JPH0347237B2 - - Google Patents
Info
- Publication number
- JPH0347237B2 JPH0347237B2 JP58135481A JP13548183A JPH0347237B2 JP H0347237 B2 JPH0347237 B2 JP H0347237B2 JP 58135481 A JP58135481 A JP 58135481A JP 13548183 A JP13548183 A JP 13548183A JP H0347237 B2 JPH0347237 B2 JP H0347237B2
- Authority
- JP
- Japan
- Prior art keywords
- cavitation
- hydrofoil
- angle
- attack
- curve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
- B63B1/24—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
- B63B1/28—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils
- B63B1/285—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils changing the angle of attack or the lift of the foil
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Feedback Control In General (AREA)
Description
【発明の詳細な説明】
本発明は水中翼の制御方法に係り、更に詳しく
は、船体の横揺れを防ぐために船体に取付けられ
る水中翼の制御(操作)方法に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for controlling a hydrofoil, and more particularly to a method for controlling (operating) a hydrofoil attached to a ship's hull to prevent rolling of the ship.
船体の両舷に水中翼を取付て、これら水中翼に
生ずる揚力を利用して船体の横揺れの防止を図る
場合がある。このような目的に用いられる水中翼
を一般にフインスタビライザ等と称するが、従来
はこの種の水中翼を制御(操作)する場合、横揺
れを防止して船体姿勢を矯正することのみをもつ
ぱらの目的とし、水中翼に生ずるキヤビテーシヨ
ンの発生を防止するための何らの試みもなされて
いなかつた。そのため、水中翼の制御に伴い大き
なキヤビテーシヨンノイズが生じて、調査船等に
おいては水中音響機器の適正な使用の障害となる
等の不都合を招いていた。 In some cases, hydrofoils are attached to both sides of a ship, and the lifting force generated by these hydrofoils is used to prevent the ship from rolling. Hydrofoils used for this purpose are generally called fin stabilizers, etc., but conventionally, when controlling (operating) this type of hydrofoil, a separate stabilizer was used that only prevented rolling and corrected the hull attitude. No attempt has been made to prevent cavitation occurring in hydrofoils. As a result, large cavitation noise is generated as a result of controlling the hydrofoils, causing inconveniences such as hindering the proper use of underwater acoustic equipment on research vessels and the like.
本発明の目的は、キヤビテーシヨンノイズを発
生させない水中翼の制御方法を提供することにあ
る。 An object of the present invention is to provide a method for controlling a hydrofoil that does not generate cavitation noise.
そのため本発明は、あるキヤビテーシヨン数下
でキヤビテーシヨンを発生させる水中翼の迎角の
臨界角を示すキヤビテーシヨン初生曲線(その具
体的曲線形状は個々の水中翼の形状による)を予
め用意してマイクロコンピユータに記憶させる等
しておくとともに、前記船体に速度検出手段およ
び前記水中翼近傍の静圧検出手段を設置してお
き、船速及び水中翼に加わる静圧を圧力センサ
(静圧計)で計測し、マイクロコンピユータ等に
より現在時点でのキヤビテーシヨン数を算定し
て、求めたところの現在のキヤビテーシヨン数下
における水中翼の迎角のキヤビテーシヨン不発生
領域、つまりキヤビテーシヨンを発生させない水
中翼の迎角の範囲を前記キヤビテーシヨン初生曲
線を参照して定め、たとえば前記マイクロコンピ
ユータに水中翼の回転駆動機構を制御させる等し
て水中翼の迎角が常にキヤビテーシヨンを発生さ
せない状態下に維持されるようにして前記目的を
達成しようとするものである。 Therefore, the present invention prepares in advance a cavitation initiation curve (the specific curve shape depends on the shape of each hydrofoil) indicating the critical angle of the attack angle of a hydrofoil that causes cavitation to occur under a certain cavitation number, and stores it in a microcomputer. At the same time, a speed detection means and a static pressure detection means near the hydrofoil are installed in the hull, and the ship speed and the static pressure applied to the hydrofoil are measured with a pressure sensor (static pressure gauge). Calculate the current cavitation number using a microcomputer, etc., and calculate the cavitation-free range of the angle of attack of the hydrofoil under the current cavitation number, that is, the range of the angle of attack of the hydrofoil in which cavitation does not occur. The above objective is achieved by determining the cavitation initiation curve with reference to the curve, and by having the microcomputer control the rotary drive mechanism of the hydrofoil, so that the angle of attack of the hydrofoil is always maintained in a state where cavitation does not occur. This is what I am trying to do.
以下、本発明の実施例を図面に基づいて説明す
る。 Embodiments of the present invention will be described below based on the drawings.
第1,2図において船体1の水中部分の両舷に
は夫々水中翼2が設けられ、各水中翼2は、第3
図に示されるように、回転軸3を介して回転駆動
機構4が連結され、水中翼2には回転駆動機構4
によりその迎角αが調整可能とされている。 In FIGS. 1 and 2, hydrofoils 2 are provided on both sides of the underwater part of the hull 1, and each hydrofoil 2 has a third
As shown in the figure, a rotational drive mechanism 4 is connected via a rotation shaft 3, and the rotational drive mechanism 4 is connected to the hydrofoil 2.
The angle of attack α can be adjusted.
水中翼2のたとえば上流(船首側)の近傍には
レーザードツプラー流速計(LDV)やピトー管
等の船速検出手段5、及び、水中翼2に加わる静
圧Pを計測する圧力センサ(静圧計)6が配置さ
れている。また、前記回転軸3にはポテンシヨメ
ータ等の迎角検出手段7が取付られており、この
手段7により水中翼2の迎角αが計測されるよう
構成されている。ここで、迎角αとは水中翼2と
流れ方向となす角である。 For example, near the upstream (bow side) of the hydrofoil 2, there is a ship speed detection means 5 such as a laser Doppler velocity meter (LDV) or a pitot tube, and a pressure sensor (static pressure sensor) that measures the static pressure P applied to the hydrofoil 2. A pressure gauge) 6 is arranged. Further, an angle of attack detection means 7 such as a potentiometer is attached to the rotating shaft 3, and the angle of attack α of the hydrofoil 2 is measured by this means 7. Here, the angle of attack α is the angle between the hydrofoil 2 and the flow direction.
第4図には本実施例における制御系統が示され
ている。図中、船速検出手段5、圧力センサ(静
圧計)6、迎角検出手段7はマイクロコンピユー
タ8に接続され、各手段5,7及び静圧計6の
夫々で検出された各値は逐次マイクロコンピユー
タ8へと送られるようになつている。またマイク
ロコンピユータ8には回転駆動機構4が接続さ
れ、駆動機構4へ駆動信号が送られ、これにより
水中翼2の迎角αはマイクロコンピユータ8の指
令に基づいて制御されるようになつている。 FIG. 4 shows the control system in this embodiment. In the figure, a ship speed detection means 5, a pressure sensor (static pressure gauge) 6, and an angle of attack detection means 7 are connected to a microcomputer 8, and each value detected by each means 5, 7 and static pressure gauge 6 is sequentially The data is sent to the computer 8. Further, a rotational drive mechanism 4 is connected to the microcomputer 8, and a drive signal is sent to the drive mechanism 4, whereby the angle of attack α of the hydrofoil 2 is controlled based on commands from the microcomputer 8. .
マイクロコンピユータ8は演算機能を有し、キ
ヤビテーシヨン数σが算出されるようになつてい
る。ここで、キヤビテーシヨン数σとは
キヤビテーシヨン数σ=P/1/2ρV2
で定義される数であり、ρは水の密度であるか
ら、この密度ρを定数とみなせば、前記船速検出
手段5により検出される船速Vと、前記静圧計6
で計測される静圧Pとがマイクロコンピユータ8
に送られることによりキヤビテーシヨン数σが逐
次算出されることとなる。 The microcomputer 8 has an arithmetic function and is adapted to calculate the cavitation number σ. Here, the cavitation number σ is a number defined by cavitation number σ=P/1/2ρV 2 , and since ρ is the density of water, if this density ρ is regarded as a constant, then the ship speed detection means 5 The ship speed V detected by the static pressure gauge 6
The static pressure P measured by the microcomputer 8
As a result, the cavitation number σ is calculated sequentially.
また、マイクロコンピユータ8には第5図に示
されるようなキヤビテーシヨン初生曲線が予め記
憶されている。このキヤビテーシヨン初生曲線と
は、具体的には水中翼2の形状によつて定まり、
あるキヤビテーシヨン数σ下でキヤビテーシヨン
を発生させる水中翼2の迎角αの臨界角を示す曲
線であり、図中、キヤビテーシヨン初生曲線の下
側(迎角αの軸側)はキヤビテーシヨン発生領域
であり、キヤビテーシヨン初生曲線の上側はキヤ
ビテーシヨン不発生領域である。 Further, the microcomputer 8 stores in advance a cavitation initial curve as shown in FIG. This cavitation initial curve is specifically determined by the shape of the hydrofoil 2,
This is a curve showing the critical angle of the angle of attack α of the hydrofoil 2 that causes cavitation to occur under a certain cavitation number σ, and in the figure, the lower side of the cavitation initiation curve (the axial side of the angle of attack α) is the cavitation generation region, The upper side of the cavitation initiation curve is a region where cavitation does not occur.
次に、第5図を参照しながら本実施例の作用に
つき説明する。 Next, the operation of this embodiment will be explained with reference to FIG.
今、船体1が速度Viで航走し水中翼2には静
圧Piが加わつているとする。本システムを作動さ
せると、このときのキヤビテーシヨン数σiはマイ
クロコンピユータ8にて
σi=Pi/1/2ρVi2
の式より算出される。このように算出されたキヤ
ビテーシヨン数σi下における水中翼2の迎角αの
臨界角は、図中σ=σiの直線と前記キヤビテーシ
ヨン初生曲線との交点である、S点より求まり、
このとき、迎角αの臨界角はαsであつたとする。 Now, assume that the hull 1 is traveling at a speed Vi and a static pressure Pi is applied to the hydrofoil 2. When this system is operated, the cavitation number σi at this time is calculated by the microcomputer 8 using the formula σi=Pi/1/2ρVi 2 . The critical angle of the angle of attack α of the hydrofoil 2 under the cavitation number σi calculated in this way is determined from the point S, which is the intersection of the straight line σ=σi in the figure and the cavitation initiation curve,
At this time, assume that the critical angle of the angle of attack α is αs.
一方、実際の(現時点での)迎角αは前記迎角
検出手段7により検出され、この検出された実際
の迎角αとキヤビテーシヨン初生曲線を参照して
求められた迎角αの臨界角αsとを比較し、たと
えば、実際の迎角が第5図中A点で示されるとこ
ろのαAであつたとすれば、迎角αを矯正して図
中B点で示される迎角αBとなるようマイクロコ
ンピユータ8から回転駆動機構4へと駆動信号を
発して水中翼2の迎角αを調整する。これによ
り、水中翼2の迎角αはキヤビテーシヨン発生領
域から脱してキヤビテーシヨン不発生領域内へと
移行され、キヤビテーシヨン発生が防止されるこ
ととなる。 On the other hand, the actual (current) angle of attack α is detected by the angle of attack detection means 7, and the critical angle αs of the angle of attack α is determined by referring to the detected actual angle of attack α and the cavitation initiation curve. For example, if the actual angle of attack is αA shown at point A in Figure 5, then the angle of attack α can be corrected to become the angle of attack αB shown at point B in the figure. A drive signal is issued from the microcomputer 8 to the rotational drive mechanism 4 to adjust the angle of attack α of the hydrofoil 2. As a result, the angle of attack α of the hydrofoil 2 moves out of the cavitation occurrence region and into the cavitation non-occurrence region, and cavitation occurrence is prevented.
このような本実施例によれば、キヤビテーシヨ
ン発生が回避されるため、キヤビテーシヨンノイ
ズの発生を有効に防止させることができる。従つ
て、水中音響機器等の使用に際しても何らの障害
が生ずることがない。 According to this embodiment, since the occurrence of cavitation is avoided, the occurrence of cavitation noise can be effectively prevented. Therefore, no trouble will occur when using underwater acoustic equipment or the like.
なお、キヤビテーシヨン初生曲線は水中翼2の
形状により具体的に実験等により定まるものであ
り、従つて、キヤビテーシヨン初生曲線は第5図
に示される形状のものに限られるわけではない。
また、前述においては水の密度ρを定数とした
が、一層正確な制御を行うために、水の密度ρを
も検出してキヤビテーシヨン数σの算出に用いて
もよい。また、静圧Pの算出についても水の飽和
蒸気圧を考慮するものであつてもよい。さらに、
マイクロコンピユータ8により自動制御を行なう
場合に限らず、マニユアル操作、あるいは半マニ
ユアル操作を行なつてもよい。 Note that the cavitation initial curve is determined specifically through experiments and the like depending on the shape of the hydrofoil 2, and therefore, the cavitation initial curve is not limited to the shape shown in FIG.
Further, in the above description, the density ρ of water was taken as a constant, but in order to perform more accurate control, the density ρ of water may also be detected and used for calculating the cavitation number σ. Further, the calculation of the static pressure P may also take into account the saturated vapor pressure of water. moreover,
The automatic control is not limited to the microcomputer 8, but manual or semi-manual operation may also be performed.
上述のように本発明によればキヤビテーシヨン
ノイズを発生させることのない水中翼の制御方法
を提供できる。 As described above, according to the present invention, it is possible to provide a hydrofoil control method that does not generate cavitation noise.
第1図は本発明に係る水中翼の制御方法が適用
される船体の一実施例を示す正面図、第2図はそ
の平面図、第3図は前記実施例が適用される制御
装置の概略構成を示す拡大断面図、第4図は前記
実施例の制御系統図、第5図はキヤビテーシヨン
初生曲線の一例を示す線図である。
2……水中翼、3……回転軸、4……回転駆動
機構、5……船速検出手段、6……圧力センサ
(静圧計)、7……迎角検出手段。
Fig. 1 is a front view showing an embodiment of a ship body to which the hydrofoil control method according to the present invention is applied, Fig. 2 is a plan view thereof, and Fig. 3 is a schematic diagram of a control device to which the above embodiment is applied. FIG. 4 is a control system diagram of the embodiment, and FIG. 5 is a diagram showing an example of a cavitation initial curve. 2...Hydrofoil, 3...Rotary shaft, 4...Rotary drive mechanism, 5...Ship speed detection means, 6...Pressure sensor (static pressure gauge), 7...Angle of attack detection means.
Claims (1)
迎角を調整可能な水中翼の制御方法であつて、 あるキヤビテーシヨン数下でキヤビテーシヨン
を発生させる水中翼の迎角の臨界角を示すキヤビ
テーシヨン初生曲線を予め用意するとともに、前
記船体に速度検出手段および前記水中翼近傍の静
圧検出手段を設置しておき、 航行中の船速および水中翼に加わる静圧を計測
してキヤビテーシヨン数を求め、求めたキヤビテ
ーシヨン数下における水中翼の迎角のキヤビテー
シヨン不発生領域を前記キヤビテーシヨン初生曲
線を参照して定め、前記水中翼を定めたキヤビテ
ーシヨン不発生領域で作動させることを特徴とす
る水中翼の制御方法。[Scope of Claims] 1. A method for controlling a hydrofoil provided on a ship hull that can adjust the angle of attack in order to prevent rolling of the ship body, the method comprising: determining the critical angle of the angle of attack of the hydrofoil that causes cavitation to occur under a certain cavitation number; In addition to preparing in advance a cavitation initiation curve showing A cavitation-free area of the angle of attack of the hydrofoil under the calculated cavitation number is determined with reference to the cavitation initiation curve, and the hydrofoil is operated in the determined cavitation-free area. How to control the wings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58135481A JPS6025878A (en) | 1983-07-25 | 1983-07-25 | Control of hydrofoil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58135481A JPS6025878A (en) | 1983-07-25 | 1983-07-25 | Control of hydrofoil |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6025878A JPS6025878A (en) | 1985-02-08 |
| JPH0347237B2 true JPH0347237B2 (en) | 1991-07-18 |
Family
ID=15152722
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58135481A Granted JPS6025878A (en) | 1983-07-25 | 1983-07-25 | Control of hydrofoil |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6025878A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0623519Y2 (en) * | 1985-06-25 | 1994-06-22 | 三菱重工業株式会社 | Marine fin stabilizer |
| JPH02120759A (en) * | 1988-10-28 | 1990-05-08 | Minolta Camera Co Ltd | Copying machine |
| JP2547376Y2 (en) * | 1990-05-23 | 1997-09-10 | 三菱重工業株式会社 | Hull damper fin drive controller |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58861B2 (en) * | 1975-07-28 | 1983-01-08 | イズミ マサヒコ | Kiyoseitai Ryuushikimameruitan Kijiyoushi Yahouhou |
-
1983
- 1983-07-25 JP JP58135481A patent/JPS6025878A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6025878A (en) | 1985-02-08 |
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