulsion system comprising a propeller arrangement having at least one adjustable propeller blade connected to a hub housing a hydraulic cylinder arrangement comprising a first pressure chamber and a second pressure chamber separated by a piston connected to and operating a regulating device for the at least one adjustable propeller blade and a propeller shaft located between the hub and a torque transmission unit where the propeller shaft comprises a valve arrangement provided with a fluid from a hydraulic power unit and having a number of valve fluid channels connected to a number of check valves for controlling a flow of fluid through a first duct to the first pressure chamber and through a second duct from the second pressure chamber or vice versa.
  • BACKGROUND OF THE INVENTION
  • Ship propulsion systems of the above-mentioned kind are well known for adjusting propeller blades on controllable pitch propellers. It is known to arrange an oil distribution arrangement, comprising a stationary oil distribution ring and a valve box, on the input shaft side of a gearbox where an external hydraulic power unit supplies servo oil to two hydraulic inlet ports connected to the stationary oil distribution ring which encloses the valve box. Usually a number of check valves are mounted in the valve box for holding the oil pressure in the two servo oil chambers in a propeller hub to lock a piston when no change in pitch is desired. The piston is connected to and operates an adjusting device for the propeller blade. An oil distribution arrangement of this type is disclosed in the Korean patent application 20120003058 . A disadvantage with such a ship propulsion system is that the check valves, which regularly require service and maintenance, are difficult to access as they are located in the valve box which is enclosed by the stationary oil distribution ring and housing. This means that service and maintenance of the check valves will require much dismantling which is time-consuming and thus costly. A further disadvantage relating to this oil distribution arrangement is that the rotating motion between the stationary oil distribution ring and the rotating valve box will induce some leakage between these elements. Moreover, it is disadvantageous that the oil distribution arrangement is located between the gearbox and the engine as the space in that area is very narrow and thus difficult to access for service and maintenance.
  • DISCLOSURE OF THE INVENTION
  • It is an object of the present invention to provide a ship propulsion system where the above-mentioned disadvantages are eliminated or significantly reduced.
  • This is achieved by a ship propulsion system of the kind mentioned in the introduction being characterized in that the valve arrangement comprises at least one check valve arranged in a valve housing being mounted on an outside surface of the propeller shaft and rotating together with the propeller shaft.
  • Hereby it is obtained that the check valves are easy accessible as the valve housings are located on the outside surface of the propeller shaft which is open to the environment in the engine room. No cover or surrounding oil distribution ring for the valve housings is needed, thus, service and maintenance can be carried out quickly without much dismantling resulting in less downtime and reduced costs. Moreover, as no relative rotational movement is present no leakage caused by such movement will occur in the arrangement.
  • It is preferred that the valve arrangement is provided with fluid from the hydraulic power unit via a number of central fluid channels located inside the propeller shaft. This ensures that at very compact design can be obtained.
  • Furthermore, it is preferred that the check valves are arranged in at least two separate valve housings distributed on the circumference of the propeller shaft. In this way the needed amount of fluid can be directed via several check valves meaning that the size of the individual check valves may be reduced and, furthermore, in case of failure of a single check valve in a valve housing the other check valves will still be able to provide enough fluid to the pressure chambers in the hydraulic cylinder arrangement for moving the piston which adjusts the propeller blades.
  • In principle the valve housings may be fixed to the propeller shaft by any suitable means e.g. by means of welding, gluing or any kind of mechanically locking arrangements. However, it is preferred that at least one valve housing is fixed to the propeller shaft by means of demountable fastening means, such as screwed connections. By mounting the valve housings, in which one or more check valves are arranged, with screwed connections, it will be easy to demount a valve housing when required, e.g. for maintenance.
  • In one embodiment at least one valve housing is configured as a sleeve or ring enclosing the propeller shaft. Such a sleeve or ring may be shrink-fitted to the propeller shaft. In this way one or more valve housings may be integrated in a single sleeve. The sleeve may be divided into two half sections, or more sections, for easy assembling around the propeller shaft.
  • In another embodiment the valve arrangement comprises an outer tube enclosing at least a portion of a inner tube device configured for axial movement and comprising a first pipe portion, an intermediate solid portion and a second pipe portion where the inner tube device is configured for directing fluid through the number of check valves to or from the hydraulic cylinder arrangement and where the first pipe portion and the second pipe portion each are provided with a radial fluid channel connected to a first intermediate fluid chamber and a second intermediate fluid chamber, respectively, provided between a portion of the outer tube and a portion of the inner tube device and where the intermediate fluid chambers are located separately from each other and connected to the number of check valves via the valve fluid channels. In this way the valve arrangement can be made very compact as the fluid from the hydraulic power unit may be supplied via a number of central fluid channels located inside the propeller shaft. The first and second intermediate fluid chambers may comprise a first recess and a second recess, respectively, provided internally in the outer tube or provided on the circumference of a portion of the inner tube device.
  • It is preferred that sealing means configured to allow axial movements between the inner tube device and the outer tube are provided at both ends of each intermediate fluid chamber. This will effectively seal the intermediate fluid chambers from each other even when the inner tube device moves axially relative to the outer tube. The sealing means are preferably also suitable for rotatable movements between the outer tube and the inner tube device.
  • Furthermore, it is preferred that the inner tube device is connected to the piston at a first end and connected to means indicating the position of the piston at a second end. Thereby it is obtained that an axial movement of the piston in the hydraulic cylinder arrangement will move the inner tube device the same distance as the piston is moved and when connected to means indicating the position of the piston it will be possible to read off the position of the propeller blades. The means for indicating the position of the piston may in principle be constituted by any means as long as it is possible to read off the position of the piston. However, it is preferred that the means comprise a ring surrounding the propeller shaft and being connected to the inner tube device via a rod through a longitudinal hole in the propeller shaft. Preferably, the ring interacts with feed-back means for on-line control and regulation of the position of the propeller blades.
  • The axial extend of each intermediate fluid chamber should preferably at least be equal to the length of the stroke of the piston to ensure that the intermediate fluid chambers at the maximum and minimum position of the piston are located within the outer tube.
  • The fluid may in principle be any kind of fluid as long as it is suitable for the hydraulic operation of the components in the ship propulsion system. However, it is preferred that the fluid is an oil.
  • The engine powering the ship propulsion system may be a two-stroke internal combustion engine, e.g. a large low speed turbocharged crosshead engine, or a four-stroke internal combustion engine. The engine may be connected directly to the propeller shaft or connected to the propeller shaft via a gear. The in the introduction mentioned torque transmission unit is preferably the gear or the engine itself when the propeller is directly connected to the engine.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • In the following detailed portion of the present description, the invention will be explained in more detail with reference to the exemplary embodiments shown in the drawings, in which:
    • Fig. 1 shows a ship propulsion system according to an exemplary embodiment of the invention, and
    • Fig. 2 shows a cross-sectional view of a section of the ship propulsion system according to an exemplary embodiment of the invention.
    DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
    • Fig. 1 shows a ship propulsion system 1 for adjusting propeller blades 3 on a controllable pitch propeller 2. A main engine (not shown), preferably an internal combustion engine, is connected to a gear 4 which is connected to a propeller shaft 5. The adjustable propeller blades 3 are connected to a hub 6 housing a hydraulic cylinder arrangement comprising a first pressure chamber 7 and a second pressure chamber 8 separated by a piston 9 connected to and operating a regulating device for the adjustable propeller blades 3. The propeller shaft 5 is located between the hub 6 and the gear 4 and comprises a valve arrangement 10 provided with fluid through the propeller shaft 5 from a hydraulic power unit 11. Valve housings 12 with check valves 15,16 (see Fig. 2) for controlling a fluid flowing to the first pressure chamber 7, through a first duct 13 arranged centrally inside the propeller shaft 5, and from the second pressure chamber 8 through a second duct 14, comprising the surrounding space between the first duct 13 and a hollow portion of the propeller shaft 5, or vice versa, are mounted by means of screwed connections (not shown) on the circumference of the propeller shaft 5. Thus, the valve housings 12 and the check valves 15,16 rotate with the propeller shaft 5.
    • Fig. 2 shows a cross-sectional view of a section of the ship propulsion system and it is seen that the valve arrangement 10 is provided with a number of valve fluid channels comprising a first 17, a second 18, a third 19 and a fourth valve fluid channel 20 located inside and in the propeller shaft and connected to the check valves 15,16 for controlling the fluid flow through the first duct 13 and the second duct 14 to move the piston 9 and thereby the propeller blades 3 (see fig. 1).
  • The valve arrangement 10 comprises an outer tube 21 arranged inside the propeller shaft 5 and enclosing a portion of an inner tube device configured for axial and rotational movement in relation to the outer tube 21 and comprising a first pipe 22 portion, an intermediate solid portion 23 and a second pipe portion 24. The inner tube device is configured for directing fluid through the check valve 16 to or from the first pressure chamber 7 (see Fig. 1). The first pipe portion 22 is provided with a first radial fluid channel 26 and the second pipe portion 24 is provided with a second radial fluid channel 25 which, respectively, are connected to a first recess 27 and a second recess 28 provided in the outer tube 21. The recesses 27,28 are provided on the inside of the outer tube 21 and located separately from each other and connected to the check valve 15 via the valve fluid channels 17,18. Sealing and stearing means 29 configured to allow axial movements between the inner tube device and the outer tube 21 are provided at both ends of each recess 27, 28.
  • When a certain adjustment of the propeller blades 3 is required a directional valve on the hydraulic power unit 11 (see Fig. 1) directs fluid into a first central fluid channel comprising the first pipe portion 22 so as to make the fluid flow through the first radial fluid channel 26, the first recess 27, the first valve fluid channel 17, the check valve 16, the second valve fluid channel 18, the second recess 28, the second radial fluid channel 25, the second pipe portion 24, the first duct 13 and into the first pressure chamber 7 (see Fig. 1) thereby moving the piston 9 axially towards the gear 4 and thus via the regulating device adjusting the pitch of the propeller blades 3. The movement of the piston 9 will force an amount of fluid, equivalent to the movement of piston, to flow out of the second pressure chamber 8 and through the second duct 14, the third valve fluid channel 19, the check valve 15, the fourth valve fluid channel 20 and through a second central fluid channel 30 comprising the space between the outer circumference of the outer tube 21 and a hollow portion of the propeller shaft 5 and back to the tank of the hydraulic power unit 11. When an adjustment of the propeller blades 3 in the opposite direction is required the fluid flow is reversed according to the before-mentioned sequence. The check valves 15,16 are preferably pilot controlled check valves where an increase in pressure on the engine side of a pilot controlled check valve will force a pilot opening of the check valve controlling the return flow. The pilot fluid channels are not shown.
  • The term "comprising" as used in the claims does not exclude other elements or steps. The term "a" or "an" as used in the claims does not exclude a plurality.
  • The reference signs used in the claims shall not be construed as limiting the scope.
  • Although the present invention has been described in detail for purpose of illustration, it is understood that such detail is solely for that purpose, and variations can be made therein by those skilled in the art without departing from the scope of the invention.

Claims (9)

  1. Ship propulsion system (1) comprising a propeller arrangement (2) having at least one adjustable propeller blade (3) connected to a hub (6) housing a hydraulic cylinder arrangement comprising a first pressure chamber (7) and a second pressure chamber (8) separated by a piston (9) connected to and operating a regulating device for the at least one adjustable propeller blade (3) and a propeller shaft (5) located between the hub (6) and a torque transmission unit (4) where the propeller shaft (5) comprises a valve arrangement (10) provided with a fluid from a hydraulic power unit (11) and having a number of valve fluid channels (17,18,19,20) connected to a number of check valves (15,16) for controlling a flow of fluid through a first duct (13) to the first pressure chamber (7) and through a second duct (14) from the second pressure chamber (8) or vice versa characterized in that the valve arrangement (10) comprises at least one check valve (15,16) arranged in a valve housing (12) being mounted on an outside surface of the propeller shaft (5) and rotating together with the propeller shaft (5).
  2. Ship propulsion system according to claim 1 characterized in that the valve arrangement (10) is provided with fluid from the hydraulic power unit (11) via a number of central fluid channels (22, 30) located inside the propeller shaft (5).
  3. Ship propulsion system according to claim 1 or 2 characterized in that at least two check valves (15,16) are arranged in at least two separate valve housings (12) distributed on the circumference of the propeller shaft (5).
  4. Ship propulsion system according to any preceding claim characterized in that at least one valve housing (12) is mounted on the propeller shaft (5) by means of demountable fastening means.
  5. Ship propulsion system according to claim 1 or 2 characterized in that the valve housing (12) is configured as a sleeve enclosing the propeller shaft (5).
  6. Ship propulsion system according to any preceding claim characterized in that the valve arrangement (10) comprises an outer tube (21) enclosing at least a portion of an inner tube device configured for axial movement and comprising a first pipe portion (22), an intermediate solid portion (23) and a second pipe portion (24) where the inner tube device is configured for directing fluid through the number of check valves (16) to or from the hydraulic cylinder arrangement (7,8,9) and where the first pipe portion (22) and the second pipe portion (24) each are provided with a radial fluid channel (25, 26) connected to a first intermediate fluid chamber (27) and a second intermediate fluid chamber (28), respectively, provided between a portion of the outer tube (21) and a portion of the inner tube device and where the intermediate fluid chambers (27,28) are located separately from each other and connected to the number of check valves (16) via the valve fluid channels (17,18).
  7. Ship propulsion system according to claim 6 characterized in that sealing means (29) configured to allow axial movements between the inner tube device (22,23,24) and the outer tube (21) are provided at both ends of each intermediate fluid chamber (27,28).
  8. Ship propulsion system according to claim 6 or 7 characterized in that the inner tube device (22,23,24) is connected to the piston (9) at a first end and connected to means indicating the position of the piston (9) at a second end.
  9. Ship propulsion system according to any of claims 6-8 characterized in that the axial extend of the first intermediate fluid chamber (27) and the second intermediate fluid chamber (28) at least is equal to the length of the stroke of the piston (9).
EP14167837.5A 2013-06-06 2014-05-12 Ship propulsion system Withdrawn EP2813421A3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DK201300349A DK177923B1 (en) 2013-06-06 2013-06-06 Valve arrangement for a propeller shaft

Publications (2)

Publication Number Publication Date
EP2813421A2 true EP2813421A2 (en) 2014-12-17
EP2813421A3 EP2813421A3 (en) 2016-03-23

Family

ID=50678108

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14167837.5A Withdrawn EP2813421A3 (en) 2013-06-06 2014-05-12 Ship propulsion system

Country Status (5)

Country Link
EP (1) EP2813421A3 (en)
JP (1) JP5646101B2 (en)
KR (1) KR101462457B1 (en)
CN (1) CN104229110A (en)
DK (1) DK177923B1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL3265380T3 (en) * 2015-03-05 2019-10-31 Waertsilae Netherlands B V A method of arranging the lubrication of a controllable pitch propeller arrangement of a marine vessel and a lubrication arrangement therefor
WO2018094575A1 (en) * 2016-11-22 2018-05-31 王金宏 Variable-pitch propeller device
CN109050787B (en) * 2018-06-29 2019-10-25 武汉船用机械有限责任公司 The method for maintaining of tuning for Controllable Pitch Propeller shafting inner hole oil pipe
CN110307320A (en) * 2019-06-03 2019-10-08 金少志 A kind of static pressure engine device
CN113277053B (en) * 2021-04-30 2022-03-25 大连海事大学 Marine air pressure drive rim propeller
CN113120204B (en) * 2021-04-30 2022-03-08 大连海事大学 Marine tandem propeller
CN113086146B (en) * 2021-04-30 2022-03-01 大连海事大学 Contra-rotating rim propeller

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120003058A (en) 2010-07-02 2012-01-10 현대중공업 주식회사 Hydraulic supply apparatus of controllable pitch propulsion system

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL294348A (en) *
US735191A (en) * 1903-03-07 1903-08-04 Rudolf Allert Grease-separator.
GB828942A (en) * 1957-04-18 1960-02-24 Ernest Charles Hatcher Improvements relating to propellers or the like having variable-pitch blades
DE1506023A1 (en) * 1967-01-18 1969-10-23 Reintjes Eisenwerke Sequence control for hydraulically controlled controllable pitch propellers
SE306891B (en) * 1967-11-28 1968-12-09 Karlstad Mekaniska Ab
DD160105A1 (en) * 1980-12-23 1983-05-04 Manfred Peetz ADJUSTMENT PROPELLERS FOR SHIPS
JPS60125299U (en) * 1984-02-02 1985-08-23 三菱重工業株式会社 Marine variable pitch propeller device
SE448295B (en) * 1985-08-02 1987-02-09 Kamewa Ab MANUAL SYSTEM FOR PROPELLER WITH STELLABLE BLADES
JP3112699B2 (en) * 1991-06-03 2000-11-27 株式会社シマノ Tubular body and manufacturing method thereof
DE4345126C1 (en) * 1993-12-30 1995-05-04 Mannesmann Ag Ship's-propulsion arrangement
US5967750A (en) * 1997-10-10 1999-10-19 Elliott; Morris C. Variable pitch marine propeller
CN102224069B (en) * 2008-09-22 2014-06-25 伯格推进技术公司 An adjustable propeller arrangement and a method of distributing fluid to and/or from such an adjustable propeller arrangement
CN102730178B (en) * 2012-07-12 2015-06-17 浙江大学舟山海洋研究中心 Electric propulsion system of large self-propelling semi-submersible transport ship

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120003058A (en) 2010-07-02 2012-01-10 현대중공업 주식회사 Hydraulic supply apparatus of controllable pitch propulsion system

Also Published As

Publication number Publication date
DK201300349A1 (en) 2015-01-05
JP2014237432A (en) 2014-12-18
JP5646101B2 (en) 2014-12-24
CN104229110A (en) 2014-12-24
DK177923B1 (en) 2015-01-12
KR101462457B1 (en) 2014-11-17
EP2813421A3 (en) 2016-03-23

Similar Documents

Publication Publication Date Title
EP2813421A2 (en) Ship propulsion system
US6796120B2 (en) Electrohydraulic actuator
US11407494B2 (en) Pitch control assembly
RU2661281C2 (en) Jack supply device with the hydraulic fluid and containing the jack gas turbine engine propeller pitch control mechanism
CN102224069B (en) An adjustable propeller arrangement and a method of distributing fluid to and/or from such an adjustable propeller arrangement
US20100014976A1 (en) Propeller blade pitch control system
EP3039299B1 (en) Electro-hydraulic actuator
KR880010219A (en) Valve device with variable characteristics using hydraulic power and link motion
JP6050870B2 (en) Rotary actuator for variable shape vanes
US7658066B2 (en) Actuation device
SE446654B (en) TILT ADJUSTER SYSTEM FOR WIND TURBLE SHOOTERS
US20170167507A1 (en) Method and system for a pitch change mechanism hydraulic fluid transfer sleeve
KR101501903B1 (en) Hub assembly for controllable pitch propeller
US11015477B2 (en) Assembly for controlling variable pitch blades
US4759186A (en) Self-powered rotary actuator utilizing rotation-generated centrifugal head
US8197213B2 (en) Turboprop including a set of adjustable-pitch blades
US20140147304A1 (en) Coolant pump for a collant circuit of an internal combustion engine
US20160290460A1 (en) Hydrodynamic converter and adjustment device for a converter of this type
EP3187414B1 (en) Oil transfer assembly for supplying oil into a rotating and translating tube
EP2909084B1 (en) Propulsion system for vessels
EP3797214B1 (en) Simplified mechanism for a scotch yoke actuator
GB2523654A (en) Turbine Engine having a Pair of Propellers for an Aircraft
US3392909A (en) Vane positioning actuator
SE540991C2 (en) Pump / motor including a gear function
US9551365B2 (en) Hydraulic device of a control device, such as a blade pitch-change device

Legal Events

Date Code Title Description
17P Request for examination filed

Effective date: 20140521

AK Designated contracting states

Kind code of ref document: A2

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

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

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

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

RIC1 Information provided on ipc code assigned before grant

Ipc: B63H 3/08 20060101AFI20160212BHEP

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

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20171201