KR101616992B1 - A ship for reducing vibromotive force - Google Patents
A ship for reducing vibromotive force Download PDFInfo
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- KR101616992B1 KR101616992B1 KR1020140077111A KR20140077111A KR101616992B1 KR 101616992 B1 KR101616992 B1 KR 101616992B1 KR 1020140077111 A KR1020140077111 A KR 1020140077111A KR 20140077111 A KR20140077111 A KR 20140077111A KR 101616992 B1 KR101616992 B1 KR 101616992B1
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- KR
- South Korea
- Prior art keywords
- working gas
- pad
- propeller
- hull
- receiving membrane
- Prior art date
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
- B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
- B63H1/14—Propellers
- B63H1/15—Propellers having vibration damping means
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
A propeller cavitation organic exciter-powered vessel is disclosed. In accordance with an aspect of the present invention, there is provided a propeller-cavitation-induced propulsion-reduction vessel comprising: a hull having a propeller; And a working gas receiving bag having a working gas pocket in which a working gas for generating a reflected wave for causing a destructive interference phenomenon with an incident wave generated when the propeller rotates is enclosed and accommodated; And a camera module having a camera for monitoring the working gas receiving membrane pads in real time and disposed within the hull adjacent to the working gas receiving membrane pads.
Description
TECHNICAL FIELD The present invention relates to a propeller cavitation organic exciter force reduction type vessel, and more particularly, to a propeller cavitation organic exciter force reduction type vessel capable of real time monitoring of a work gas receiving membrane pad.
When the propeller provided at the rear of the ship rotates in water, the water flows to the propeller blade surface, causing a difference in hydraulic pressure between the front and back surfaces of the propeller blade surface. The propulsion generated in this way allows the ship to be operated at sea.
On the other hand, when the propeller is operated for the operation of the ship, that is, when the propeller is rotated in water, a fluctuating pressure is generated in the water due to the propeller as the rotating body. The fluctuating pressure thus generated increases the excitation force to the hull, (Including noise).
Particularly, when cavitation occurs in the water by the propeller, vibration of the hull is severely generated because the excitation force is further increased.
This is because when the pressure in the water is low, the gas contained in the water escapes from the water and collects at a low pressure. As a result, bubbles are generated in the water, and when the bubbles reach the high pressure part, Thereby generating a fluctuating pressure.
In order to solve the problem of increased excitation force due to such fluctuating pressure, it is necessary to design the shape and size of the propeller blade itself differently, to improve the shape of the rear of the ship, to attach a separate reinforcing material for preventing noise and vibration, Or by applying various methods such as attaching a guide device for guiding the flow of the water flowing in the propeller, reducing the size of the propeller, or the like. However, it is practically effective to reduce the excitation force it's difficult.
The vibration problem including the noise transmitted to the hull by the propeller is increased when the propeller is operated. For example, when the ship is a cruise ship, such as a cruise ship or a warship, .
Accordingly, the present applicant has filed with the Korean Intellectual Property Office (KIPO) a number of technologies for reducing the excitation force by forming an air layer in the form of an air bubble on the surface of the hull adjacent to the propeller.
However, most of the prior art attempts to use the air layer, including the last-filed technology, require air to be continuously injected using a compressor to form an air layer, so that due to the installation and operation of the compressor and its related components Energy consumption and so on.
Accordingly, it is an object of the present invention to prevent vibrations from occurring in the hull by increasing the excitation force at the time of operation of the propeller while fundamentally preventing the burden of energy consumption due to the installation and operation of the compressor and related parts, A method of applying a working gas containing membrane pad accommodated in one side to a hull can be considered.
However, when such a working gas receiving membrane pad is intended to be applied to the hull, the work gas receiving membrane pads may be damaged due to tearing or the like, and if the working gas receiving membrane pads are damaged, A method for real-time monitoring of the situation is required.
SUMMARY OF THE INVENTION Accordingly, the present invention has been made in view of the above problems, and it is therefore an object of the present invention to provide a propulsion device for a propeller which is capable of preventing a vibration from being generated in a hull by increasing propulsion force during operation of a propeller while fundamentally preventing a burden of energy consumption, And it is possible to monitor the working gas receiving membrane pads in real time so that the maintenance work on the working gas receiving membrane pads can be carried out without delay and the propeller cavitation organic excitation force reducing type vessel can be provided.
According to an aspect of the present invention, there is provided a hull comprising: a hull having a propeller; A working gas accommodating membrane pad having a working gas pocket in which a working gas generating a reflected wave for causing a destructive interference phenomenon with an incident wave generated when the propeller rotates is hermetically sealed; And a camera module having a camera for real time monitoring of the working gas receiving membrane pads, the camera module being disposed in the hull adjacent to the working gas receiving membrane pads.
And a paddle rotation control unit coupled to the work gas receiving membrane pads and the camera module, the paddles being provided in the hull to rotationally drive the work gas receiving membrane pads so that the work gas pockets of the work gas receiving membrane pads can be moved in and out of the hull, And may further include a driving unit.
The pad rotation driving unit may include a pad and a module supporting body supporting the working gas accommodating membrane pad and the camera module, one side being hemispherical; A waterproof rotary shaft connected to the pad and the module support to form a rotation axis of the pad and the module support; And a shaft rotating part connected to the waterproof rotating shaft to rotate the waterproof rotating shaft.
The shaft rotation unit includes: a rotation motor; A driving gear connected to a motor shaft of the rotary motor; And a driven gear coupled to an end of the waterproof rotary shaft and meshing with the drive gear.
The camera module may further include a module support coupled to the pad and the module support while supporting the camera.
And a seawater inflow preventing cover disposed inside the hull to surround the working gas receiving membrane pad to prevent inflow of seawater.
A drain portion may be coupled to the side portion of the seawater inflow prevention cover, and a detachable lid having a handle may be provided on the upper portion of the seawater inflow prevention cover.
According to the present invention, it is possible to prevent vibrations from occurring in the hull due to increased propulsive force at the time of operation of the propeller while fundamentally preventing the burden of energy consumption due to the installation and operation of the compressor and related parts. The gas-receiving membrane pads can be monitored in real-time, allowing maintenance work on the working gas-receiving membrane pads to be carried out without delay.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a structural view of a propeller area of a propeller cavitation organic exciter force reduction type ship according to a first embodiment of the present invention; FIG.
FIG. 2 is a schematic view showing an installation structure of a work gas accommodating membrane pad, which is a region A in FIG.
3 is an operation diagram of Fig.
Fig. 4 is a chart for measuring the impedance of water, rubber, and air.
5 is a view for explaining the principle of incident wave and reflected wave.
6 is a view of a working gas receiving membrane pad for illustrating equation (1).
Fig. 7 is a view showing a state where a working gas receiving membrane pad is installed in a region on the upstream side of the propeller, and shows a plurality of variable pressure measuring points.
Figure 8 is a graphical representation of the efficiency of a working gas receiving membrane pad relative to the frequency of the propeller.
Figure 9 is a graph summarizing the results of the 150 Hz band for the working gas receiving membrane pads corresponding to Figure 7;
In order to fully understand the present invention, operational advantages of the present invention, and objects achieved by the practice of the present invention, reference should be made to the accompanying drawings and the accompanying drawings which illustrate preferred embodiments of the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. Like reference symbols in the drawings denote like elements.
FIG. 1 is a structural view of a propeller area of a propeller cavitation propellant-reducing type propulsion vessel according to a first embodiment of the present invention. FIG. 2 is a view schematically showing an installation structure of a working gas receiving membrane pad, And Fig. 3 is an operation diagram of Fig.
Referring to these drawings, the propeller cavitation propulsion reduction type ship according to the present embodiment can prevent the burden of energy consumption and the like due to the installation and operation of the related parts including the compressor, It is possible to prevent vibrations from occurring in the
At the rear of the
For reference, the ship to which the present invention is applied may include all of marine vessels, warships, fishing vessels, carriers, drillships, cruise ships, special work ships, and the like, as well as floating marine structures. Therefore, the scope of right of the present embodiment can not be limited to a specific ship.
As described above, when the
The vibration transmitted to the
In other words, the vibrating force is increased due to the fluctuating pressure generated in the water during the operation of the
As will be described in detail below, the working gas receiving
In other words, since the working gas receiving
Therefore, it is possible to fundamentally prevent the burden of installing and operating the compressor and related parts, and energy consumption.
The working gas receiving
In this embodiment, the working gas receiving
And is further augmented with respect to the mounting position of the working gas receiving
The working gas receiving
The working gas
(Or anode) is attached to the working gas receiving
In this embodiment, the material of the working gas receiving
The
In this embodiment, the
The working
Although the working
As described above, the working
On the other hand, as described above, since the working
If the working
Therefore, if the working
The
The
The
The
This may be a function for preventing the
If the working gas receiving
The pad
The pad
The pad and
As the pad and
The waterproof
At this time, the waterproof
The
When the
On the other hand, when the work gas accommodating
The
A
A
As a result, if the pad
Hereinafter, the principle of reducing the exciting force due to the working gas receiving
Fig. 4 is a graph showing impedance of water, rubber and air, Fig. 5 is a view for explaining the principle of an incident wave and a reflected wave, Fig. 6 is a drawing of a working gas receiving membrane pad for explaining [Equation 1] 7 is a view showing a state in which a working gas receiving membrane pad is installed in a region immediately upstream of the propeller, and FIG. 8 is a graph showing the efficiency of the working gas receiving membrane pad based on the frequency of the propeller And FIG. 9 is a graph summarizing the results of the 150 Hz band for the working gas receiving membrane pads corresponding to FIG.
Referring to these drawings, referring first to FIG. 4, an acoustic impedance (which means an acoustical resistance) of rubber, which is a material of the working gas receiving
Typically, when sound waves propagate in a specific medium and a medium having a different impedance is encountered, a transmission phenomenon and a reflection phenomenon occur. Since the impedance of seawater and rubber is similar, only the reflection phenomenon occurs without reflection at the boundary between sea water and rubber.
For example, as shown in FIG. 5, the incident wave generated in the operation of the
I will explain this again. The spherical pressure wave generated by the cavitation during the operation of the
In this case, when the working gas receiving
When the incident wave is formed as a reflected wave that is reflected by the opposite phase and strikes against the air, the reflected wave meets an incident wave incident on the workpiece receiving
As a result, the fluctuating pressure transmitted from the outside of the working gas receiving
On the other hand, such a reduction performance is limited to a specific frequency band of the propeller as shown in the following equation (1).
[Equation 1]
In this case, f is the reduced frequency band of the propeller, ca (= 340m / s) and cw (= 1500m / s) A " and " b " denote the inner diameter and outer diameter of the working gas receiving membrane pads 130a to 130c, respectively, when they are regarded as equivalents.
A model test was carried out to verify these items. That is, as shown in FIG. 7, one working gas receiving
8, the horizontal axis (x axis) indicates the frequency, and the vertical axis (y axis) indicates the amount of increase / decrease after attachment of the work gas accommodating
FIG. 9 summarizes the results of the 150 Hz band. Referring to FIG. 9, the fluctuating pressures at the positions P2, P3 and P4 located outside the working gas receiving
According to the present embodiment having the structure and function as described above, it is possible to prevent vibrations from being generated in the
As a result, it is possible to effectively prevent vibration from being generated in the
In particular, the structure according to the present embodiment is different from the structure of the present embodiment in that the shape and size of the
As described above, according to the present embodiment, it is possible to prevent vibrations from occurring in the hull by increasing the excitation force at the time of operation of the propeller while fundamentally preventing the burden of energy consumption due to installation and operation of the compressor and other related components And can easily replace the working gas receiving
It will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the spirit or scope of the invention. Accordingly, such modifications or variations are intended to fall within the scope of the appended claims.
110: Hull 120: Propeller
125: rudder 130: working gas receiving membrane pad
131: Pad body 132: Working gas pocket
150: pad rotation driving part 160: pad and module support
162: waterproof
164:
164b:
170: Seal inflow preventing cover 172: Drain part
173: handle 174: detachable cover
180: camera module 181: camera
182: Module support
Claims (7)
A working gas accommodating membrane pad including a working gas pocket in which a working gas generating a reflected wave for causing a destructive interference phenomenon with an incident wave generated when the propeller rotates is hermetically sealed;
A camera module having a camera for monitoring the working gas receiving membrane pads in real time and disposed in the hull adjacent to the working gas receiving membrane pads; And
And a paddle rotation control unit coupled to the work gas receiving membrane pads and the camera module, the paddles being provided in the hull to rotationally drive the work gas receiving membrane pads so that the work gas pockets of the work gas receiving membrane pads can be moved in and out of the hull, And a driving unit,
The pad rotation driving unit includes:
A pad and a module support supporting the work gas accommodating membrane pad and the camera module, one side being hemispherical;
A waterproof rotary shaft connected to the pad and the module support to form a rotation axis of the pad and the module support; And
And a shaft rotating part connected to the waterproof rotary shaft to rotate the waterproof rotary shaft.
The shaft-
A rotary motor;
A driving gear connected to a motor shaft of the rotary motor; And
And a driven gear coupled to an end of the waterproof rotary shaft and meshing with the drive gear.
Wherein the camera module further comprises a module support coupled to the pad and the module support while supporting the camera.
Further comprising a seawater inflow preventing cover disposed inside the hull so as to surround the working gas receiving membrane pad to prevent inflow of seawater.
A drain portion is coupled to a side portion of the seawater inflow prevention cover,
And a detachable lid having a handle is provided on an upper portion of the cover for preventing seawater inflow.
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Cited By (1)
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KR20180135959A (en) * | 2017-01-31 | 2018-12-21 | 미츠비시 쥬고교 가부시키가이샤 | Duct devices and vessels |
Families Citing this family (1)
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KR101866916B1 (en) * | 2018-01-03 | 2018-06-14 | 한국해양과학기술원 | Water apparatus for usbl operation |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001001985A (en) | 1999-06-16 | 2001-01-09 | Nkk Corp | Propeller observing device |
JP2002264894A (en) * | 2001-03-07 | 2002-09-18 | Ishikawajima Harima Heavy Ind Co Ltd | Bottom structure of stern part |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH08188192A (en) | 1995-01-10 | 1996-07-23 | Mitsubishi Heavy Ind Ltd | Propeller fluctuating pressure absorbing device for marine vessel |
KR100688933B1 (en) | 2005-07-07 | 2007-03-02 | 주식회사 모아텍 | apparatus for gear protection of stepping motor |
CN106005241B (en) * | 2008-04-01 | 2018-06-19 | 国立研究开发法人海上·港湾·航空技术研究所 | The frictional resistance of ship reduces device |
JP4183048B1 (en) | 2008-04-17 | 2008-11-19 | 有限会社ランドエンジニアリング | Friction resistance reducing ship and its operating method |
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Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001001985A (en) | 1999-06-16 | 2001-01-09 | Nkk Corp | Propeller observing device |
JP2002264894A (en) * | 2001-03-07 | 2002-09-18 | Ishikawajima Harima Heavy Ind Co Ltd | Bottom structure of stern part |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20180135959A (en) * | 2017-01-31 | 2018-12-21 | 미츠비시 쥬고교 가부시키가이샤 | Duct devices and vessels |
KR102104195B1 (en) * | 2017-01-31 | 2020-05-29 | 미츠비시 쥬고교 가부시키가이샤 | Duct device and ship |
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