KR101422239B1 - Propulsion apparatus for vessel - Google Patents

Abstract

A ship propulsion system capable of increasing propulsion efficiency by reducing resistance is introduced.
The ship propulsion device includes a pair of propellers disposed opposite to each other, a pair of ring gears connecting the ends of the propellers in the outer circumferential direction, driving means And a duct which is arranged to surround the outer periphery of the propeller and has a rail groove portion on the inner side of which a pair of ring gears are rotated.

Description

{PROPULSION APPARATUS FOR VESSEL}

The present invention relates to a ship propulsion device, and more particularly, to a ship propulsion device capable of minimizing a resistance element and increasing propulsion efficiency by transmitting propulsion force to a propeller through a ring gear.

In general, ships can be moved using thrust generated by the propeller.

In order to reduce the waste of rotational energy, a counter rotating propulsion system (CRP) may be applied to the propeller.

The dual inversion propulsion system is a concept of recovering the kinetic energy of the rotational direction provided by the propeller to the fluid, and it is possible to arrange a pair of propellers rotating in mutually opposite directions to face each other. When applied to the Azimuth propulsion system, it is possible to improve the aft linearity of the hull and the utilization of the internal space of the hull and improve the propulsion efficiency by recovering the rotary energy of the abandoned rotating current.

However, since the dual inversion propulsion system is composed of a complicated internal gear system, a large amount of time and effort must be applied to maintain and repair the inversion gear system, and since the shaft for transmitting the thrust is located at the central portion of the propeller, It can act as an element and reduce the overall propulsion efficiency of the ship.

Domestic patent disclosure 10-2012-0051439 (2012.05.22. Disclosed)

Embodiments of the present invention are directed to providing a propulsion system capable of minimizing resistance elements to improve propulsion efficiency.

According to an aspect of the present invention, there is provided a propeller comprising first and second opposed propeller disposed oppositely; First and second ring gears connected to a blade end of each of the first and second propellers and rotated together with the first and second propellers; Driving means for providing rotational forces in opposite directions to the first and second ring gears; And a duct disposed on the outer periphery of the first and second propellers and having a rail groove portion rotatably connected to the first and second ring gears on an inner surface thereof.

At this time, the driving means includes an inclined thread formed on the opposing surfaces of the first and second ring gears; A bevel gear formed on an outer circumferential surface of the bevel thread engaging with the oblique thread and disposed on one side of the duct; And a driving motor connected to the bevel gear via a drive shaft to rotate the bevel gear.

The support ring may further include a support gear disposed to be spaced along the inner periphery of the duct to support the first and second ring gears.

Further, the support gear may include a bevel gear engaged with the first and second ring gears.

The rail groove portion may be provided with a support roller or a support bearing for supporting the first and second ring gears.

Further, the driving means may include an inclined screw thread formed on the opposing surfaces of the first and second ring gears; A plurality of bevel gears formed on an outer circumferential surface of the bevel thread engaging with the oblique threads and spaced apart along the duct; And a plurality of drive motors respectively connected to the plurality of bevel gears via a drive shaft, for rotating the respective bevel gears.

The duct may be provided with a mounting housing that surrounds the plurality of driving motors, respectively, and has a curved curved surface on an outer surface thereof.

Embodiments of the present invention are advantageous in that maintenance and repair of the propulsion device can be easily performed because the configuration of the shaft and gear system of the complex structure used in the conventional Ajmus propulsion device is unnecessary.

Embodiments of the present invention also have the advantage that a single motor and a plurality of supporter gears are distributed in a balanced manner in the duct, so that the propulsive force of the motor can be transmitted to the propeller in a balanced and stable manner.

Further, the embodiments of the present invention can distribute the propulsive force of the motor to the propeller in a balanced and stable manner by distributing a plurality of motors in a balanced manner in the duct, and even if an abnormality occurs in some motors among a plurality of motors, It is possible to effectively cope with a crisis situation in which an abnormality occurs in the motor at the time of navigation of the ship.

1 is a partial cross-sectional view illustrating a ship propulsion apparatus according to a first embodiment of the present invention.
2 is a front view showing a ship propulsion apparatus according to a first embodiment of the present invention.
3 is a partial cross-sectional view showing a ship propulsion apparatus according to a modification of the first embodiment.
4 is a front view showing a ship propulsion apparatus according to another modification of the first embodiment.
5 is a partial cross-sectional view illustrating a ship propulsion apparatus according to a second embodiment of the present invention.
6 is a front view showing a ship propulsion apparatus according to a second embodiment of the present invention.
7 is a front view showing a ship propulsion apparatus according to a modification of the second embodiment.

Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.

In the following description of the present invention, detailed description of known functions and configurations incorporated herein will be omitted when it may make the subject matter of the present invention rather unclear.

FIG. 1 is a partial cross-sectional view showing a ship propelling apparatus according to a first embodiment of the present invention, FIG. 2 is a front view showing a ship propelling apparatus according to a first embodiment of the present invention, FIG. 4 is a front view showing a ship propulsion apparatus according to another modification of the first embodiment. FIG.

1 and 3, the left side of the drawing is shown forward and the right side of the drawing is shown rearward. However, the present invention is not limited thereto, and depending on the shape of the blades of the propeller and the shape of the duct, Rearward, the right side of the drawing may be defined forward.

1 and 2, a ship propulsion device according to a first embodiment of the present invention includes a pair of propellers 100 disposed to face each other, and a pair of propellers 100 connecting the ends of the pair of propellers 100 A driving means 300 for providing a rotational force in the opposite direction to the pair of ring gears 200, a duct 400 for providing a fluid movement path, a ring gear 200 And a support gear 500 for supporting the support gear 500.

Specifically, the propeller 100 may include a plurality of blades extending outward in a spiral shape with respect to the center of rotation, and spaced apart in the circumferential direction. The propeller 100 may be rotated clockwise or counterclockwise by receiving driving force from the driving means 300.

The propeller 100 may include a first propeller 100a and a second propeller 100b that are spaced apart from each other to face each other. When the driving force is transmitted from the driving means 300, the first and second propellers 100a and 100b are rotated in opposite directions to recover rotational energy of the discarded rotating electric current. The propeller 100 is rotated through the ring gear 200 connected to the tip of the propeller 100 without the axis of the central portion for rotating the propeller 100, The resistance element can be minimized.

The first propeller 100a is disposed on the front side of the ship propulsion device so as to be spaced apart from the second propeller 100b and is composed of three blades that are deployed in a spiral shape in one direction (clockwise with respect to the front face) And a first ring gear 200a, which will be described later, may be fixedly connected to the corresponding tip. The second propeller 100b is disposed on the rear side of the ship propulsion device so as to be spaced apart from the first propeller 100a and has three blades extending in a spiral shape in the other direction (counterclockwise with respect to the front face) And the second ring gear 200b, which will be described later, can be fixedly connected to the corresponding tip.

In the present embodiment, the first and second propellers 100a and 100b are each formed of three blades, but the present invention is not limited thereto. Depending on the optimum design conditions for improving the propulsion efficiency, the propeller 100 ) May be composed of four or more blades.

At the tip of the propeller 100, more specifically, at the outermost end located farthest from the center of rotation, the ring gear 200 can be fixedly connected.

The ring gear 200 is formed in a ring shape surrounding the outer periphery of the propeller 100. The outermost end of the propeller 100 is fixedly connected to the inner circumferential surface of the ring gear 200 and an inclined thread 310 . Accordingly, when the driving force for propelling the ship is transmitted to the oblique thread 310 of the ring gear 200, the ring gear 200 can be rotated by the driving force transmitted to the oblique thread 310, 200, propulsion force for movement can be provided to the ship as the propeller 100 is rotated.

The ring gear 200 may include a first ring gear 200a fixed to the first propeller 100a and a second ring gear 200b disposed on the second propeller 100b. The first and second ring gears 200a and 200b are positioned between the propeller 100 and the drive means 300 so that the driving force of the drive means 300 is transmitted to the first and second propellers 100a and 100b ).

The first and second ring gears 200a and 200b can be mounted on the rail groove portion 410 of the duct 400 to be rotatable in opposite directions. The first and second ring gears 200a and 200b are provided in the roller groove 411 of the rail groove portion 410 for smooth rotation of the first and second ring gears 200a and 200b. And can be supported by a plurality of support rollers 630b. The support roller 630b is disposed on the front side of the first ring gear 200a and the front side of the second ring gear 200b so that the pair of ring gears 200 can be in close contact with the bevel gear 320 of the driving means 300. [ And can be respectively supported on the rear side. At this time, the contact surface of the ring gear 200 to which the support roller 630b is contacted may be formed to be inclined.

Of course, the first and second ring gears 200a and 200b may be rotatably mounted on the rail groove portion 410 through various supporting means in addition to the configuration of the supporting roller 630b.

3, the ring gear bearing 630d is provided in the rail groove portion 410 so that the ring gear bearing 630d is disposed between the front side of the first ring gear 200a and the front side of the second ring gear 200b. It is also possible to support the rear side of the second housing 200b. At this time, the upper portions of the first and second ring gears 200a and 200b are supported by the bevel gear 320 of the driving means 300, and the upper ends of the first and second ring gears 200a and 200b Since the lower portion is supported by the support gear 500, the upward and downward flows of the first and second ring gears 200a and 200b can be restricted.

The first and second ring gears 200a and 200b may be interlocked to rotate in opposite directions through the driving means 300. [

The driving means 300 is configured to simultaneously drive the first and second propellers 100a and 100b fixed to the first and second ring gears 200a and 200b in opposite directions to each other, A gear 310, a bevel gear 320, and a drive motor 330.

Here, the oblique thread 310 is formed obliquely on the opposite faces of the pair of ring gears 200, for example, the first and second ring gears 200a and 200b, so that the bevel thread 320 321). The bevel gear 320 is formed on the outer circumferential surface of the bevel gear 320 with a bevel thread 321 engaged with the bevel thread 310 and disposed on one side of the duct 400. The driving motor 330 may be connected to the bevel gear 320 via the driving shaft 340 in a state where the driving motor 330 is fixed to the hull.

When the drive shaft 340 is rotated in one direction by the operation of the drive motor 330, the bevel gear 320 is rotated by the rotation of the drive shaft 340, and the rotational force of the bevel gear 320 is transmitted to the bevel thread The first and second ring gears 200a and 200b are rotated in opposite directions to each other while being transmitted to the inclined threads 310 of the first and second ring gears 200a and 200b engaged with the first and second ring gears 200a and 321 As a result, the first and second propellers 100a and 100b can be rotated forward and reverse, respectively, by the rotation of the first and second ring gears 200a and 200b in the opposite direction.

The duct 400 can be fixed to the bottom surface of the hull 610 through the support 620 and is formed in the shape of a cylindrical tube surrounding the outer sides of the first and second propellers 100a and 100b, The second propeller 100a, and the second propeller 100b.

The duct 400 may be formed with a rail groove portion 410 for guiding rotation of the first and second ring gears 200a and 200b. The rail groove portion 410 has a groove shape into which the ring gear 200 is inserted and can provide a rotation path of the ring gear 200 when the ring gear 200 rotates. In addition, the rail groove portion 410 may be formed with a roller groove 411 on which the support roller 630b is mounted. At this time, the support roller 630b can be rotatably mounted on the roller groove 411 via a rotation shaft.

In addition, the duct 400 may be provided with a support bearing 630a for smoothly maintaining the rotation of the drive shaft 340. The support bearing 630a can be used to mount the support body to support the drive shaft 340 or to support the support shaft 501 of the support gear 500 described later.

The support gear 500 can support the ring gear 200 to maintain the balance of the position of the ring gear 200. [ For example, the support gears 500 may be spaced apart at regular intervals along the inner circumference of the duct 400 to support the ring gear 200.

The support gear 500 includes a bevel gear 320 engageable with the pair of ring gears 200, a support shaft 501 connected to the bevel gear 320, And a support bearing 630b supporting the support bearing 630b.

In this embodiment, the support gear 500 is disposed at an interval of 90 degrees around the circumference of the duct 400 with reference to one side of the duct 400 where the bevel gear 320 is located. However, As a matter of course, they can be arranged at intervals of 120 degrees.

The operation of the ship propulsion device according to the present embodiment having the above-described configuration is as follows.

First, when the driving motor 330 of the driving means 300 is operated, the driving shaft 340 is rotated in one direction by the driving motor 330, and the bevel gear 320 is also rotated in one direction Can be rotated.

At this time, the first and second ring gears 200a and 200b engaged with the bevel gear 320 can be rotated in opposite directions while the bevel gear 320 is rotated. For example, when the bevel gear 320 is rotated in one direction, the first ring gear 200a may be rotated clockwise and the second ring gear 200b may be rotated counterclockwise. Here, the clockwise or counterclockwise direction is described based on the direction in which the ship propulsion device is viewed from the front. (See FIG. 2)

When the first and second ring gears 200a and 200b are rotated, the first and second propellers 100a and 100b are rotated by the rotation of the first and second ring gears 200a and 200b And can be rotated in the same direction as the rotational direction of the ring gear 200 connected to each of them. For example, the first propeller 100a rotates in a clockwise direction and the second propeller 100b rotates in a counterclockwise direction.

When the first and second propellers 100a and 100b are rotated in opposite directions to each other, the first and second propellers 100a and 100b are rotated counterclockwise Therefore, the propulsion efficiency can be increased, and the vortex phenomenon due to the wake can be reduced to improve the steering efficiency. In addition, in the present embodiment, since there is no axis at the central portion for rotating the propeller 100, the resistance element can be minimized, and the structure of the main shaft and the gear system of a complicated structure is unnecessary, Can be easily accomplished.

FIG. 5 is a partial cross-sectional view showing a ship propelling apparatus according to a second embodiment of the present invention, FIG. 6 is a front view showing a ship propelling apparatus according to a second embodiment of the present invention, 1 is a front view showing a ship propulsion apparatus according to a modified example.

5 to 6, the ship propulsion device according to the second embodiment includes a pair of propellers 100, a pair of ring gears 200, a drive means 300, a duct 400 And a mounting housing 350.

Here, the propeller 100, the ring gear 200 and the duct 400 except for the drive means 300 and the mounting housing 350 are installed on the propeller 100, the ring gear 200 and the duct 400 described in the first embodiment, 400, description of the previously described configuration and operation may be omitted, and similar reference numerals may be given to similar configurations.

The driving means 300 may include an oblique thread 310, a plurality of bevel gears 320, and a plurality of driving motors 330.

Here, the oblique threads 310 are formed to be inclined on the opposing surfaces of the first and second ring gears 200a and 200b, and can be engaged with the bevel thread 321 of the bevel gear 320. The plurality of bevel gears 320 may be disposed at regular intervals along the circumference of the duct 400 and a bevel thread 321 may be formed on the outer circumferential surface of the bevel thread 310 to engage with the bevel thread 310. The plurality of driving motors 330 may be arranged at regular intervals along the circumference of the duct 400. The bevel gears 320 may be driven by a driving shaft 340 Can be connected.

That is, when the driving shaft 340 is rotated in one direction by the operation of each driving motor 330, the plurality of bevel gears 320 are rotated by the rotation of the plurality of driving shafts 340, The first and second ring gears 200a and 200b are transmitted to the bevel thread 310 of the first and second ring gears 200a and 200b engaged with the bevel thread 321, And the first and second propellers 100a and 100b can be simultaneously rotated in the forward and reverse directions.

In this embodiment, the driving motors 330 are disposed at intervals of 90 degrees along the circumference of the duct 400, but they may be spaced apart from each other by 120 degrees as shown in FIG.

The mounting housing 350 is a case for protecting the driving motor 330, and a driving motor 330 is provided inside the mounting housing 350. The outer surface of the driving motor 330 may be formed into a streamlined curved surface. This minimizes the fluid resistance due to the mounting housing 350 when moving the ship.

As described above, since the structure of the shaft and the gear system of a complicated structure is unnecessary, maintenance and repair of the propulsion device can be easily performed, and when one motor and a plurality of supporter gears are distributed in a balanced manner in the duct, The propulsive force of the motor can be transmitted to the propeller in a balanced manner and stably. When a plurality of motors are distributed in a balanced manner in the duct, even if an abnormality occurs in some motors among a plurality of motors, It is possible to effectively cope with a crisis situation in which an abnormality occurs in the motor.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed exemplary embodiments, but, on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the invention. Skilled artisans may implement a pattern of features that are not described in a combinatorial and / or permutational manner with the disclosed embodiments, but this is not to depart from the scope of the present invention. It will be apparent to those skilled in the art that various changes and modifications may be readily made without departing from the spirit and scope of the invention as defined by the appended claims.

100: Propeller 100a: First propeller
100b: second propeller 200: ring gear
200a: first ring gear 200b: second ring gear
300: drive means 310: oblique thread
320: Bevel gear 321: Bevel thread
330: drive motor 340: drive shaft
400: Duct 410: Rail groove
500: Support gear 501: Support shaft
610: Hull 620: Support
630a: Support bearing 630b: Support roller

Claims (7)

First and second propellers 100a, 100b arranged to face each other;
The first and second ring gears 200a and 200b connected to the respective blade ends of the first and second propellers 100a and 100b and rotated together with the first and second propellers 100a and 100b, (200b);
A driving means (300) for providing a rotational force in opposite directions to the first and second ring gears (200a, 200b); And
The first and second ring gears 200a and 200b are rotatably connected to the inner side surfaces of the first and second propellers 100a and 100b, And a duct 400,
The driving means (300)
An oblique thread 310 formed on opposing surfaces of the first and second ring gears 200a and 200b;
A plurality of bevel gears 320 formed on the outer circumferential surface of the bevel thread engaging with the oblique threads 310 and spaced apart along the duct 400; And
And a plurality of drive motors (330) connected to the plurality of bevel gears (320) through a drive shaft to rotate the respective bevel gears (320). delete The method according to claim 1,
Further comprising a support gear (500) spaced apart along the inner circumference of the duct (400) to support the first and second ring gears (200a, 200b). The method of claim 3,
The support gear (500) includes a bevel gear (320) engaged with the first and second ring gears (200a, 200b). The method according to claim 1,
Wherein the rail groove portion (410) is provided with a support roller or a support bearing for supporting the first and second ring gears (200a, 200b). delete The method according to claim 1,
Wherein the duct (400) is provided with a mounting housing (350) which surrounds the plurality of drive motors, respectively, and has a curved surface in a streamlined shape on its outer surface.

Images