US20150017033A1

US20150017033A1 - Ship's propulsion unit

Info

Publication number: US20150017033A1
Application number: US14/325,439
Authority: US
Inventors: Petri SÄKKINEN; Olli TOIVANEN
Original assignee: ABB Oy
Current assignee: ABB Oy
Priority date: 2013-07-09
Filing date: 2014-07-08
Publication date: 2015-01-15
Also published as: CN104369853B; EP2824806B1; CA2856000A1; EP2824806A1; BR102014016874A2; RU2573694C1; JP2015027871A; KR20150007229A; JP6516979B2; KR101715315B1; CN104369853A; AU2014203531A1; SG10201403077TA

Abstract

The disclosure relates to a ship's propulsion unit including a shell structure arranged below a hull of the ship and an electric motor for rotating a propeller. The propulsion unit can include a closed gas circulation cooling system containing gas and include a gas circulation device for circulating gas through channels in the electric motor, a closed liquid cooling system having an inner space containing liquid, and a gas-liquid-heat exchanger in fluid connection with the closed gas circulation cooling system and with the closed liquid cooling system for exchanging thermal energy between gas circulating in the closed gas circulation cooling system and liquid in the closed liquid cooling system.

Description

FIELD OF THE INVENTION

The invention relates to a ship's propulsion unit as defined in the preamble of independent claim 1.
The invention relates to ship's propulsion units such as azimuthing propulsion units as presented in U.S. Pat. No. 5,403,216.
U.S. Pat. No. 6,312,298 B1 presents in an electromotive drive system in an improved form of a propeller motor for a ship, the cooling of the motor in a simple manner is provided. For re-cooling a circulating coolant, an annular duct is provided, which is arranged inside a shaft-like supporting part on its wall. With the assistance of this supporting part, the propeller motor is arranged, gondola-like, on the lower side of the ship.
U.S. Pat. No. 6,485,339 B1 presents an electric propulsion pod for a ship having an electric propulsion pod heat rejection member. The electric propulsion pod is attached below the ship by a hollow ship access shaft. The electric propulsion pod contains an electric motor for producing a water propulsion. The electric motor generates an amount of heat that is conducted and subsequently released into the water through the electric propulsion pod and ship access shaft surfaces. The heat rejection member is fitted for increasing the conduction and subsequent release of the electric motor heat.
U.S. Pat. No. 7,186,156 B1 presents a propulsion unit for propelling a waterborne vessel includes an electric motor arranged to provide propulsion, and a housing arranged to contain the motor. The interior of the housing is maintained at an increased pressure of above roughly 2 bar to increase the cooling effect of a cooling gas maintained therein. An end region of the housing is provided with a heat exchange mechanism arranged to cool a cooling gas passing thereover. The heat exchange mechanism is associated with the housing such that, in use, water surrounding the housing absorbs heat therefrom.
WO0154973 presents a propulsion unit arrangement for a ship. The arrangement includes a motor unit comprising a motor housing which is arranged in the water and which comprises a motor and any control means related thereto, as well as a propeller which is arranged at a motor shaft. Said motor unit comprises an electrical motor for which the cooling is arranged to take place via the surface of the motor's whole circumference through the motor's casing structure directly into the water which surrounds said unit.
U.S. Pat. No. 6,231,407 presents to improve the propulsion efficiency of a ship propulsion having a housing to be arranged on the bottom of the hull in a gondola-like manner, with a synchronous motor in the housing, at propulsion powers of approximately 10 MW, the rotor of the synchronous motor is designed as a permanent-magnet rotor, and the stator of the synchronous motor is fitted into the housing in a form-fitting manner to be cooled through the housing wall. An additional cooling device in the form of a fan or a spray device may be provided for each winding overhang.
Publication WO 2012/123547 A1 relates to a ship comprising at least one electric motor for driving the ship, and a cooling device for cooling the at least one electric motor by means of at least one coolant. The invention also provides that the cooling device has a heat exchanger, which is designed for cooling the at least one coolant by means of seawater.

OBJECTIVE OF THE INVENTION

The object of the invention is to provide efficient cooling of a ship's propulsion unit.

SHORT DESCRIPTION OF THE INVENTION

The ship's propulsion unit of the invention is characterized by the definitions of independent claim 1.
Preferred embodiments of the ship's propulsion unit are defined in the dependent claims.
The propulsion unit comprises a shell structure arranged at least partly below a hull of the ship and immersible at least partly in water so that the shell structure is at least partly surrounded by water, and an electric motor for rotating a propeller outside the shell structure. The electric motor has a stator and a rotor for rotating in the stator. The electric motor is arranged in a motor housing section of the shell structure so that the stator of the electric motor is form-fitted into a cylindrical section of the motor housing section of the shell structure. The cylindrical section has a cylindrical outer surface. The shell structure includes a support section having a lower end connected to the motor housing section of the shell structure and an upper end connected to the hull of the ship.
The invention is based on using liquid in a closed liquid cooling system for transferring thermal energy from gas circulating in closed gas circulation cooling system through the electric motor to water surrounding the propulsion unit. The closed gas circulation cooling system contains gas and comprises a gas circulation means for circulating gas through channels in the electric motor. The closed liquid cooling system has an inner space containing liquid. The propulsion unit comprises a gas-liquid-heat exchanger in fluid connection with the closed gas circulation cooling system and in fluid connection with the closed liquid cooling system for exchanging thermal energy between gas circulating in the closed gas circulation cooling system and liquid in the closed liquid cooling system. In the propulsion unit, the closed gas circulation cooling system, the closed liquid cooling system, and the gas-liquid-heat exchanger are all parts of the propulsion unit.
Because the closed gas circulation cooling system, the closed liquid cooling system, and the gas-liquid-heat exchanger are all parts of the propulsion unit, installing and mounting of the propulsion unit to a ship is easy, because no cooling lines for cooling fluid such as for cooling liquid or for cooling gas for cooling the electric propeller motor is necessarily needed between the propulsion unit and the ship.
In the propulsion unit, the closed liquid cooling system, closed gas circulation cooling system, and the gas-liquid-heat exchanger are preferably, but not necessarily, arranged at least partly enclosed by the shell structure of the propulsion unit. In the propulsion unit, the closed liquid cooling system, closed gas circulation cooling system, and the gas-liquid-heat exchanger are more preferably, but not necessarily, arranged fully enclosed by the shell structure of the propulsion unit.
“Closed gas circulation cooling system” in means in this connection for example that gas such as air present in the propulsion unit, is not let into the closed gas circulation cooling system, nor is gas discharged from the closed gas circulation cooling system into the propulsion unit.
“Closed liquid cooling system” in means in this connection for example that water surrounding the propulsion unit, when the propulsion unit is at least partly immersed in water, is not let into the closed liquid cooling system, nor is liquid discharged from the closed liquid cooling system into water surrounding the propulsion unit, when the propulsion unit is at least partly immersed in water.
In the propulsion unit, the surface of the propulsion unit is more effectively used for transferring thermal energy from the electric motor to the water surrounding the propulsion unit than in a solution where the electric motor is only cooled through the motor's casing structure to the water surrounding the propulsion unit. Because the cooling is effective, a more powerful electric motor may be used in comparison to a solution where the electric motor is only cooled through the motor's casing structure to the water surrounding the propulsion unit.
In a preferred embodiment of the invention the electric motor is an induction motor. In an induction motor a significant amount of thermal energy is generated in the rotor and the propulsion unit is especially advantageous, because the propulsion unit provides for effective cooling of the rotor of the induction motor. However, the same cooling principle can be used to cool any type of electric motor, for example a permanent magnet synchronous motor.

LIST OF FIGURES

In the following the invention will described in more detail by referring to the figures, of which

FIG. 1 shows a first embodiment of the propulsion unit,

FIG. 2 the function principle of the propulsion unit shown in FIG. 1,

FIG. 3 shows the propulsion unit shown in FIG. 1 as seen from one side,

FIG. 4 shows a variant of the first embodiment shown in FIG. 1,

FIGS. 5 to 8 shows some alternative configurations of section X-X in FIGS. 1 to 3,

FIG. 9 shows the configuration of section X-X of the variant of the first embodiment shown in FIG. 4,

FIGS. 10 to 12 shows some alternative configurations of section Y-Y in FIG. 3,

FIG. 13 shows the configuration of section Y-Y of the variant of the first embodiment shown in FIG. 4,

FIG. 14 shows a second embodiment of the propulsion unit,

FIG. 15 the function principle of the propulsion unit shown in FIG. 14,

FIG. 16 shows the propulsion unit shown in FIG. 14 as seen from one side,

FIG. 17 shows a configuration of section X-X in FIGS. 14 to 17,

FIG. 18 shows a third embodiment of the propulsion unit,

FIG. 19 the function principle of the propulsion unit shown in FIG. 18,

FIG. 20 shows the propulsion unit shown in FIG. 18 as seen from one side,

FIG. 21 shows a configuration of section X-X in FIGS. 18 to 20,

FIG. 22 shows a fourth embodiment of the propulsion unit,

FIG. 23 the function principle of the propulsion unit shown in FIG. 22,

FIG. 24 shows the propulsion unit shown in FIG. 22 as seen from one side,

FIGS. 25 to 28 shows some alternative configurations of section X-X in FIGS. 22 to 24,

FIG. 29 shows a fifth embodiment of the propulsion unit,

FIG. 30 the function principle of the propulsion unit shown in FIG. 29,

FIG. 31 shows the propulsion unit shown in FIG. 29 as seen from one side,

FIGS. 32 to 35 shows some alternative configurations of section X-X in FIGS. 29 to 31,

FIG. 36 shows a sixth embodiment of the propulsion unit,

FIG. 37 the function principle of the propulsion unit shown in FIG. 36,

FIG. 38 shows the propulsion unit shown in FIG. 36 as seen from one side,

FIGS. 39 to 42 shows some alternative configurations of section X-X in FIGS. 36 to 38,

FIG. 43 shows a seventh embodiment of the propulsion unit,

FIG. 44 the function principle of the propulsion unit shown in FIG. 43,

FIG. 45 shows the propulsion unit shown in FIG. 43 as seen from one side,

FIGS. 46 to 49 shows some alternative configurations of section X-X in FIGS. 43 to 45,

FIG. 50 shows an eight embodiment of the propulsion unit,

FIG. 51 the function principle of the propulsion unit shown in FIG. 50,

FIG. 52 shows the propulsion unit shown in FIG. 50 as seen from one side,

FIGS. 53 to 55 shows some alternative configurations of section X-X in FIGS. 50 to 52,

FIG. 56 shows a ninth embodiment of the propulsion unit,

FIG. 57 the function principle of the propulsion unit shown in FIG. 56,

FIG. 58 shows the propulsion unit shown in FIG. 56 as seen from one side,

FIG. 59 shows a configuration of section X-X in FIGS. 56 to 58,

FIG. 60 shows a tenth embodiment of the propulsion unit,

FIG. 61 shows a configuration of section X-X in FIG. 60,

FIG. 62 shows an eleventh embodiment of the propulsion unit,

FIG. 63 the function principle of the propulsion unit shown in FIG. 62,

FIG. 64 shows the propulsion unit shown in FIG. 62 as seen from one side,

FIG. 65 shows a first configuration of section X-X in FIGS. 63 and 64,

FIG. 66 shows a first configuration of section Y-Y in FIGS. 63 and 64,

FIG. 67 shows a second configuration of section X-X in FIGS. 63 and 64,

FIG. 68 shows a second configuration of section Y-Y in FIGS. 63 and 64,

FIG. 69 shows a twelfth embodiment of the propulsion unit,

FIG. 70 the function principle of the propulsion unit shown in FIG. 69,

FIG. 71 is another view of the propulsion unit shown in FIG. 69, and

FIG. 72 shows a configuration of section Y-Y in FIGS. 70 and 71.

DETAILED DESCRIPTION OF THE INVENTION

In the following the ship's propulsion unit and some preferred embodiments and variants of the ship's propulsion unit will be described in greater detail.
The ship's propulsion unit (not marked with a reference numeral) such as a ship's azimuthing propulsion unit comprises a shell structure 1 arranged below a hull 2 of the ship (not marked with a reference numeral) and immersible at least partly in water (not marked with a reference numeral) so that the shell structure 1 is at least partly surrounded by water.
The propulsion unit comprises additionally an electric motor 3 for rotating a propeller 4 outside the shell structure 1. The electric motor 3 has a stator 5 and a rotor 6 for rotating in the stator 5. In the figures a propeller shaft 7 is connected to the rotor 6 for rotating with the rotor 6 as the rotor 6 rotates in the stator 5. In the figures the propeller shaft 7 is rotatable supported by means of bearing arrangements 8. In the figures the propeller 4 is attached to the propeller shaft 7.
The electric motor 3 is arranged in a motor housing section 9 of the shell structure 1 so that the stator 5 of the electric motor 3 is form-fitted into a cylindrical section 10 of the motor housing section 9 of the shell structure 1.
The cylindrical section 10 has a cylindrical outer surface 11.
The shell structure 1 includes a support section 26 having a lower end (not marked with a reference numeral) connected to the motor housing section 9 of the shell structure 1 and an upper end (not marked with a reference numeral) connected to the hull 2 of the ship. The upper end of the support section 26 may be connected to the hull 2 of the ship by means of a turning arrangement (not shown in the drawings) for turning the propulsion unit with respect to the hull 2 of the ship.
The propulsion unit comprises a closed gas circulation cooling system 12 containing gas 13 such as air and comprising a gas circulation means 14 for circulating gas 13 through channels 23 in the electric motor 3. The channels 23 through the electric motor 3 are preferably, but not necessarily, formed by at least one of channels 23 in the rotor of the electric motor 3 and a channel 23 formed by an air gap (not marked with a reference numeral) between the stator 5 and the rotor 6 of the electric motor 3. The gas circulation means can be in the form of a separate gas circulation means or arranged in connection with the propeller shaft as in the tenth embodiment of the propulsion unit shown in FIGS. 60 and 61.
The propulsion unit comprises a closed liquid cooling system 15 having an inner space (not marked with a reference numeral) containing liquid 16 such as water.
The inner space of the closed liquid cooling system 15 is preferably, but not necessarily, partly limited by the shell structure 1 of the propulsion unit so that liquid 16 in the inner space of the closed liquid cooling system 15 is in direct contact with the shell structure 1 of the propulsion unit for exchanging thermal energy between liquid 16 in the closed liquid cooling system 15 and water surrounding the propulsion unit via the shell structure 1 of the propulsion unit.
The propulsion unit comprises a gas-liquid-heat exchanger 17 in fluid connection with the closed gas circulation cooling system 12 and in fluid connection with the closed liquid cooling system 15 for exchanging thermal energy between gas 13 circulating in the closed gas circulation cooling system 12 and liquid 16 in the closed liquid cooling system 15 without mixing gas 13 circulating in the closed gas circulation cooling system 12 with circulating liquid 16 in the closed liquid cooling system 15 or vice versa.
The closed gas circulation cooling system 12, the closed liquid cooling system 15, and the gas-liquid-heat exchanger 17 are all parts of the propulsion unit.
The support section 26 of the shell structure 1 may be provided with an opening 18 for allowing water surrounding the propulsion unit to flow through opening 18 in the shell structure 1, when the propulsion unit is at least partly immersed in water. Such opening 18 may be closed with covering parts 36 provided with apertures 37 for enabling water surrounding the propulsion unit to enter the opening 18 via the apertures 37 and correspondingly for enabling water in the opening 18 to exit the opening via the apertures 37. It is alternatively possible that such opening 18 may be closed with covering parts 36 so that apertures 37 for enabling water surrounding the propulsion unit to enter the opening 18 via the apertures 37 and correspondingly for enabling water in the opening 18 to exit the opening via the apertures 37 is formed.
The lower end of the support section 26 of the shell structure 1 may be connected to the motor housing section 9 of the shell structure 1 so that an opening 18 is formed in the support section 26 of the shell structure 1. Such opening 18 may be closed with covering parts 36 provided with apertures 37 for enabling water surrounding the propulsion unit to enter the opening 18 via the apertures 37 and correspondingly for enabling water in the opening 18 to exit the opening via the apertures 37. It is alternatively possible that such opening 18 may be closed with covering parts 36 so that apertures 37 for enabling water surrounding the propulsion unit to enter the opening 18 via the apertures 37 and correspondingly for enabling water in the opening 18 to exit the opening via the apertures 37 is formed.
The lower end of the support section 26 of the shell structure 1 may connected to the motor housing section 9 of the shell structure 1 so that an opening 18 is formed between the support section 26 of the shell structure 1 and the motor housing section 9 of the shell structure 1 and so that a cylindrical part 19 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 forms a part of an outermost surface (not marked with a reference numeral) of the propulsion unit, as is the case in the first embodiment of the propulsion unit shown in FIGS. 1 to 13, in the second embodiment of the propulsion unit shown in FIGS. 14 to 17, and in the third embodiment of the propulsion unit shown in FIGS. 18 to 21. The outermost surface is at least partly in contact with water surrounding the propulsion unit, when the propulsion unit is at least partly immersed in water. Such opening 18 may be closed with covering parts 36 provided with apertures 37 for enabling water surrounding the propulsion unit to enter the opening 18 via the apertures 37 and correspondingly for enabling water in the opening 18 to exit the opening via the apertures 37. It is alternatively possible that such opening 18 may be closed with covering parts 36 so that apertures 37 for enabling water surrounding the propulsion unit to enter the opening 18 via the apertures 37 and correspondingly for enabling water in the opening 18 to exit the opening via the apertures 37 is formed.
Such cylindrical part 19 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 may be provided with projecting heat-exchanging elements 20 for enhancing transfer of thermal energy between the electric motor 3 in the cylindrical section 10 of the motor housing section 9 and water surrounding the cylindrical part 19 of the cylindrical section 10 of the motor housing section 9, as is shown in FIG. 5.
In the propulsion unit, the closed liquid cooling system 15 may be in the form of a closed liquid tank 21 forming said inner space containing liquid 16, as is the case in the third embodiment of the propulsion unit shown in FIGS. 18 to 21, in the ninth embodiment of the propulsion unit shown in FIGS. 56 to 59, and in the tenth embodiment of the propulsion unit shown in FIGS. 60 and 61. Closed liquid tank 21 means in this context that no liquid or other fluids such as gases is during use of the closed liquid tank 21 for cooling purposes let in or let of from the closed liquid tank 21.
Such closed liquid tank 21 may be partly limited by the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 so that liquid 16 in the closed liquid tank 21 is in direct contact with the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 for exchanging thermal energy between the electrical motor arranged in the cylindrical section 10 of the motor housing section 9 and liquid 16 in the closed liquid tank 21 via the cylindrical section 10 of the motor housing section 9, as is the case in the ninth embodiment of the propulsion unit shown in FIGS. 56 to 59, and in the tenth embodiment of the propulsion unit shown in FIGS. 60 and 61.
Such closed liquid tank 21 may be partly limited by the support section 26 of the shell structure 1 of the propulsion unit so that liquid 16 in the closed liquid tank 21 is in direct contact with the support section 26 of the shell structure 1 of the propulsion unit for exchanging thermal energy between liquid 16 in the closed liquid tank 21 and water surrounding the support section 26 of the shell structure 1 of the propulsion unit via the shell structure 1 of the propulsion unit, as is the case in the third embodiment of the propulsion unit shown in FIGS. 18 to 21, in the ninth embodiment of the propulsion unit shown in FIGS. 56 to 59, and in the tenth embodiment of the propulsion unit shown in FIGS. 60 and 61.
If the closed liquid cooling system 15 is in the form of a closed liquid tank 21 forming said inner space containing liquid 16, the gas-liquid-heat exchanger 17 may be formed by ducts 22 in fluid communication with the closed gas circulation cooling system 12 so that the ducts 22 extends through the closed liquid tank 21 for leading gas 13 circulating in the closed gas circulation cooling system 12 in said ducts 22 through the closed liquid tank 21 and for exchanging thermal energy between gas 13 flowing in said ducts 22 and liquid 16 in the closed liquid tank 21, as is the case in the third embodiment of the propulsion unit shown in FIGS. 18 to 21, in the ninth embodiment of the propulsion unit shown in FIGS. 56 to 59, and in the tenth embodiment of the propulsion unit shown in FIGS. 60 and 61.
If the closed liquid cooling system 15 is in the form of a closed liquid tank 21 forming said inner space containing liquid 16, inner surface of the closed liquid tank 21 may be provided with projecting heat exchanging elements 32 projecting from the support section 26 of the shell structure 1 of the propulsion unit into the closed liquid tank for enhancing transfer of thermal energy between liquid 16 in the inner space of the closed liquid tank 21 and water surrounding the shell structure of the propulsion unit.
In the propulsion unit, the closed liquid cooling system 15 may be in the form of a closed liquid circulation cooling system 24 containing liquid 16 and forming said inner space containing liquid 16 and provided with liquid circulation means 25 for circulating liquid 16 in the inner space of the closed liquid circulation cooling system 24, as is the case in the first embodiment of the propulsion unit shown in FIGS. 1 to 13, in the second embodiment of the propulsion unit shown in FIGS. 14 to 17, in the fourth embodiment of the propulsion unit shown in FIGS. 22 to 28, in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, in the sixth embodiment of the propulsion unit shown in FIGS. 36 to 42, in the seventh embodiment of the propulsion unit shown in FIGS. 43 and 49, in the eleventh embodiment of the propulsion unit shown in FIGS. 62 to 68, and in the twelfth embodiment of the propulsion unit shown in FIGS. 69 to 72.
The closed liquid circulation cooling system 24 may be partly formed by a tube section 33 having an outer surface 34 that is in direct contact with water surrounding the propulsion unit for exchanging thermal energy between liquid 16 circulating in the closed liquid circulation cooling system 24 and water surrounding the propulsion unit via the tube section 33 of the closed liquid circulation cooling system 24, as is the case in the eleventh embodiment of the propulsion unit shown in FIGS. 62 to 68, and in the twelfth embodiment of the propulsion unit shown in FIGS. 69 to 72. The tube section 33 may include a part in the form of a coiled tube.
If the closed liquid circulation cooling system 24 is partly formed by a tube section 33, the tube section 33 may be a part of a liquid-liquid-heat exchanger 38 that is in fluid communication with the closed liquid cooling system 15 so that liquid circulating in the inner space of the closed liquid cooling system 15 circulates through the tube section 33 of the liquid-liquid-heat exchanger 38 for exchanging thermal energy between liquid flowing through the tube section 33 of the liquid-liquid-heat exchanger 38 and water in contact with the tube section 33 of the liquid-liquid-heat exchanger 38 and surrounding the shell structure 1 of the propulsion unit.
The inner space of such closed liquid circulation cooling system 24 may be partly limited by the support section 26 of the shell structure 1 of the propulsion unit so that liquid 16 flowing in the inner space of the closed liquid circulation cooling system 24 is in direct contact with the support section 26 of the shell structure 1 for exchanging thermal energy between liquid 16 flowing in the inner space of the closed liquid circulation cooling system 24 and water surrounding the support section 26 of the shell structure 1 via the support section 26 of the shell structure 1.
The inner space of such closed liquid circulation cooling system 24 may additionally be partly limited by a part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 so that liquid 16 flowing in the inner space of the closed liquid circulation cooling system 24 is in direct contact with said part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 for exchanging thermal energy between the electric motor 3 arranged in the cylindrical section 10 of the motor housing section 9 and liquid 16 flowing in the inner space of the closed liquid circulation cooling system 24 via said part 31 of the cylindrical section 10 of the motor housing section 9 between the electric motor 3 and liquid 16 circulating in the inner space of the closed liquid circulation cooling system 24, as is the case in the fourth embodiment of the propulsion unit shown in FIGS. 22 to 28, in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, in the sixth embodiment of the propulsion unit shown in FIGS. 36 to 42, in the seventh embodiment of the propulsion unit shown in FIGS. 43 to 49, and in the eight embodiment of the propulsion unit shown in FIGS. 50 to 55.
Said part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 in contact with liquid 16 in the inner space of the closed liquid circulation cooling system 24 may be provided with partition elements 27 for creating several individual flows of liquid 16 along said part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9, as is shown in FIGS. 26, 33, 40, and 47.
Said part 31 of the cylindrical section 10 of the cylindrical outer surface 11 of the motor housing section 9 in contact with liquid 16 in the closed liquid cooling system 15 may be provided with projecting heat-exchanging elements for enhancing transfer of thermal energy between the electric motor 3 in the motor housing section 9 and liquid 16 in the closed liquid cooling system 15, as is shown in FIGS. 25, 32, 39, and 46.
If the closed liquid cooling system 15 is in the form of a closed liquid circulation cooling system 24, the closed liquid circulation cooling system 24 may be provided with a first liquid tank 28, having a first inner space (not marked with a reference numeral) that forms a part 31 of the inner space of the closed liquid circulation cooling system 24, as is the case in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, in the sixth embodiment of the propulsion unit shown in FIGS. 36 to 42, and in the eight embodiment of the propulsion unit shown in FIGS. 50 to 55.
Such first liquid tank 28 is in fluid communication with the closed liquid circulation cooling system 24 such that liquid 16 flowing in the closed liquid circulation cooling system 24 flows through the first inner space of the first liquid tank 28. The first inner space of the first liquid tank 28 is partly limited by said part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 so that liquid 16 in a first inner space of the first liquid tank 28 is in direct contact with the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 for exchanging thermal energy between the electric motor 3 arranged in the motor housing section 9 and liquid 16 flowing in the first inner space of the first liquid tank 28 via said part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9.
If the closed liquid circulation cooling system 24 is provided with a first liquid tank 28, the first liquid tank 28 may be additionally partly limited by the support section 26 of the shell structure 1 so that liquid 16 in the first inner space of the first liquid tank 28 is additionally in direct contact with the support section 26 of the shell structure 1 for exchanging thermal energy between liquid 16 flowing in the first inner space of the first liquid tank 28 of the closed liquid circulation cooling system 24 and water surrounding the support section 26 of the shell structure 1 via the support section 26 of the shell structure 1, as is the case in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, in the sixth embodiment of the propulsion unit shown in FIGS. 36 to 42, and in the eight embodiment of the propulsion unit shown in FIGS. 50 to 55.
If the closed liquid circulation cooling system 24 is provided with a first liquid tank 28, the first liquid tank 28 being provided with baffles 29 for guiding liquid 16 through the first liquid tank 28 to prolong the residence time of liquid 16 in the first liquid tank 28 and/or for serving as heat exchanging elements between liquid 16 flowing through the first liquid tank 28 and the support section 26 of the shell structure 1, as is the case in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, and in the sixth embodiment of the propulsion unit shown in FIGS. 36 to 42.
If the closed liquid circulation cooling system 24 is provided with a first liquid tank 28, the gas-liquid-heat exchanger 17 can be formed by ducts 22 in fluid communication with the closed gas circulation cooling system 12, wherein the ducts 22 extends through the first liquid tank 28 for leading gas 13 circulating in the closed gas circulation cooling system 12 in said ducts 22 through the first liquid tank 28 and for exchanging thermal energy between gas 13 flowing in said ducts 22 through the first liquid tank 28 and liquid 16 in the first liquid tank 28, as in the eight embodiment of the propulsion unit shown in FIGS. 50 to 55.
If the closed liquid cooling system 15 is in the form of a closed liquid circulation cooling system 24, the closed liquid circulation cooling system 24 may be provided with a second liquid tank 30 having a second inner space (not marked with a reference numeral) that forms a part of the inner space of the closed liquid circulation cooling system 24, as is the case in the first embodiment of the propulsion unit shown in FIGS. 1 to 13, in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, and in the seventh embodiment of the propulsion unit shown in FIGS. 43 to 49.
Such second liquid tank 30 is in fluid communication with the closed liquid circulation cooling system 24 such that liquid 16 flowing in the closed liquid circulation cooling system 24 flows through the second inner space of the second liquid tank 30. The second liquid tank 30 being partly limited by the support section 26 of the shell structure 1 so that liquid 16 in the second inner space (not marked with a reference numeral) of the second liquid tank 30 is in direct contact with the support section 26 of the shell structure 1 for exchanging thermal energy between liquid 16 flowing in the second inner space of the second liquid tank 30 and water surrounding the support section 26 of the shell structure 1 via the support section 26 of the shell structure 1.
If the closed liquid circulation cooling system 24 is provided with a second liquid tank 30, the second inner space of the second liquid tank 30 may be provided with baffles 29 for guiding liquid 16 through the second inner space of the second liquid tank 30 to prolong the residence time of liquid 16 in the second inner space of the second liquid tank 30 and/or for serving as heat exchanging elements between liquid 16 flowing through the second inner space of the second liquid tank 30 and the support section 26 of the shell structure 1, as is the case in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, and in the seventh embodiment of the propulsion unit shown in FIGS. 43 to 49.
If the closed liquid circulation cooling system 24 is provided with a second liquid tank 30, the gas-liquid-heat exchanger 17 can be formed by ducts 22 in fluid communication with the closed gas circulation cooling system 12, wherein the ducts 22 extends through the second liquid tank 30 for leading gas 13 circulating in the closed gas circulation cooling system 12 in said ducts 22 through the second liquid tank 30 and for exchanging thermal energy between gas 13 flowing in said ducts 22 through the second liquid tank 30 and liquid 16 in the second liquid tank 30 as in the second embodiment of the propulsion unit shown in FIGS. 14 to 17.
In the propulsion unit the lower end of the support section 26 of the shell structure 1 may be connected to the motor housing section 9 of the shell structure 1 so that the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 of the shell structure 1 of the propulsion unit partly forms the outermost surface of the propulsion unit, as is shown in the figures. In such case the part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 forming the outermost surface of the propulsion unit may be provided with projecting heat-exchanging elements 20 for enhancing transfer of thermal energy between the electric motor 3 in the motor housing section 9 and water surrounding the part 31 of the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 forming the outermost surface of the propulsion unit.
The gas-liquid-heat exchanger 17 can be a separate heat exchanger in fluid connection with the closed gas circulation cooling system 12 and in fluid connection with the closed liquid cooling system 15 as is the case in the first embodiment of the propulsion unit shown in FIGS. 1 to 13, in the fourth embodiment of the propulsion unit shown in FIGS. 22 to 28, in the fifth embodiment of the propulsion unit shown in FIGS. 29 to 35, in the sixth embodiment of the propulsion unit shown in FIGS. 36 to 42, and in the seventh embodiment of the propulsion unit shown in FIGS. 43 to 49.
The cylindrical section 10 of the motor housing section 9 is preferably, but not necessarily, of a single-layer construction, as is illustrated in the figures. It is however obvious for a person skilled in the art that the cylindrical outer surface 11 of the cylindrical section 10 of the motor housing section 9 can for example additionally be painted.
The closed liquid cooling system 15 is preferably, but not necessarily, arranged at least partly enclosed by the shell structure 1 of the propulsion unit. The closed liquid cooling system 15 is more preferably, but not necessarily, arranged fully enclosed by the shell structure 1 of the propulsion unit, as is illustrated in the figures.
The closed gas circulation cooling system 12 is preferably, but not necessarily, arranged at least partly enclosed by the shell structure 1 of the propulsion unit. The closed gas circulation cooling system 12 is more preferably, but not necessarily, arranged fully enclosed by the shell structure 1 of the propulsion unit, as is illustrated in the figures.
The gas-liquid-heat exchanger 17 is preferably, but not necessarily, arranged at least partly enclosed by the shell structure 1 of the propulsion unit. The gas-liquid-heat exchanger 17 is more preferably, but not necessarily, arranged fully enclosed by the shell structure 1 of the propulsion unit, as is illustrated in the figures.
The closed liquid cooling system 15 is preferably, but not necessarily, arranged fully outside the hull of the ship, as is illustrated in the figures.
The closed gas circulation cooling system 12 is preferably, but not necessarily, arranged fully outside the hull of the ship, as is illustrated in the figures.
The gas-liquid-heat exchanger 17 is preferably, but not necessarily, arranged fully outside the hull of the ship, as is illustrated in the figures.
The electric motor 3 is preferably, but not necessarily, an induction electric motor 3.
It is apparent to a person skilled in the art that as technology advances, the basic idea of the invention can be implemented in various ways. The invention and its embodiments are therefore not restricted to the above examples, but they may vary within the scope of the claims.

Claims

1. A ship propulsion unit, comprising:

a shell structure configured to be arranged below a hull of a ship and immersible at least partly in water so that the shell structure will be at least partly surrounded by water in use; and

an electric motor for rotating a propeller outside the shell structure, the electric motor having a stator and a rotor for rotating in the stator;

wherein the electric motor is arranged in a motor housing section of the shell structure so that the stator of the electric motor is form-fitted into a cylindrical section of the motor housing section of the shell structure, the cylindrical section having a cylindrical outer surface; and

wherein the shell structure includes a support section having an lower end connected to the motor housing section of the shell structure and an upper end for connection to a hull of a ship;

a closed gas circulation cooling system containing gas and having gas circulation means for circulating gas through channels in the electric motor,

a closed liquid cooling system having an inner space containing liquid; and

a gas-liquid-heat exchanger in fluid connection with the closed gas circulation cooling system and in fluid connection with the closed liquid cooling system for exchanging thermal energy between gas circulating in the closed gas circulation cooling system and liquid in the closed liquid cooling system, the closed gas circulation cooling system, the closed liquid cooling system, and the gas-liquid-heat exchanger being parts of the propulsion unit.

2. The propulsion unit according to claim 1, wherein the inner space of the closed liquid cooling system is partly limited by the shell structure of the propulsion unit so that liquid in the inner space of the closed liquid cooling system will be in direct contact with the shell structure of the propulsion unit for exchanging thermal energy between liquid in the closed liquid cooling system and water surrounding the propulsion unit via the shell structure of the propulsion unit.

3. The propulsion unit according to claim 1, wherein the lower end of the support section of the shell structure is connected to the motor housing section of the shell structure so that an opening for allowing water surrounding the propulsion unit to flow through the opening in the shell structure is formed in the support section of the shell structure.

4. The propulsion unit according to claim 3, wherein the lower end of the support section of the shell structure is connected to the motor housing section of the shell structure so that the opening in the support section of the shell structure is formed between the support section of the shell structure and the motor housing section of the shell structure, and so that a cylindrical part of the cylindrical outer surface of the cylindrical section of the motor housing section forms a part of an outermost surface of the propulsion unit, which outermost surface is configured to be at least partly in contact with water surrounding the propulsion unit.

5. The propulsion unit according to claim 1, wherein the closed liquid cooling system is a closed liquid tank forming said inner space containing liquid.

6. The propulsion unit according to claim 5, wherein the closed liquid tank is partly limited by the cylindrical outer surface of the cylindrical section of the motor housing section so that liquid in the closed liquid tank will be in direct contact with the cylindrical outer surface of the cylindrical section of the motor housing section for exchanging thermal energy between the electrical motor arranged in the cylindrical section of the motor housing section and liquid in the closed liquid tank via the cylindrical section of the motor housing section.

7. The propulsion unit according to claim 5, wherein the closed liquid tank is partly limited by the support section of the shell structure of the propulsion unit so that liquid in the closed liquid tank will be in direct contact with the support section of the shell structure of the propulsion unit for exchanging thermal energy between liquid in the closed liquid tank and water surrounding the support section of the shell structure of the propulsion unit via the shell structure of the propulsion unit.

8. The propulsion unit according to claim 1, wherein the closed liquid cooling system is a closed liquid circulation cooling system containing liquid and forming said inner space containing liquid, and is provided with liquid circulation means for circulating liquid in the inner space of the closed liquid circulation cooling system.

9. The propulsion unit according to claim 8, wherein the closed liquid circulation cooling system is partly formed by a tube section having an outer surface that is will be in direct contact with water surrounding the propulsion unit for exchanging thermal energy between liquid circulating in the closed liquid circulation cooling system and water surrounding the propulsion unit via the tube section of the closed liquid circulation cooling system.

10. The propulsion unit according to claim 9, wherein the tube section is a part of a liquid-liquid-heat exchanger that is in fluid communication with the closed liquid cooling system so that liquid circulating in the inner space of the closed liquid cooling system will circulate through the tube section of the liquid-liquid-heat exchanger for exchanging thermal energy between liquid which flows through the tube section of the liquid-liquid-heat exchanger and water in contact with the tube section of the liquid-liquid-heat exchanger and surrounding the shell structure of the propulsion unit.

11. The propulsion unit according to claim 8, wherein the inner space of the closed liquid circulation cooling system is partly limited by the support section of the shell structure of the propulsion unit so that liquid which flows in the inner space of the closed liquid circulation cooling system will be in direct contact with the support section of the shell structure for exchanging thermal energy between liquid flowing in the inner space of the closed liquid circulation cooling system and water surrounding the support section of the shell structure via the support section of the shell structure.

12. The propulsion unit according to claim 8, wherein the inner space of the closed liquid circulation cooling system is partly limited by a part of the cylindrical outer surface of the cylindrical section of the motor housing section so that liquid which flows in the inner space of the closed liquid circulation cooling system will be in direct contact with said part of the cylindrical outer surface of the cylindrical section of the motor housing section for exchanging thermal energy between the electric motor arranged in the cylindrical section of the motor housing section and liquid which flows in the inner space of the closed liquid circulation cooling system via said part of the cylindrical section of the motor housing section between the electric motor and liquid circulating in the inner space of the closed liquid circulation cooling system.

13. The propulsion unit according to claim 12, wherein said part of the cylindrical outer surface of the cylindrical section of the motor housing section in contact with liquid in the inner space of the closed liquid circulation cooling system is provided with partition elements for creating several individual flows of liquid along said part of the cylindrical outer surface of the cylindrical section of the motor housing section.

14. The propulsion unit according to claim 8, wherein the closed liquid circulation cooling system is provided with a first liquid tank;

wherein the first liquid tank has a first inner space that forms a part of the inner space of the closed liquid circulation cooling system, the first liquid tank being in fluid communication with the closed liquid circulation cooling system such that liquid which flows in the closed liquid circulation cooling system will flow through the first inner space of the first liquid tank; and

wherein the first inner space of the first liquid tank is partly limited by said part of the cylindrical outer surface of the cylindrical section of the motor housing section so that liquid in a first inner space of the first liquid tank is will be in direct contact with the cylindrical outer surface of the cylindrical section of the motor housing section for exchanging thermal energy between the electric motor arranged in the motor housing section and liquid which flows in the first inner space of the first liquid tank via said part of the cylindrical outer surface of the cylindrical section of the motor housing section.

15. The propulsion unit according to claim 14, wherein the first liquid tank is additionally partly limited by the support section of the shell structure so that liquid in the first inner space of the first liquid tank will be additionally in direct contact with the support section of the shell structure for exchanging thermal energy between liquid which flows in the first inner space of the first liquid tank of the closed liquid circulation cooling system and water surrounding the support section of the shell structure via the support section of the shell structure.

16. The propulsion unit according to claim 8, wherein the closed liquid circulation cooling system is provided with a second liquid tank, wherein the second liquid tank has a second inner space that forms a part of the inner space of the closed liquid circulation cooling system, the second liquid tank being in fluid communication with the closed liquid circulation cooling system such that liquid which flows in the closed liquid circulation cooling system will flow through the second inner space of the second liquid tank; and

wherein the second liquid tank is partly limited by the support section of the shell structure so that liquid in the second inner space of the second liquid tank will be in direct contact with the support section of the shell structure for exchanging thermal energy between liquid flowing in the second inner space of the second liquid tank and water surrounding the support section of the shell structure via the support section of the shell structure.

17. The propulsion unit according to claim 8, wherein the gas-liquid-heat exchanger is a separate heat exchanger in fluid connection with the closed gas circulation cooling system and in fluid connection with the closed liquid cooling system for exchanging thermal energy between gas circulating in the closed gas circulation cooling system and liquid in the closed liquid cooling system.

18. The propulsion unit according to claim 1, wherein the lower end of the support section of the shell structure is connected to the motor housing section of the shell structure so that the cylindrical outer surface of the cylindrical section of the motor housing section of the shell structure of the propulsion unit partly forms the outermost surface of the propulsion unit, which outermost surface is configured to be at least partly in contact with water surrounding the propulsion unit.

19. The propulsion unit according to claim 1, wherein the cylindrical section of the motor housing section is of a single-layer construction.

20. The propulsion unit according to claim 1, wherein the closed liquid cooling system is arranged at least partly enclosed by the shell structure of the propulsion unit, wherein the closed gas circulation cooling system is arranged at least partly enclosed by the shell structure of the propulsion unit, and wherein the gas-liquid-heat exchanger is arranged at least partly enclosed by the shell structure of the propulsion unit.

21. The propulsion unit according to claim 1, wherein the closed liquid cooling system is configured to be arranged fully outside a hull of a ship, wherein the closed gas circulation cooling system is configured to be arranged fully outside the hull of the ship, and wherein the gas-liquid-heat exchanger is configured to be arranged fully outside the hull of the ship.