Technical Field
[0001] The present disclosure relates to an azimuth thruster for a marine vessel, and a
method for lubricating an azimuth thruster for a marine vessel.
Background
[0002] Azimuth thrusters are commonly used as propulsion devices for marine vessels. Azimuth
thrusters are at least partly arranged beneath a hull of a marine vessel and typically
comprise an upper gear unit, an azimuth unit and a lower gear unit. The upper gear
unit is connected to a horizontal drive shaft via an upper gear crown wheel and configured
to mechanically drive a vertical input shaft of the azimuth thruster. The azimuth
unit is connected to the upper gear unit via a slewing bearing. The azimuth unit has
an outer azimuth stem and an inner azimuth stem. The slewing bearing allows a relative
rotation between the outer azimuth stem and the inner azimuth stem so that the azimuth
thruster can be slewed for maneuvering the vessel. The lower gear unit includes one
or more propellers connected to the vertical input shaft for providing thrust to the
marine vessel.
[0003] Lubrication of the azimuth thruster typically is such that the slewing bearing within
the azimuth unit is immersed in lubricant to arrange a full bath lubrication, whereas
the upper gear crown wheel within the upper gear unit is splash lubricated. The splash
lubrication is arranged to reduce frictional losses due to the upper gear crown wheel
churning the lubricant.
[0004] The present disclosure is directed, at least in part, to improving or overcoming
one or more aspects of prior systems.
Summary of the Disclosure
[0005] In one aspect, the present disclosure relates to an azimuth thruster for a marine
vessel. The azimuth thruster comprises an upper gear unit configured to be connected
to a drive source. The azimuth thruster further comprises a lower gear unit configured
to be connected to a propeller. The azimuth thruster further comprises an input shaft
drivingly connecting the upper gear unit and the lower gear unit. The input shaft
includes an inner lubricant channel extending in a longitudinal direction of the input
shaft. The azimuth thruster further comprises a lubricant pump fluidly connected to
the inner lubricant channel.
[0006] In another aspect, the present disclosure relates to a method for lubricating an
azimuth thruster for a marine vessel. The method comprises providing a first lubricant
path through an input shaft drivingly connecting an upper gear unit for connecting
to a drive source, and a lower gear unit for connecting to a propeller. The first
lubricant path receives a lubricant from a lubricant pump and supplies the lubricant
to the lower gear unit.
[0007] Other features and aspects of this disclosure will be apparent from the following
description and the accompanying drawings.
Brief Description of the Drawings
[0008] The accompanying drawings, which are incorporated herein and constitute a part of
the specification, illustrate exemplary embodiments of the disclosure and, together
with the description, serve to explain the principles of the disclosure. In the drawings:
Fig. 1 shows a schematic drawing of an exemplary azimuth thruster for a marine vessel
(ship, oil rig, etc.) according to the present disclosure;
Fig. 2 shows a schematic drawing of a lubrication circuit for the azimuth thruster
of Fig. 1.
Detailed Description
[0009] The following is a detailed description of exemplary embodiments of the present disclosure.
The exemplary embodiments described therein and illustrated in the drawings are intended
to teach the principles of the present disclosure, enabling those of ordinary skill
in the art to implement and use the present disclosure in many different environments
and for many different applications. Therefore, the exemplary embodiments are not
intended to be, and should not be considered as, a limiting description of the scope
of patent protection. Rather, the scope of patent protection shall be defined by the
appended claims.
[0010] The present disclosure is based in part on the realization that a lubricant channel
extending vertically through the azimuth thruster can be integrally formed with the
input shaft that also vertically extends through the azimuth thruster. Accordingly,
a separate lubrication line can be omitted.
[0011] The present disclosure is further based in part on the realization that providing
an inner lubricant channel in the input shaft allows for lubrication directly provided
to the highly stressed components of the lower gear unit of the azimuth thruster to
improve lubrication and heat dissipation.
[0012] The present disclosure is further based in part on the realization that lubricant
directly provided to the lower gear unit can be cooled and/or filtered in advance
such that the lubricant and heat dissipation effects are particularly improved at
those components of the azimuth thrusters, which typically bear the highest loads
during operation, particularly bearings supporting the rotating shafts of the lower
gear unit.
[0013] The present disclosure is further based in part on the realization that a lubricant
channel integrally formed with or included in an outer azimuth stem of the azimuth
unit allows cooling of the lubricant in the lubricant channel. The reason is that
the outer azimuth stem includes an outer circumferential face that contacts water
in the mounted state of the azimuth thruster. The water cools the outer circumferential
face and thus the outer azimuth stem. By cooling the outer azimuth stem, lubricant
flowing through the lubricant channel integrated in the outer azimuth stem is cooled
too.
[0014] Referring now to the drawings. It should be noted that throughout the drawings, like
elements are referred to with the same reference signs.
[0015] Fig. 1 shows a schematic drawing of an exemplary azimuth thruster 100 for a marine
vessel. The azimuth thruster 100 includes an upper gear unit 102, an azimuth unit
104 and a lower gear unit 106.
[0016] The upper gear unit 102 includes a substantially horizontal drive shaft 108 for connecting
to a drive source. The drive shaft 108 terminates to an upper gear pinion wheel 110.
The upper gear pinion wheel 110 includes an upper gear pinion wheel extension 112
configured to rotatably support the horizontal drive shaft 108 within an upper gear
housing 114. The upper gear pinion wheel 110 is configured to transmit power from
the horizontal drive shaft 108 to an upper gear crown wheel 116.
[0017] The upper gear crown wheel 116 is mounted on top of a substantially vertical input
shaft 118. The vertical input shaft 118 includes an upper crown wheel shaft 120, an
intermediate shaft 122, and a lower pinion shaft 124. The upper crown wheel shaft
120 is drivably connected to the intermediate shaft 122 via a first connection 126.
The lower pinion shaft 124 is drivably connected to the intermediate shaft 122 via
a second connection 128. The first and second connections 126, 128 may be splined
connections, flexible shaft couplings and/or floating shaft couplings.
[0018] The horizontal drive shaft 108, the upper gear pinion wheel 110, the upper gear crown
wheel 116 and the upper crown wheel shaft 120 together form part of an upper gear
transmission 121.
[0019] The vertical input shaft 118 terminates to a lower gear pinion wheel 130 formed on
the lower pinion shaft 124. The lower gear pinion wheel 130 extends into the lower
gear unit 106 and transmits the power to a lower gear crown wheel 132. The lower gear
crown wheel 132 is connected to a propeller shaft 134. The propeller shaft 134 extends
substantially horizontal and is provided with a propeller 136 for providing thrust
to the azimuth thruster 100. The propeller 136 may be any type of propeller 136 known
to a person skilled in the art, for example a variable or fixed pitch propeller.
[0020] The lower gear pinion wheel 130, the lower gear crown wheel 132 and the propeller
shaft 134 together form a lower gear transmission 131 . The lower gear transmission
131 is disposed inside the lower gear unit 106.
[0021] The propeller 136 is surrounded by a nozzle 138. The nozzle 138 is fixedly connected
to the lower gear unit 106 and may be any type of nozzle known to a person skilled
in the art. The nozzle 138 is configured to increase a thrust of the propeller 136
and to protect the propeller 136 against, for example, debris. In some embodiments,
the azimuth thruster 100 may not include the nozzle 138.
[0022] For maneuvering the marine vessel, the lower gear unit 106 including the propeller
136 and the nozzle 138 need to be rotated (slewed) around the vertical input shaft
118. This means that the upper gear unit 102 needs to be stationary, e.g. non-rotatable,
whereas the lower gear unit 106 needs to be rotatable. To rotate the lower gear unit
106 relative to the upper gear unit 102 and thus about the vertical input shaft 118,
the azimuth thruster 100 includes the azimuth unit 104.
[0023] The azimuth unit 104 is connected to the upper gear unit 102 via a separation plate
140. The separation plate 140 includes an opening 142 configured to at least partially
accommodate the upper crown wheel shaft 120. Thus, the separation plate 140 at least
partially separates the azimuth unit 104 from the upper gear unit 102. An upper crown
wheel shaft housing (not shown) may be connected to the separation plate 140 and may
protrude through the opening 142 for rotatably supporting the upper crown wheel shaft
120 via suitable bearings.
[0024] The azimuth unit 104 further includes an azimuth stem 144 with an inner azimuth stem
146 and an outer azimuth stem 148. The outer azimuth stem 148 is connected to the
separation plate 140 via an outer ring body 152. The outer ring body 152 is fixedly
connected to an annular flange 150 of the outer azimuth stem 148. The outer azimuth
stem 148 includes an outer circumferential face 149 which at least partially contacts
water in a mounted state of the azimuth thruster 100. The annular flange 150 is fixedly
connected to a hull structure (foundation) of the marine vessel. Thus, the outer azimuth
stem 148 including the separation plate 140 and the upper gear unit 102 are stationary,
e.g. non-rotatable, with respect to the marine vessel.
[0025] A ring-shaped gearwheel 154 is rotatable relative to the outer ring body 152 via
a plurality of suitable bearings 153. The ring-shaped gearwheel 154 is fixedly connected
to the inner azimuth stem 146. The outer ring body 152 and the ring-shaped gearwheel
154 together form a slewing bearing 156. Specifically, the outer ring body 152 forms
an outer race of the slewing bearing 156, and the ring-shaped gearwheel 154 forms
an inner race of the slewing bearing 156. The slewing bearing 156 is configured to
allow a rotation of the inner azimuth stem 146 relative to the outer azimuth stem
148 (relative rotation between the ring-shaped gearwheel 154 and the outer ring body
152).
[0026] The ring-shaped gearwheel 154 includes teeth on an inner circumferential face. A
slewing drive including at least one drive gearwheel (both not shown) is arranged
to rotate the ring-shaped gearwheel 154. Specifically, teeth on an outer circumferential
face of the at least one drive gearwheel engage with the teeth on the inner circumferential
face of the ring-shaped gearwheel 154. Thus, the slewing drive rotates the at least
one drive gearwheel which in turn rotates the ring-shaped gearwheel 154 relative to
the outer ring body 152.
[0027] The inner azimuth stem 146 is connected at its lower part to a vertical shaft housing
158. The vertical shaft housing 158 surrounds the vertical input shaft 118 and connects
the inner azimuth stem 146 with the lower gear unit 106. The vertical shaft housing
158 is fixedly connected to a lower gear housing 159. The lower gear housing 159 surrounds
the lower gear transmission of the lower gear unit 106.
[0028] As the outer azimuth stem 148 is non-rotatably connected to the hull structure of
the marine vessel, and as the inner azimuth stem 146 is rotatably connected to the
outer azimuth stem 148 via the slewing bearing 156, the lower gear unit 106 is rotatable
relative to the upper gear unit 102 via the slewing bearing 156.
[0029] Inside the azimuth unit 104 a first lubricant compartment 160 is disposed to accommodate
lubricant for bath lubricating the slewing bearing 156. Lubricant may be any type
of lubricant known to a person skilled in the art. For example, the lubricant may
be oil.
[0030] The first lubricant compartment 160 is formed by an annular space surrounding the
vertical input shaft 118. The first lubricant compartment 160 is filled with lubricant
such that the slewing bearing 156 is immersed in lubricant for arranging a full bath
lubrication of the slewing bearing 156. For keeping the lubricant within the azimuth
stem 144, a radial shaft seal 157 is arranged between a lower end of the outer azimuth
stem 148 and a lower end of inner azimuth stem 146.
[0031] Typically, the first lubricant compartment 160 accommodates a volume of lubricant
in a range between about 0.5 m
3 and about 3 m
3, depending on the type and size of the azimuth thruster 100 and the inner azimuth
stem 146.
[0032] Inside the upper gear unit 102 a second lubricant compartment 162 is disposed. The
second lubricant compartment 162 is configured to accommodate lubricant for splash
lubricating the upper gear pinion wheel 110 and the upper gear crown wheel 116. For
this, lubricant spray nozzles (not shown) may be disposed inside the upper gear unit
102. The lubricant spray nozzles are configured to spray lubricant onto the upper
gear transmission, thereby providing a splash lubrication of the upper gear pinion
wheel 110 and the upper gear crown wheel 116. In some embodiments, for example, pinched
lubricant pipes may be used instead of lubricant spray nozzles.
[0033] The first lubricant compartment 160 disposed inside the azimuth unit 104 and the
second lubricant compartment 162 disposed inside the upper gear unit 102 are fluidly
connected via the opening 142. Thus, lubricant sprayed onto the upper gear pinion
wheel 110 and the upper gear crown wheel 116 drains from the second lubricant compartment
162 to the first lubricant compartment 160 via the opening 142. On the other hand,
lubricant accommodated in the first lubricant compartment 160 may enter the second
lubricant compartment 162 via the opening 142. Lubricant may enter the second lubricant
compartment 162, for example, during operation of the azimuth thruster 100, because
during operation of the azimuth thruster 100 lubricant expands and the space provided
in the first lubricant compartment 160 for accommodating lubricant may not be sufficient
to accommodate the expanded lubricant. Lubricant expansion is caused by heat and aeration.
Thus, during normal operation of the azimuth thruster 100 lubricant may enter the
second lubricant compartment 162 and reach at least partially the upper gear transmission,
such as the upper gear crown wheel 116.
[0034] Referring to Fig. 2, an exemplary lubricant circuit for circulating lubricant in
the azimuth thruster 100 is depicted. It should be noted that the shown lubricant
circuit is simplified for the purpose of the present disclosure.
[0035] The lubricant circuit includes a plurality of elements including an inner lubricant
channel 200, the first lubricant compartment 160, a lubricant pump 202, a lubricant
filter 204, a lubricant cooler 206, and a manifold unit 208.
[0036] The inner lubricant channel 200 extends along a longitudinal axis of the input shaft
118, particularly along an entire length of the input shaft 118. The inner lubricant
channel 200 includes an inlet 210 at an upper gear side of the input shaft 118. The
inner lubricant channel 200 includes an outlet 212 at a lower gear side of the input
shaft 118. The upper gear side of the input shaft 118 is oppositely directed to the
lower gear side of the input shaft 118. Particularly, the inlet 210 may be provided
in an end face 214 of the crown wheel 116 meshing with the upper gear pinion wheel
110 of the upper gear unit 102. The outlet 212 may be provided in an end face 216
of the gear pinion wheel 130 meshing with the lower gear crown wheel 132 of the of
lower gear unit 106.
[0037] The lubricant pump 202 is fluidly connected to the inlet 210 of the inner lubricant
channel 200 via a lubricant line 201. The lubricant pump 202 is connected to supply
a lubricant to the inlet 210 to flow through the inner lubricant channel 200 to the
outlet 212.
[0038] In some embodiments, the inlet 210 is configured as a swivel joint (pivot joint)
including an inner lubricant channel. Particularly, the inlet 210 includes two bodies.
The two bodies are connected to allow a swivel (pivot) motion between each other.
The first body is attached at an end of the lubrication line connected to the lubricant
pump 202. The first body is stationary (does not rotate) during operation. The second
body is attached at the upper gear crown wheel 116 and/or the input shaft 118. The
second body rotates together with the input shaft 118 during operation. Both the first
and the second bodies include at least one lubricant channel that together form an
inner lubricant channel through the first and second bodies of the inlet 210 to the
inner lubricant channel 200. For example, the lubricant channels may be radial lubricant
channels. An annular lubricant channel may be formed between the two bodies at an
interface region to facilitate a transition between the two bodies. Additionally,
the first and second bodies are designed such that the interface region between both
bodies is lubricated with a lubricant film at the same time as it is functioning as
a channel to direct lubricant to the inner lubricant channel 200.
[0039] Lubricant exiting the outlet 212 bathes the lower gear unit 106 (flows around the
elements of the lower gear unit 106). Here, a good lubrication is particularly required,
because the bearings and gears of the lower gear unit 106 are particularly highly
stressed during operation. The inner lubricant channel 200 allows for the supply of
filtered and/or cooled lubricant to those highly stressed components for improving
the lubrication at those components and improving heat dissipation from those components.
As a result, wear may be reduced.
[0040] The lubricant further flows through the first lubricant compartment 160, and reaches
a lubricant suction port 218. The lubricant suction port 218 is fluidly connected
to the lubricant pump 202 via a lubricant line 222. The lubricant pump 202 is configured
to draw lubricant from the first lubricant compartment 160 to circulate the lubricant
to the inlet 210 of the inner lubricant channel 200. The lubricant suction port 218
is disposed in the azimuth unit 104.
[0041] In some embodiments, the lubricant suction port 218 is disposed at an inner circumferential
face 220 (see Fig. 1) of the inner azimuth stem 146. The lubricant line 222 connected
to the lubricant suction port 218 may at least partially extend through the outer
azimuth stem 148. Since the outer circumferential face 149 of the outer azimuth stem
148 contacts (relatively cold) water in the mounted state of the azimuth thruster
100, lubricant flowing through the lubricant line 222 is cooled by heat exchange with
the water.
[0042] The lubricant filter 204 is fluidly connected to the lubricant pump 202. Particularly,
the lubricant filter 204 is fluidly interconnected between the lubricant pump 202
and the inlet 210. The lubricant filter 204 is configured to clean the lubricant flowing
therethrough, for example by filtering particles to purify the lubricant. The lubricant
filter 204 may include one or more (replaceable) filter units arranged in series and/or
in parallel.
[0043] In some embodiments, the lubricant filter 204 may be omitted. For example, in those
embodiments, worn lubricant may be replaced by new lubricant according to a predefined
service interval.
[0044] The lubricant cooler 206 is fluidly connected to the lubricant pump 202. Particularly,
the lubricant cooler 206 is fluidly interconnected between the lubricant pump 202
and the inlet 210. More particularly, the lubricant cooler 206 is fluidly interconnected
between the lubricant filter 204 and the manifold unit 208. The lubricant filter 204
is configured to cool the lubricant flowing therethrough. Cooling of the lubricant
may be necessary due to a significant heating of the lubricant, for example, in the
lower gear unit 106. The lubricant cooler 206 may include one or more (replaceable)
cooler units arranged in series and/or in parallel.
[0045] In some embodiments, the lubricant cooler 206 may be omitted. For example, in those
embodiments, the cooling effect obtained by the lubricant line 222 extending through
the outer azimuth stem 148 may provide a sufficient cooling amount.
[0046] Lubricant pumped by the lubricant pump 202 passes the lubricant filter 204 and the
lubricant cooler 206, and reaches the manifold unit 208. The manifold unit 208 is
configured to distribute the lubricant to various lubrication targets. The manifold
unit 208 may include a plurality of components for controllably distributing the lubricant
to desired target regions. Those components include, for example, control valves,
orifices, lubricant lines etc. not shown in further detail herein.
[0047] The manifold unit 208 distributes lubricant to regions of the azimuth thruster 100
in which point lubrication is used to lubricate the components. Said point lubrication
is used for components which require lubrication and which are not bath lubricated
in the first lubrication compartment 160. Those components are particularly included
in the upper gear unit 102. For example, components being lubricated by point lubrication
are bearings 224 to 226 rotatably supporting the drive shaft 108. Additionally, in
some embodiments, bearing 230 rotatably supporting the input shaft 180 at the upper
gear side thereof may be point lubricated. Additionally, in some embodiments, a meshing
region 232 of the upper gear pinion wheel 110 and the upper gear crown wheel 116 may
be point lubricated. As used herein, point lubrication may include spray lubrication.
[0048] The manifold unit 208 also distributes lubricant to the inlet 210. The lubricant
flows through the inner lubricant channel 200, reaches the lower gear unit 106, and
contributes to the bath lubrication of the lower gear unit 106 and the azimuth unit
104. It should be noted that Fig. 2 indicates a lubricant level to be below the bearing
230 of the upper gear side end of the input shaft 118, and to be above the slewing
bearing 156 of the azimuth unit 104.
[0049] The azimuth thruster 100 may further include a temperature sensor 234 for measuring
a temperature of the lubricant in the first lubricant compartment 160. A lubricant
level measuring device 236 may be disposed for measuring a lubricant level of the
lubricant in the first lubricant compartment 160. The azimuth thruster 100 may further
include service ports for draining lubricant from the first lubricant compartment
160, and further separate lubricant lines not discussed in detail herein.
Industrial Applicability
[0050] The azimuth thruster as disclosed herein provides for a method for lubricating the
azimuth thruster. A corresponding exemplary method is described in the following with
reference to Figs. 1 and 2.
[0051] The method includes providing a first lubricant path. The first lubricant path extends
through the input shaft 118. In the embodiment described with reference to Figs. 1
and 2, the first lubricant path is formed by the inner lubricant channel 200. The
first lubricant path receives a lubricant from the lubricant pump 202 and supplies
the lubricant to the lower gear unit 106.
[0052] In a further method step, a second lubricant path may be provided. The second lubricant
path may pass from the lower gear unit 106 through the shaft housing 158. In other
words, the second lubricant path may be formed by the first lubricant compartment
160. The second lubricant path receives lubricant from the first lubricant path.
[0053] In another method step, a third lubricant path may be provided. The third lubricant
path may pass through the azimuth unit 104, particularly the inner and outer azimuth
stems 146 and 148. For example, the third lubricant path may be cooled by providing
the third lubricant path in heat exchange relationship to an environment of the azimuth
unit 104. Particularly, the heat from the first lubricant path, particularly lubricant
flowing through the third lubricant path, may be dissipated by water flowing around
the outer azimuth stem 148.
[0054] As explained with reference to Fig. 2, the lubricant may be further cooled and/or
cleaned by the lubricant cooler 206 and the lubricant filter 204, respectively, before
circulating the cooled and/or cleaned lubricant back to the first lubricant path.
[0055] The method may further comprise the method step of distributing the lubricant to
the first lubricant path, and a fourth lubricant path. The fourth lubricant path may
pass at least one region to be point lubricated, for example, bearings 224-230 and
meshing regions 232. From the regions to be point lubricated, lubricant may flow along
the fourth lubricant path to the second lubricant path to join the lubricant from
the first lubricant path. Stated differently, lubricant provided to the upper gear
unit 102 (second lubricant compartment 162) may flow and fall into the first lubricant
compartment 160 due to gravity.
[0056] Terms such as "about", "around", "approximately", or "substantially" as used herein
when referring to a measurable value such as a parameter, an amount, a temporal duration,
and the like, is meant to encompass variations of ±10% or less, preferably ±5% or
less, more preferably ±1% or less, and still more preferably ±0.1% or less of and
from the specified value, insofar as such variations are appropriate to perform in
the disclosed invention. It is to be understood that the value to which the modifier
"about" refers is itself also specifically, and preferably, disclosed. The recitation
of numerical ranges by endpoints includes all numbers and fractions subsumed within
the respective ranges, as well as the recited endpoints.
[0057] Although the preferred embodiments of this invention have been described herein,
improvements and modifications may be incorporated without departing from the scope
of the following claims.
1. An azimuth thruster (100) for a marine vessel, comprising:
an upper gear unit (102) configured to be connected to a drive source;
a lower gear unit (106) configured to be connected to a propeller (136);
an input shaft (118) drivingly connecting the upper gear unit (102) and the lower
gear unit (106), the input shaft (118) including an inner lubricant channel (200)
extending in a longitudinal direction of the input shaft (118); and
a lubricant pump (202) fluidly connected to the inner lubricant channel (200).
2. The azimuth thruster (100) of claim 1, wherein the lubricant pump (202) is arranged
to provide a lubricant to the inner lubricant channel (200) such that the lubricant
flows through the inner lubricant channel (200) to the lower gear unit (106).
3. The azimuth thruster (100) of claim 1 or claim 2, wherein the inner lubricant channel
(200) includes:
an inlet (210) at an upper gear side of the input shaft (118), and/or
an outlet (212) at a lower gear side of the input shaft (118).
4. The azimuth thruster (100) of any one of the preceding claims, wherein the input shaft
(118) includes a crown wheel (116) meshing with the upper gear unit (102), and an
inlet (210) of the inner lubricant channel (200) is disposed in an end face (214)
of the crown wheel (116).
5. The azimuth thruster (100) of any one of the preceding claims, wherein the input shaft
(118) includes a gear pinion wheel (130) meshing with the lower gear unit (106), and
an outlet (212) of the inner lubricant channel (200) is disposed in an end face (216)
of the gear pinion wheel (130).
6. The azimuth thruster (100) of any one of the preceding claims, further comprising
an azimuth unit (104) for slewing the azimuth thruster (100), the azimuth unit (104)
including a lubricant suction port (218) fluidly connected to the lubricant pump (202).
7. The azimuth thruster (100) of claim 6, wherein the azimuth unit (104) includes an
inner azimuth stem (146) and an outer azimuth stem (148), and a lubricant line (222)
fluidly connected between the lubricant suction port (218) and the lubricant pump
(202) at least partially extends through the outer azimuth stem (148).
8. The azimuth thruster (100) of claim 7, wherein the outer azimuth stem (148) includes
an outer circumferential face (149) being arranged to contact water in a mounted state
of the azimuth thruster (100).
9. The azimuth thruster (100) of any one of the preceding claims, further comprising:
a lubricant filter (204) fluidly connected to the lubricant pump (202), particularly
fluidly connected between the lubricant pump (202) and an inlet (210) of the inner
lubricant channel (200), and/or
a lubricant cooler (206) fluidly connected to the lubricant pump (202), particularly
fluidly connected between the lubricant pump (202) and an inlet (210) of the inner
lubricant channel (200).
10. The azimuth thruster (100) of any one of the preceding claims, wherein the inlet (210)
is configured as a swivel joint including a lubricant channel extending therethrough.
11. A method for lubricating an azimuth thruster (100) for a marine vessel, the method
comprising:
providing a first lubricant path through an input shaft (118) drivingly connecting
an upper gear unit (102) for connecting to a drive source, and a lower gear unit (106)
for connecting to a propeller (136), the first lubricant path receiving a lubricant
from a lubricant pump (202) and supplying the lubricant to the lower gear unit (106).
12. The method of claim 11, further comprising:
providing a second lubricant path from the lower gear unit (106) through a shaft housing
(158) surrounding the input shaft (118), the second lubricant path receiving lubricant
from the first lubricant path.
13. The method of claim 11 or claim 12, further comprising:
providing a third lubricant extending through an azimuth unit (104) of the azimuth
thruster (100) to the lubricant pump (202), the third lubricant path supplying the
lubricant to the lubricant pump (202).
14. The method of any one of claims 13, further comprising:
cooling the third lubricant path by providing the third lubricant path in heat exchange
relationship to an environment of the azimuth unit (104).
15. The method of any one of claims 11 to 14, further comprising:
cleaning and/or cooling lubricant before providing the lubricant to the first lubricant
path.