Embodiments of the present invention relate to a ship propulsion device and a ship having the same, and more particularly to a ship propulsion device in which two propellers generate propulsive force via counter rotation thereof and a ship having the same.
Ships have a propulsion device to generate propulsive force for sailing. In general, a single propeller is used in the propulsion device. However, the propulsion device having a single propeller cannot acquire propulsive force from rotational energy of water streams, and thus causes substantial energy loss.
A Counter Rotating Propeller (CRP) type propulsion device is a device that acquires propulsive force from rotational energy without energy loss. In the counter rotating propeller type propulsion device, two propellers installed on the same axis generate propulsive force via counter rotation thereof. A rear propeller of the counter rotating propeller type propulsion device is rotated in reverse with respect to a rotating direction of a front propeller, thereby acquiring propulsive force from rotational energy of fluid caused by the front propeller. Accordingly, the counter rotating propeller type propulsion device may exhibit higher propulsion performance than the aforementioned propulsion device having a single propeller.
The counter rotating propeller type propulsion device includes an inner shaft connected to an engine within a hull, a rear propeller coupled to a rear end of the inner shaft, a hollow outer shaft rotatably installed around an outer surface of the inner shaft, and a front propeller coupled to a rear end of the outer shaft. In addition, the counter rotating propeller type propulsion device includes a counter rotation unit installed within the hull to reverse rotating direction of the inner shaft and transmit reversed rotation to the outer shaft. A typical planetary gear mechanism is used as the counter rotation unit.
However, in the case of the above-described counter rotating propeller type propulsion device, the hollow outer shaft has difficulty in center alignment with respect to the inner shaft upon installation of the counter rotating propeller type propulsion device to a ship. In addition, the outer shaft needs an increased lubrication area for reduction in friction between the inner shaft and the outer shaft. The counter rotation of the inner shaft and the outer shaft causes shear of a lubrication layer between the inner shaft and the outer shaft, which makes it difficult to realize efficient lubrication.
Meanwhile, in the case of a typical azimuth thruster system, a propeller is rotatable within a range of 360 degrees to enable free forward and rearward propulsion or rotation of a ship. For example, azimuth thrusters, azipods, and the like are used in the azimuth thruster system. The azimuth thruster system is used in various ships including drill ships, icebreakers, shuttle tankers, floating production storage and offloading (FPSO) vessels, polar sailing cargo ships, passenger ships, and the like, owing to control performance and various other advantages.
However, in case of applying a propulsion method of the above-described counter rotating propeller type propulsion device to the typical azimuth thruster system, the same problems as those of the typical counter rotating propeller type propulsion device may occur, and there is a need for a more effective counter rotating propeller type propulsion device.
It is an embodiment of the present invention to provide a ship propulsion device which may realize counter rotation of two propellers even without an outer shaft and a ship having the same.
In addition, it is another embodiment of the present invention to provide a ship propulsion device which applies a propulsion method to enable counter rotation of two propellers without an outer shaft to an azimuth propulsion method and a ship having the same.
In accordance with one aspect of the present invention, a ship propulsion device includes a rear propeller fixed to a drive shaft, a front propeller rotatably supported by the drive shaft in front of the rear propeller, a counter rotation unit configured to reverse rotating direction of the drive shaft and transmit reversed rotation to the front propeller, a motor configured to rotate the drive shaft, and a housing configured to extend downward from a stern part of a hull and surround the counter rotation unit and the motor.
The counter rotation unit may include a driving bevel gear fixed to the drive shaft, a driven bevel gear fixed to a hub of the front propeller, and one or more reverse bevel gears configured to reverse rotating direction of the driving bevel gear and transmit reversed rotation to the driven bevel gear.
Shafts of the reverse bevel gears installed in a direction crossing the drive shaft to support the reverse bevel gears may further be provided.
A casing configured to support the shafts of the reverse bevel gears may further be provided.
A first cylindrical lining attached to a front surface of the hub of the front propeller for sealing between the hub of the front propeller and a rear surface of the housing, and a first cylindrical sealing member installed to the rear surface of the housing so as to come into contact with an outer surface of the first lining may further be provided.
A second cylindrical lining attached to a front surface of a hub of the rear propeller for sealing between the hub of the rear propeller and the hub of the front propeller, and a second cylindrical sealing member installed to a rear surface of the front propeller so as to come into contact with an outer surface of the second lining may further be provided.
In accordance with another aspect of the present invention, a ship including a ship propulsion device is provided.
A ship propulsion device and a ship having the same according to the embodiment of the present invention may realize counter rotation of two propellers without an outer shaft.
Further, applying a propulsion method that enables counter rotation of two propellers without the outer shaft to an azimuth propulsion method may enhance propulsion efficiency.
Furthermore, owing to absence of the outer shaft, installation of a drive shaft as well as center alignment of the installed drive shaft may be easily implemented.
In addition, absence of the outer shaft may reduce a required lubrication area than the related art and minimize problems due to lubrication.
The exemplary embodiments of the present invention will hereinafter be described in detail with reference to the accompanying drawings.
As exemplarily shown in
As exemplarily shown in
The drive shaft 10, as exemplarily shown in
The rear propeller 20 includes a hub 21 fixed to a tail portion of the drive shaft 10 and a plurality of blades 22 arranged on an outer surface of the hub 21. The rear propeller 20 is fixed to the drive shaft 10 as an outer surface of the tapered portion 14 of the drive shaft 10 is press-fitted into a center shaft-coupling bore 23 of the hub 21. In addition, the rear propeller is more firmly fixed to the drive shaft 10 as a fixing nut 24 is fastened to a rear end of the drive shaft 10. To achieve this coupling, the shaft-coupling bore 23 of the hub 21 may have a shape corresponding to the outer surface of the tapered portion 14 of the drive shaft 10. In
The front propeller 30 is rotatably coupled to the outer surface of the drive shaft 10 at a position forwardly spaced apart from the rear propeller 20. The front propeller 30 includes a hub 31 rotatably supported by the outer surface of the drive shaft 10 and a plurality of blades 32 arranged on an outer surface of the hub 31. The front propeller 30 and the rear propeller 20 are configured to implement counter rotation, and therefore blade angles of the front and rear propellers are opposite to each other.
The hub 31 of the front propeller 30 is rotatably supported at the center thereof by a radial bearing 51, and is rotatably supported at both sides thereof by a front thrust bearing 52 and a rear thrust bearing 53 respectively.
The front thrust bearing 52 has an inner race supported by an edge of the second stepped portion 13 of the drive shaft 10 and an outer race supported by a front bearing support portion 33 of the hub 31. The rear thrust bearing 53 has an inner race supported by a support ring 60 so as not to be axially pushed, the support ring being mounted on the outer surface of the drive shaft 10, and an outer race supported by a rear bearing support portion 34 of the hub 31. In this case, the radial bearing 51 serves to bear radial load of the front propeller 30 applied in a radial direction of the drive shaft 10, and the front and rear thrust bearings 52 and 53 serve to bear thrust load applied to the drive shaft 10 in both axial front and rear directions. In particular, the front thrust bearing 52 serves to bear thrust load applied from the front propeller 30 to the bow during forward movement of the ship, and the rear thrust bearing 53 serves to bear thrust load applied from the front propeller 30 to the stern during rearward movement of the ship.
The hub 31 of the front propeller 30 may be provided with reinforcing members 41 and 42 respectively at positions where the front and rear bearing support portions 33 and 34 are provided. Providing the reinforcing members 41 and 42 respectively at installation positions of the front thrust bearing 52 and the rear thrust bearing 53 increases rigidity of the hub 31. The reinforcing members 41 and 42 may be formed of steel that is more rigid than the hub 31. In the same manner, a reinforcing member 43 may further be provided at a front surface of the hub 21 of the rear propeller 20 at a portion thereof to come into contact with the support ring 60.
Here, after the front propeller 30 and the rear thrust bearing 53 are mounted to the first drive shaft 10, the hub 21 of the rear propeller 20 may be coupled to the first drive shaft 10 via press fitting, and then the support ring 60 may be interposed between the rear propeller hub 21 and the rear thrust bearing 53. The reason why the support ring 60 is installed as described above is because accurately maintaining a distance between the rear thrust bearing 53 and the rear propeller hub 21 is difficult due to a coupling error of the rear propeller caused according to circumstances when the rear propeller 20 is press-fitted to the first drive shaft 10. Accordingly, after the rear propeller 20 is first assembled, a distance between the rear thrust bearing 53 and the rear propeller hub 21 is measured, and the support ring 60 is fabricated to correspond to the distance. In this way, accurate coupling of the support ring and the first drive shaft 10 may be achieved.
The counter rotation unit 70, as exemplarily shown in
The counter rotation unit 70 includes a driving bevel gear 71 fixed to the flange portion 11 of the drive shaft 10 so as to rotate along with the drive shaft 10, a driven bevel gear 72 fixed to a front surface of the hub 31 of the front propeller 30 so as to face the driving bevel gear 71, and a plurality of reverse bevel gears 73 to reverse rotating direction of the driving bevel gear 71 and transmit reversed rotation to the driven bevel gear 72. In addition, to support a plurality of reverse bevel gear shafts 74, the counter rotation unit includes a cylindrical casing 75 configured to surround the reverse bevel gears 73.
The driving bevel gear 71 is fixed to the flange portion 11 as a plurality of fixing bolts 71 a is fastened to the driving bevel gear supported by the first stepped portion 12 of the flange portion 11. The driven bevel gear 72 is fixed to the hub 31 as a plurality of fixing bolts 72a is fastened to the driven bevel gear in a state in which a rear surface of the driven bevel gear comes into contact with the front propeller hub 31. In addition, an inner diameter portion of the driven bevel gear 72 is spaced apart from an outer surface of the drive shaft 10 to prevent generation of friction during rotation thereof. Although
The plurality of reverse bevel gears 73 is tooth-engaged with one another between the driving bevel gear 71 and the driven bevel gear 72. The shafts 74 configured to support the respective reverse bevel gears 73 may installed in a direction crossing the drive shaft 10 and may be arranged radially about the drive shaft 10. In addition, the reverse bevel gear shaft 74, as exemplarily shown in
Although the present embodiment illustrates the plurality of reverse bevel gears 73, it may be unnecessary to provide the plurality of reverse bevel gears 73 so long as the reverse bevel gear 73 serves to reverse rotating direction of the driving bevel gear 71 and transmit reversed rotation to the driven bevel gear 72. In the case of a small ship having less driving load, only one reverse bevel gear may realize the above-described function.
The reverse bevel gears 73, as exemplarily shown in
The above-described counter rotation unit 70 enables counter rotation of the driving bevel gear 71 and the driven bevel gear 72 as the plurality of reverse bevel gears 73 reverses rotating direction of the driving bevel gear 71 and transmits reversed rotation to the driven bevel gear 72. Accordingly, it is possible to achieve counter rotation of the front propeller 30 directly connected to the driven bevel gear 72 and the rear propeller 20 directly connected to the drive shaft 10.
In addition, the counter rotation unit 70 of the present embodiment reverses rotation via the plurality of bevel gears 71, 72, and 73, thus having a smaller volume than that of a typical planetary gear type counter rotation unit. In particular, according to the present embodiment, upon installation of the counter rotation unit 70, a rear surface of the driven bevel gear 72 may face a front surface of the front propeller hub 31 and rotation centers of the driven bevel gear 72 and the hub 31 may coincide with each other, which enables direct connection between the driven bevel gear 72 and the front propeller hub 31. Accordingly, differently from the related art, it is possible to transmit power to the front propeller 30 without using an outer shaft. Moreover, absence of the outer shaft may ensure less friction of the drive shaft 10 than the related art, and consequently, ensure a smaller lubrication area than the related art. In addition, absence of the outer shaft may facilitate installation of the drive shaft 10 and center alignment of the shaft after installation thereof.
A typical planetary gear type counter rotation unit includes a sun gear installed to a drive shaft, a planetary gear around the sun gear, and a cylindrical internal gear around the planetary gear, thus having a relatively large volume. In addition, the planetary gear type counter rotation unit should have a very large volume in consideration of a casing around the internal gear because the internal gear located at an outermost position needs to rotate. In addition, it is necessary to use a hollow shaft corresponding to the typical outer shaft for power transmission from the cylindrical internal gear to the front propeller. In conclusion, the related art has difficulty in achieving a simplified configuration and reduced volume as proposed in the present embodiment.
The propulsion device of the present embodiment, as exemplarily shown in
The propulsion device of the present embodiment, as exemplarily shown in
The first sealing unit 90, as exemplarily shown in
The first sealing member 92 includes a plurality of packings 93a, 93b, and 93c arranged at an interval on an inner surface thereof facing the first lining 91 so as to come into contact with an outer surface of the first lining 91, and a path 95 configured to supply fluid for sealing into grooves between the packings 93a, 93b, and 93c. The path 95 of the first sealing member 92 may be connected to a lubricant supply path 96 defined in the housing 130 to supply lubricant having a predetermined pressure. The lubricant having a predetermined pressure is supplied into the grooves between the packings 93a, 93b, and 93c to press the respective packings 93a, 93b, and 93c onto the first lining 91 until the packings come into close contact with the first lining, which may prevent invasion of saltwater or foreign substances.
The first lining 91, as exemplarily shown in
In addition, a packing 91 d may be provided at a divided portion 91 c of any one of the first and second members 91a and 91b to achieve sealing upon coupling of the first and second members. A free end of the divided portion 91c of the first member 91a is provided with a first coupling portion 91e that protrudes toward the second member, and the second member 91b is provided with a second coupling portion 91f corresponding to the first coupling portion for insertion of the first coupling portion. As a fixing bolt 91g is fastened through the first coupling portion and the second coupling portion, strong mutual coupling of the first and second members is accomplished. A plurality of fixing bolts 91i may be fastened to a flange portion 91h fixed to the front propeller hub 31 to achieve strong fixing of the flange portion with respect to the hub 31.
In the case of the first sealing member 92, a plurality of semicircular rings 92a, 92b, and 92c may be stacked one above another in a longitudinal direction of the drive shaft 10 at the outside of the first lining 91 and fixed to one another. In this case, the plurality of rings 92a, 92b, and 92c may be coupled to one another via bolting or welding.
The second sealing unit 110, as exemplarily shown in
The path 115 of the second sealing member 112 may be connected to a lubricant supply path 124 defined in the drive shaft 10. To this end, the drive shaft 10 and the support ring 60 may be provided with a first radial connection path 121 that connects the lubricant supply path 124 to a space 122 inside the second lining 111. The reinforcing member 42 at the rear surface of the front propeller hub 31 may be provided with a second connection path 123 that connects the space 122 inside the second lining 111 to the path 115 of the second sealing member 112. Lubricant for sealing is supplied from the center of the drive shaft 10 to the second sealing member 112 to press the packings 113a, 113b, and 113c, which may realize sealing.
Similar to the first lining 91 and the first sealing member 92 of the first sealing unit 90, the second lining 111 and the second sealing member 112 have a semicircular shape so as to be coupled to each other after installation of the rear propeller 20 and the support ring 60.
Next, operation of the propulsion device according to the present embodiment will be described.
In operation of the propulsion device, if the drive source 140 within the hull 1 supplies power to the motor 131 and the motor 131 rotates the drive shaft 10, the rear propeller 20 directly connected to the rear end of the drive shaft 10 is rotated in the same direction as that of the drive shaft 10. Simultaneously, the driving bevel gear 71 of the counter rotation unit 70 fixed to the drive shaft 10 is rotated along with the drive shaft 10. Rotating direction of the driving bevel gear 71 is reversed by the plurality of reverse bevel gears 73 and transmitted to the driven bevel gear 72, which causes the driven bevel gear 72 to be rotated in reverse with respect to a rotating direction of the drive shaft 10. Accordingly, the front propeller 30 directly connected to the driven bevel gear 72 and is rotated in reverse with respect to a rotating direction of the rear propeller 20.
The front propeller 30 and the rear propeller 20, which implement counter rotation, have blade angles opposite to each other, and therefore generate propulsive water streams in the same direction. That is, the front and rear propellers generate rearward propulsive water streams during forward movement of the ship, and generate forward propulsive water streams during rearward movement of the ship via counter rotation thereof In addition, with regard to the propulsive water streams generated during forward movement of the ship, the rear propeller 20 acquires propulsive force from rotational energy of fluid having passed through the front propeller 30 via reverse rotation thereof, which results in enhanced propulsion performance. This is equally applied even during rearward movement of the ship. In addition, the steering unit may be used to change the direction of propulsive force applied to the hull 1 by the front propeller 30 and the rear propeller 20, which may change a movement direction of the ship.
Meanwhile, the front propeller 30 generates rearward propulsive water streams during forward movement of the ship, and thus is affected by corresponding repulsive force. This force is transmitted to the drive shaft 10 via the front thrust bearing 52, thereby serving as propulsive force. Similarly, the rear propeller 20 generates rearward propulsive water streams during forward movement of the ship and is affected by repulsive force. This force is similarly transmitted to the drive shaft 10 directly connected to the rear propeller, thereby serving as propulsive force.
During rearward movement of the ship, propulsive force (repulsive force) of the front propeller 30 is transmitted to the drive shaft 10 via the rear thrust bearing 53, and propulsive force of the rear propeller 20 is also transmitted to the drive shaft 10 directly connected to the rear propeller. In conclusion, the propulsion device of the present embodiment allows propulsive force generated via operation of the front propeller 30 and the rear propeller 20 during forward movement and rearward movement of the ship to be wholly transmitted to the hull 1 through the drive shaft 10.
Number | Date | Country | Kind |
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10-2011-0058053 | Jun 2011 | KR | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/KR2011/007025 | 9/23/2011 | WO | 00 | 10/13/2014 |