The invention relates to a propulsion unit for a marine vessel. The invention also relates to a propulsion system comprising a propulsion unit, and to a marine vessel comprising a propulsion system.
The invention is not restricted to any particular type of marine vessel. Instead it may be used on any type and any size of marine vessel, in particular water surface vessels.
Propulsion units for marine vessels are known, in which the propulsion unit comprises a stationary part adapted to be mounted to a hull of the marine vessel, and a movable part comprising one or more propellers. It is also known, from WO2020083494A1, that such a propulsion unit may be adapted to receive power from two internal combustion engines. An advantage thereby is that the engine size may be reduced, which allows the use of readily available engines for relatively large power requirements.
There is nevertheless a desire to provide a manner of handling exhausts from the engines which is beneficial from a noise control point of view, and from a design and installation point of view. For example, spaces for propulsion engines in marine vessels, in particular relatively large vessels, e.g. 25-50 meter vessels, may differ in layout from one vessel to another. The exhaust system design may involve arranging for exhausts to be emitted through a transom, or a hull side, and arranging mufflers, and secure hull penetrations. The design of the exhaust systems for such relatively large vessels, which may be commercial vessels or private yachts, are guided by extensive sets of regulations. All this contributes to making the exhaust system design and installation complicated.
An object of the invention is to provide a manner of handling exhausts from the engines which is beneficial from a noise control point of view, from a design point of view, and/or from an installation point of view.
The object is reached with a method according to claim 1. Thus, the object is reached with a propulsion unit for a marine vessel,
Embodiments of the invention allow for exhausts from the engines to be released in the water carrying the vessel. Thereby, noise levels from the engines may be reduced. Also, the smell of exhaust gases may be reduced for persons on the vessel. In addition, where the one or more thrust generating devices are one or more propellers, the exhaust gases may be transported with the propeller slip stream, allowing them to be transported relatively far from the vessel before emerging to the water surface.
Further, where the engines are in the vicinity of the propulsion unit, the exhausts may travel a relatively short distance in the vessel, which allows a relative short piping arrangement for the exhausts. This reduces requirements on space, and installation time. It also reduces the complexity of the engine installation. In addition, no separate cutout in the hull is needed for guiding the exhaust gases, since the hull cutout for the propulsion unit is used also for the exhaust gases. Further, exhaust systems may be designed to fit vessels with different layout of engine rooms, which may greatly simplify the exhaust system installation process.
The propulsion unit may be a pod drive. A pod drive, exemplified below, is herein understood as a propulsion unit which extends through the bottom of the hull, e.g. as opposed through the transom. However, in some embodiments, the propulsion unit may be a stern drive.
The one or more thrust generating devices may be adapted to be in contact with the water carrying the marine vessel. The thrust provided by the one or more thrust generating devices may provide a propulsive force to the vessel. The movable part may be rotatable in relation to the stationary part around a rotation axis for adjusting the direction of the thrust in relation to the hull. Thereby, a steering action of the marine vessel may be provided.
The stationary part may be mounted to the hull in an opening in the hull. The stationary part may be flexibly mounted to the hull. For example, one or more sealing rings may be provided between the stationary part and the hull. The sealing rings may extend along a periphery of the opening in the hull through which the stationary part extends. The sealing rings may allow minor movements of the stationary part in relation to the hull. Thereby, the sealing rings may provide a flexible mounting of the stationary part. The sealing rings may also be arranged to seal between the stationary part and the hull. However, in some embodiments, the stationary part may be fixed to the hull, e.g. by bolting or adhesive.
The at least one power supply unit, from which the propulsion unit is adapted to receive power, may be said at least two internal combustion engines. Thereby, the propulsion unit is adapted to receive power from at least two power supply units. Thus, the propulsion unit may be adapted to receive power from the at least two internal combustion engines. Thereby, the propulsion unit may be a pod drive, in which a drive shaft extends through the hull to an output transmission outside of the hull, from which output transmission one or more propeller shafts extend to respective propellers. The drive shaft may be mainly perpendicular to a local extension of the hull where the propulsion unit is installed. If the hull is locally horizontal where the propulsion unit is installed, the drive shaft may be mainly vertical. The one or more propeller shafts may be mainly horizontal when the propulsion unit is installed in a vessel.
However, in some embodiments, the propulsion unit is adapted to receive electrical power from at least one power supply unit. For example, where the propulsion unit is a pod drive, the propulsion unit may comprise one or more electric motors for driving the one or more thrust generating devices. Thereby, the propulsion unit may be adapted to receive electrical power for driving the one or more electric motors. Thereby, the at least one power supply unit may be one or more electrical generators. Thereby, the at least two internal combustion engines may be arranged to drive the one or more electrical generators.
In some embodiments, the propulsion unit is adapted to receive power from a parallel hybrid drivetrain. Thereby, an electric motor may be arranged between one of, or a respective of, the engines. In some embodiments, one or both of the engines may be arranged to supply auxiliary power in the vessel,
In preferred embodiments, the propulsion unit is adapted to receive exhaust gases from two internal combustion engines. The exhaust gases may in some embodiments contain a coolant.
Preferably, the propulsion unit comprises two unit inlets each adapted to receive exhaust gases from a respective of two engines. Thereby, exhaust gases from the engines may be guided separately from the engines to the propulsion unit. This excludes mixing of the exhaust paths before they reach the propulsion unit. Thereby, a risk of exhaust gases from one of the engines being pushed into the other of the engines is reduced or eliminated. For example, where only one of the engines is operating, there may be no back pressure in the exhaust passage of the other engine. Thereby, where the exhaust passages are connected, exhausts from the one of the engines may reach the another of the engines. Thereby, damages, e.g. of an exhaust treatment system of the exhaust receiving engine, may occur. By the propulsion unit comprising two unit inlets each adapted to receive exhaust gases from a respective of two engines, the risk of such damages is reduced or eliminated. Also, this risk is reduced without the need for valves etc. in the exhaust passages. Thereby, a robust engine installation is allowed.
Preferably, the movable part comprises at least one unit outlet for releasing the exhaust gases into the water, and the propulsion unit is adapted to keep the exhaust gases separate along at least a part of the distance between the unit inlets and the unit outlet. Thereby, the exhaust gases remain separated along at least a part of the distance through the propulsion unit. Thereby, the risk of exhaust from one of the engines reaching another of the engines is further reduced. In some embodiments, there is a single unit outlet. In some embodiments, there are two unit outlets, one for each unit inlet.
Preferably, the stationary part comprises two stationary exhaust conduits each extending from a respective of the unit inlets to the movable part. Thereby, the stationary part comprises two stationary outlets adapted to deliver the exhaust gases to the movable part. Thereby, the exhaust gases are kept separate through the stationary part. Thereby, the risk of exhaust from one of the engines reaching another of the engines is further reduced.
In some embodiments, the movable part comprises two movable inlets each adapted to receive exhaust gases from a respective of the stationary outlets. Thereby, two movable exhaust conduits may be provided in the movable part. Thereby, the exhaust gases may be kept separate through the movable part. Thereby, the risk of exhaust from one of the engines reaching another of the engines is further reduced.
In some embodiments, the movable part comprises at least one movable inlet adapted to receive exhaust gases from the stationary outlets. In addition to a radial direction, the at least one movable inlet extend in a circumferential direction in relation to the rotational axis of the movable part. Similarly, in addition to a radial direction the stationary outlets extend in a circumferential direction in relation to the rotational axis. Preferably, the extension in the circumferential direction of the at least one movable inlet is larger than the extension in the circumferential direction of the stationary outlets.
Thereby, the at least one movable inlet may fully overlap the stationary outlet within an angular interval of the movable part rotation. Thereby, the transport of the exhaust gases to the movable part is secured through the angular interval. The interval may consist of two angular distances in opposite directions from the neutral position for straight forward travel. Each angular distance may be for example within 4-10 degrees.
The at least one movable inlet may extend in the circumferential direction between delimiting sidewalls of the movable part. Thereby, in the event of large steering angles, e.g. at harbor maneuvers, at least some of the exhaust gases may be emitted from the stationary part directly into the surrounding water, outside of the movable part. Even if the exhaust gases are emitted outside of the movable part, with the separation in the stationary part of the exhaust gases from the engines, the risk of exhaust gases from one of the engines reaching the other engine is nevertheless reduced or eliminated.
In some embodiments, the unit inlets, which are each adapted to receive exhaust gases from a respective of two engines, are located at separate positions in a circumferential direction in relation to the rotation axis. Thereby, where the stationary outlets are located at separate positions in a radial direction in relation to the rotation axis, a stationary wall separating the stationary exhaust conduits may be twisted along the stationary exhaust conduits.
The unit inlets and the stationary outlets may be arranged to be located behind the rotational axis in relation to a direction of straight forward travel of the vessel. Thereby, the unit inlets may be located at substantially the same radial distance from the rotational axis of the movable part. The unit inlets may be arranged to be located on opposite sides of an imaginary plane which coincides with the rotational axis and which coincides with the direction of vessel straight forward travel. The unit inlets may be located at substantially the same radial distance from the rotational axis of the movable part. Thereby, the extension of the propulsion unit in the direction of vessel straight forward travel may be kept relatively short. This is beneficial from a space saving point of view. It may also reduce the size of an opening or a cut-out in the vessel hull for the stationary part of the propulsion unit.
In addition, the stationary outlets being located at separate positions in a radial direction in relation to the rotation axis, allows the stationary outlets to extend within the same circumferential intervals. Thereby, it may be secured that exhaust gases from both engines reach the movable part within an angular interval of rotation of the movable part.
It should be noted that in alternative embodiments, the unit inlets are located at the same circumferential position, albeit at different radial distances from the rotational axis. In further embodiments, the unit inlets are located in different circumferential positions, and at different radial distances from the rotational axis.
Preferably, where the stationary part comprises a stationary wall separating the stationary exhaust conduits, the distance, at the movable part, from the rotation axis to the stationary wall is constant along the stationary wall. Thereby, the stationary wall may be curved. Thereby, where the movable part comprises two movable exhaust conduits, and the movable part comprises a movable wall separating the movable exhaust conduits, the movable wall may coincide, at the stationary part, as seen along the rotation axis, with the stationary wall. Thereby, the movable wall may be curved.
Thereby, similar to the distance from the rotation axis to the stationary wall, the distance, at the movable part, from the rotation axis to the movable wall may be constant along the movable wall. Thereby, the distance from the rotation axis to the stationary wall, and the distance from the rotation axis to the movable wall, may be the same. Thereby, it may be secured that the stationary wall and the movable wall radially overlap. Thereby, the separation of the exhaust gases at the interface between the stationary and movable parts may be secured throughout an interval of rotation of the movable part.
However, in some embodiments, the stationary wall and/or the movable wall may have a width, at the interface between the stationary and the movable parts, which is large enough to secure the separation of the exhaust gases throughout an interval of rotation of the movable part. I.e., the stationary wall and/or the movable wall may have an extension in the radial direction of the movable part, which secures an overlap between the walls throughout the interval of rotation of the movable part. For this, one or both of the walls may be widened at the interface, e.g. gradually and/or by a flange.
It is understood that the movable exhaust conduits may each extend from the stationary part towards the at least one unit outlet.
Preferably, the propulsion unit comprises a seal at an interface between the stationary part and the movable part, the seal being adapted to seal exhaust gases guided by one of the stationary exhaust conduits, and by one of the movable exhaust conduits, from exhaust gases guided by the other of the stationary exhaust conduits, and by the other of the movable exhaust conduits. Thereby, the separation of the exhaust gases at the interface between the stationary and movable parts may be further secured throughout the interval of rotation of the movable part.
In some embodiments, the movable part comprises two movable exhaust conduits, each adapted to receive exhaust gases from a respective of the stationary exhaust conduits, wherein the movable exhaust conduits terminate at a respective of two unit outlets for releasing the exhaust gases into the water. Thereby, the two unit outlets may be arranged to be distributed substantially transversally in relation to the movable part rotation axis.
The movable part rotation axis may be substantially perpendicular to the local extension of hull where the propulsion unit is installed. In some examples, the rotation axis may be mainly vertical when the propulsion unit is installed in a vessel. This may be the case if the propulsion unit is installed in a substantially horizontal bottom part of the hull. Thereby, the two unit outlets may be arranged to be distributed substantially horizontally. However, where the propulsion unit is installed in a part of the hull which is at a non-zero angle to horizontal, e.g. in a so-called deadrise of the hull, the movable part rotation axis may extend at a non-zero angle to vertical. This angle may be e.g. 0-30 degrees, or 0-22 degrees, for example about 15 degrees. Nevertheless, at such angles, the vertical overlap of the unit outlets may be small.
By the non-existing, or small, vertical overlap of the unit outlets, when the vessel is not moving, and only one of the engines is operating, the risk of exhaust gases from the operating engine entering the exhaust path of the non-operating engine, is eliminated. More specifically, in such a situation, the exhaust gases exiting any of the outlets will rise in the surround water, without passing the other of the unit outlets.
Advantageously, where the movable part comprises a movable wall separating the movable exhaust conduits, and the unit outlets are formed at least partly by the movable wall, at least a lower part of the movable wall is removable. Thereby, the unit outlets may be joined to form an opening for access to a thrust generating device drive assembly of the movable part.
The object is also reached with a propulsion system comprising a propulsion unit according to any embodiment of the invention, and two internal combustion engines, the engines both being arranged to deliver power to the propulsion unit. Thereby, the propulsion unit preferably comprises, as suggested above, two unit inlets each adapted to receive exhaust gases from a respective of two engines. However, in some embodiments, while the propulsion unit is adapted to receive exhaust gases from the engines, the exhaust passages from the engines may be arranged to bring the exhaust gases from the engines together upstream of the propulsion unit.
The object is also reached with a marine vessel comprising a propulsion system according to any embodiment of the invention.
Further advantages and advantageous features of the invention are disclosed in the following description and in the dependent claims.
With reference to the appended drawings, below follows a more detailed description of embodiments of the invention cited as examples. In the drawings:
Reference is made also to
The propulsion unit also comprises a movable part 220. The movable part is adapted to be immerged in water carrying the marine vessel. The propulsion system comprises two internal combustion engines 210a, 210b. In this embodiment, the engines form respective power supply units, adapted to deliver mechanical power to the propulsion unit 200. In this embodiment, the engines are, in relation to a direction of straight forward travel of the marine vessel, located forward and behind the propulsion unit 200.
The movable part comprises two thrust generating devices in the form of propellers 230, adapted to transform the received power into a thrust by acting on the water carrying the marine vessel. The propellers are coaxially arranged, and counter-rotating. However, the invention is equally applicable to propulsion units with a single propeller. The propellers are in this embodiment pulling propellers. However, the invention is equally applicable to propulsion units with one or more pushing propellers. It should be also be noted that the invention is equally applicable to other types of propulsion units, such as stern drives.
Reference is made also to
The stationary part 215 comprises an input transmission 2151 for transferring power from respective power supply unit output shafts 210a1, 210b1, to an intermediate drive shaft 2152 of the power unit. The power supply units 210a, 210b may be disengageably connectable to the input transmission, e.g. by means of respective disc clutches, such as e.g. dry or wet plate clutches, centrifugal clutches, overrunning clutches, and/or electromagnetic clutches. The input transmission 2151 may be provided as described in WO2020083494A1, incorporated herein by reference. Such a transmission has two output gears and two clutches for reversing the rotational direction of the intermediate drive shaft 2152. However, it should be noted that the input transmission may be provided in any suitable way. For example, reversing gears may be provided between the engines and the propulsion unit. Thereby, the input transmission may be provided with a single output gear, and no clutch.
In use, the intermediate drive shaft 2152 may be substantially perpendicular to a local extension of the hull where the propulsion unit is installed. The intermediate drive shaft 2152 extends from the stationary part 215 to into the movable part 220. The intermediate drive shaft 2152 is coaxial with the rotation axis R. The movable part 220 comprises an output transmission 2201 arranged to transfer power from the intermediate drive shaft 2152 to two final drive shafts 2301, 2302, each arranged to transfer respective portions of the power to a respective of the thrust generating devices 230. The intermediate shaft preferably comprises two shaft parts, connected with a spline sleeve (not shown).
The propulsion unit is adapted to receive exhaust gases from the engines 210a, 210b, and the movable part 220 is adapted to release the exhaust gases into the water.
Reference is made also to
As exemplified in
The stationary part 215 further comprises two stationary outlets 307, 308 adapted to deliver the exhaust gases to the movable part 220. The movable part 220 comprises two movable inlets 313, 314 each adapted to receive exhaust gases from a respective of the stationary outlets 307, 308.
As can be seen in
Reference is made also to
As can be seen in
As can be seen in
The movable part 220 comprises a unit outlet 311 for releasing the exhaust gases into the water. The unit outlet 311 is formed at a rear end of a substantially cylindrically shaped access space 2202 for reaching the propeller drive assembly of the movable part, e.g. for service or repair. The movable wall 317 terminates between the movable inlets 313, 314 and the unit outlet 311. Thus, the propulsion unit is adapted to keep the exhaust gases separate along the distance between the unit inlets 301, 302 and where the movable wall 317 terminates.
As can be seen in
The movable inlets 313, 314 extend in the circumferential direction all the way to delimiting walls of the movable part. As the rotation angle of the movable part 220 increases, the movable part is moved so as to expose the stationary outlets 307, 308 directly to the surrounding water, as illustrated by
Reference is made to
Reference is made to
A lower part 3171 of the movable wall 317 is twisted. At the unit outlets 311, 312, the movable wall 317 extends substantially in parallel with the movable part rotational axis. Thereby, as understood from
The lower part 3171 of the movable wall 317 is removable. Thereby, access can be provided to the access space 2202 for reaching the propeller drive assembly. It should be noted however, that in some embodiments, the entire movable wall is fixed to the remainder of the movable part 220. In such embodiments, the movable part may be arranged so that access to the propeller drive assembly can be provided from where the propellers are located.
It should be noted that where the propulsion unit has one or more pushing propellers, one or more unit outlets may be provided in a propeller hub. Thereby, the exhaust gases may be guided through one or more of the one or more propellers.
It is to be understood that the present invention is not limited to the embodiments described above and illustrated in the drawings; rather, the skilled person will recognize that many changes and modifications may be made within the scope of the appended claims.
For example, one or more auxiliary exhaust conduit may be provided, to guide exhaust gases from the engines to one or more auxiliary exhaust outlets. The one or more auxiliary exhaust outlets may be located in the vessel hull, e.g. above the waterline. The one or more auxiliary exhaust conduits may be used when the vessel is not moving, or moving slowly, and the engines are idling, or are running at a rotational speed slightly above idling.
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21156729 | Feb 2021 | EP | regional |
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Number | Date | Country | |
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20220258844 A1 | Aug 2022 | US |