JPH06305413A - Side wall type air cushion hydrofoil craft - Google Patents

Side wall type air cushion hydrofoil craft

Info

Publication number
JPH06305413A
JPH06305413A JP12091293A JP12091293A JPH06305413A JP H06305413 A JPH06305413 A JP H06305413A JP 12091293 A JP12091293 A JP 12091293A JP 12091293 A JP12091293 A JP 12091293A JP H06305413 A JPH06305413 A JP H06305413A
Authority
JP
Japan
Prior art keywords
hydrofoil
hull
air cushion
side wall
type air
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.)
Withdrawn
Application number
JP12091293A
Other languages
Japanese (ja)
Inventor
Yusuke Takagi
祐介 高木
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP12091293A priority Critical patent/JPH06305413A/en
Publication of JPH06305413A publication Critical patent/JPH06305413A/en
Withdrawn legal-status Critical Current

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Abstract

PURPOSE:To prevent a side wall type air cushion hydrofoil craft, which is provided with a hydrofoil to control the attitude of the hull, from being subjected to excessive bending force at the hydrofoil mounted portion by giving a level difference especially between a water level in an air cushion room and a water level outside the hull. CONSTITUTION:In a craft which has an air cushion room 5 between mutually right and left body side walls 3, 3, a hydrofoil 4 located at the lower end of the hull side wall 3 to control the attitude of the hull is formed with the outside portion 4a and the inside portion 4b. The hydrofoil area of the inside portion 4a is formed larger than that of the outside portion 4a or the flap operation angle of the inside portion 4b is controlled greater than that of the outside portion 4a so that the outside portion 4a and the inside portion 4b of the hydrofoil can have almost the same lift, whether there is a level difference between a water level 1 outside the hull and a water level 2 in the air cushion room 5 or not.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、左右の船体側壁の相互
間にエアクッション室をそなえた側壁型エアクッション
船に関し、特に航走中に船体の姿勢を制御するための水
中翼をそなえた水中翼付き側壁型エアクッション船に関
する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a side wall type air cushion ship having an air cushion chamber between the left and right side walls of a hull, and more particularly to a hydrofoil for controlling the attitude of the hull during sailing. The present invention relates to a sidewall type air cushion ship with hydrofoils.

【0002】[0002]

【従来の技術】従来の水中翼付き側壁型エアクッション
船としては図5(a),(b),(c)に示すようなものがあ
り、図5(a)はその船体横断面図、図5(b)はその水中
翼装着部分の側面図、図5(c)はその水中翼装着部分の
平面図である。図5(a)〜(c)に示すように、左右の船
体側壁部3,3の相互間に船体重量の一部を支持するた
めのエアクッション室5が形成されて、図示しない高圧
空気供給手段に接続されている。そして、左右の船体側
壁部3,3の各下端には、支柱6を介して船体姿勢制御
用の水中翼4,4が別個に支持されている。
2. Description of the Related Art There is a conventional side wall type air cushion ship with hydrofoil as shown in FIGS. 5 (a), 5 (b) and 5 (c). FIG. 5 (b) is a side view of the hydrofoil mounting portion, and FIG. 5 (c) is a plan view of the hydrofoil mounting portion. As shown in FIGS. 5 (a) to 5 (c), an air cushion chamber 5 for supporting a part of the weight of the hull is formed between the left and right hull side wall parts 3 and 3, and a high pressure air supply (not shown) is formed. Connected to the means. Further, hydrofoils 4 and 4 for hull attitude control are separately supported at the lower ends of the left and right hull side wall parts 3 and 3 via struts 6.

【0003】[0003]

【発明が解決しようとする課題】ところで、前述のよう
な従来の水中翼付き側壁型エアクッション船では、水中
翼4の支柱6による取付け部から外側方へ延在する水中
翼外側部分4aと同取付け部から内側方へ延在する水中
翼内側部分4bとが同じ翼面積を有しているが、船体の
航走中には船体外側水面1に比べてエアクッション室5
内の水面2のレベルが低くなるため、水中翼外側部分4
aの方が、没水深さの浅くなる水中翼内側部分4bより
も大きい揚力を生じ、これにより支柱6による水中翼4
の取付け部に曲げ力が働くという問題点がある。
By the way, in the conventional side wall type air cushion ship with hydrofoil as described above, the hydrofoil 4 has the same outer part 4a as the hydrofoil outer part 4a which extends outward from the mounting part of the hydrofoil 4 by the column 6. Although the hydrofoil inner part 4b extending inward from the mounting portion has the same wing area, the air cushion chamber 5 is larger than the water surface 1 on the outer side of the hull while the hull is in motion.
Since the level of the water surface 2 inside becomes low, the hydrofoil outer part 4
a produces a larger lift than the inner portion 4b of the hydrofoil where the submersion depth becomes shallower, and as a result, the hydrofoil 4 by the support column 6 is generated.
There is a problem that bending force acts on the attachment part of.

【0004】本発明は、このような問題点の解消をはか
ろうとするもので、左右の船体側壁部の各下端に別個に
取付けられる水中翼の外側部分と内側部分とが、船体の
航走中に船体外側水面とエアクッション室内の水面との
レベル差に拘らず同程度の揚力を発生するようにして、
水中翼取付け部に働く曲げ力を極力小さくできるように
した水中翼付き側壁型エアクッション船を提供すること
を目的とする。
The present invention is intended to solve such problems, and the outer portion and the inner portion of the hydrofoil, which are separately attached to the lower ends of the left and right side wall portions of the hull, respectively, are the navigation of the hull. The same level of lift force is generated regardless of the level difference between the water surface outside the hull and the water surface inside the air cushion room.
An object of the present invention is to provide a sidewall-type air cushion ship with a hydrofoil in which the bending force acting on the hydrofoil mounting portion can be minimized.

【0005】[0005]

【課題を解決するための手段】上述の目的を達成するた
め、本発明の水中翼付き側壁型エアクッション船は、左
右の船体側壁部の相互間にエアクッション室をそなえる
とともに、上記船体側壁部の各下端に別個に支持されて
左右に対をなす船体姿勢制御用水中翼をそなえ、同水中
翼が上記船体側壁部の下端への取付け部から外側方へ延
在する水中翼外側部分と上記取付け部から内側方へ延在
する水中翼内側部分とで構成されて、航走中における上
記エアクッション室内の水面と船体外側水面とのレベル
差に拘らず上記の水中翼外側部分と水中翼内側部分とが
同じ翼角でほぼ同等の揚力を発生すべく、上記水中翼内
側部分が上記水中翼外側部分よりも広い翼面積を有して
いることを特徴としている。
In order to achieve the above-mentioned object, a side wall type air cushion ship with hydrofoil of the present invention has an air cushion chamber between the left and right hull side wall parts and the hull side wall part. And a pair of left and right hull attitude control hydrofoils supported separately at each lower end of the hull, and the hydrofoil outer part extending outward from the attachment part to the lower end of the hull side wall and the hydrofoil outer part described above. The inner part of the hydrofoil that extends inward from the mounting part, and the outer part of the hydrofoil and the inner part of the hydrofoil regardless of the level difference between the water surface inside the air cushion chamber and the water surface outside the hull during navigation. The inside portion of the hydrofoil has a larger blade area than the outside portion of the hydrofoil so that the portions generate substantially the same lift at the same blade angle.

【0006】また、本発明の水中翼付き側壁型エアクッ
ション船は、上記水中翼内側部分が上記水中翼外側部分
よりも大きい翼幅を有していることを特徴としている。
さらに、本発明の水中翼付き側壁型エアクッション船
は、上記水中翼内側部分が上記水中翼外側部分よりも大
きい翼弦長さを有していることを特徴としている。
Further, the side wall type air cushion ship with hydrofoil of the present invention is characterized in that the inner part of the hydrofoil has a larger wing width than the outer part of the hydrofoil.
Further, the sidewall-type air cushion ship with hydrofoil of the present invention is characterized in that the inner part of the hydrofoil has a larger chord length than the outer part of the hydrofoil.

【0007】また、本発明の水中翼付き側壁型エアクッ
ション船は、左右の船体側壁部の相互間にエアクッショ
ン室をそなえるとともに、上記船体側壁部の各下端に別
個に支持されて左右に対をなす船体姿勢制御用水中翼を
そなえ、同水中翼が上記船体側壁部の下端への取付け部
から外側方へ延在するフラップ付き水中翼外側部分と上
記取付け部から内側方へ延在するフラップ付き水中翼内
側部分とで構成されて、航走中における上記エアクッシ
ョン室内の水面と船体外側水面とのレベル差に拘らず上
記の水中翼外側部分と水中翼内側部分とがほぼ同等の揚
力を発生すべく上記水中翼外側部分におけるフラップの
作動角と上記水中翼内側部分におけるフラップの作動角
とを別個に制御するフラップ制御系が設けられたことを
特徴としている。
Further, the side wall type air cushion ship with hydrofoil of the present invention is provided with an air cushion chamber between the left and right side wall portions of the hull, and is supported separately at each lower end of the side wall portion of the hull and is opposed to the left and right sides. A hydrofoil for controlling the attitude of the hull, the hydrofoil having a flap extending outward from an attachment portion to the lower end of the side wall of the hull and a flap extending inward from the attachment portion. The inner part of the hydrofoil and the inner part of the hydrofoil have almost the same lift regardless of the level difference between the water surface inside the air cushion chamber and the water surface outside the hull. It is characterized in that a flap control system for separately controlling the operating angle of the flap in the outer portion of the hydrofoil and the operating angle of the flap in the inner portion of the hydrofoil to be generated is provided.

【0008】[0008]

【作用】上述の本発明の水中翼付き側壁型エアクッショ
ン船では、航走中にエアクッション室における水面のレ
ベルが船体外側水面よりも低くなるが、水中翼外側部分
と水中翼内側部分とは同じ翼角でほぼ同等の揚力を発生
できるように、水中翼内側部分が水中翼外側部分よりも
広い翼面積を有しているので、水中翼取付け部に働く曲
げ力を十分に低減させる作用が行なわれる。また、水中
翼内側部分におけるフラップの作動角と水中翼外側部分
におけるフラップの作動角とを別個に制御するフラップ
制御系を有する場合も、航走中におけるエアクッション
室内の水面と船体外側水面とのレベル差に拘らず水中翼
外側部分と水中翼内側部分とがほぼ同等の揚力を発生す
るように上記制御系によるフラップ制御が行なわれるの
で、水中翼取付け部に働く曲げ力が低減されるようにな
る。
In the above-described side wall type air cushion ship with hydrofoils of the present invention, the level of the water surface in the air cushion chamber becomes lower than the water surface on the outer side of the hull during traveling. Since the inner part of the hydrofoil has a larger blade area than the outer part of the hydrofoil so that almost the same lift can be generated with the same blade angle, it has the effect of sufficiently reducing the bending force acting on the hydrofoil attachment part. Done. In addition, even if there is a flap control system that separately controls the operating angle of the flap on the inside portion of the hydrofoil and the operating angle of the flap on the outside portion of the hydrofoil, the water surface inside the air cushion chamber and the water surface outside the hull during navigation are Since the flap control by the above control system is performed so that the outer portion of the hydrofoil and the inner portion of the hydrofoil generate almost the same lift force regardless of the level difference, the bending force acting on the hydrofoil mounting portion is reduced. Become.

【0009】[0009]

【実施例】以下、図面により本発明の実施例について説
明すると、図1(a),(b)は、本発明の第1実施例とし
ての水中翼付き側壁型エアクッション船を示すもので、
図1(a)はその船体横断面図、図1(b)はその水中翼装
着部分の側面図である。図1(a),(b)に示すように、
左右の船体側壁部3,3の相互間に船体重量の一部を支
持するためのエアクッション室5が形成されて、図示し
ない高圧空気供給手段に接続されている。
Embodiments of the present invention will now be described with reference to the drawings. FIGS. 1 (a) and 1 (b) show a side wall type air cushion ship with hydrofoil as a first embodiment of the present invention.
1 (a) is a cross-sectional view of the hull, and FIG. 1 (b) is a side view of the hydrofoil mounting portion. As shown in FIGS. 1 (a) and 1 (b),
An air cushion chamber 5 for supporting a part of the hull weight is formed between the left and right hull side wall parts 3, 3 and is connected to a high pressure air supply means (not shown).

【0010】そして、左右の船体側壁部3,3の各下端
に支柱6を介し別個に支持されて左右に対をなす船体姿
勢制御用水中翼4,4が装備されている。各水中翼4
は、支柱6による船体側壁部3下端への取付け部から外
側方へ延在する水中翼外側部分4aと、上記の取付け部
から内側方へ延在する水中翼内側部分4bとで構成され
て、航走中におけるエアクッション室5内の水面2と船
体外側水面1とのレベル差に拘らず水中翼外側部分4a
と水中翼内側部分4bとが同じ翼角でほぼ同等の揚力を
発生できるように、水中翼内側部分4bが水中翼外側部
分4aよりも5〜20%程度広い翼面積を有している。
Further, watercraft wings 4 and 4 for hull attitude control, which are separately supported via pillars 6 and are paired to the left and right, are provided at the lower ends of the left and right hull side wall portions 3 and 3, respectively. Each hydrofoil 4
Is composed of a hydrofoil outer portion 4a extending outward from an attachment portion to the lower end of the hull side wall portion 3 by the support column 6 and a hydrofoil inner portion 4b extending inward from the attachment portion. The outer portion 4a of the hydrofoil regardless of the level difference between the water surface 2 in the air cushion chamber 5 and the water surface 1 on the outer side of the hull during traveling.
The inner portion 4b of the hydrofoil has a larger blade area than the outer portion 4a of the hydrofoil by about 5 to 20% so that the and the inner portion 4b of the hydrofoil can generate almost the same lift at the same blade angle.

【0011】すなわち図1(a),(b)に示す第1実施例で
は水中翼4の外側部分4aと内側部分4bとは同じ翼弦
長さを有しているが、翼幅は水中翼内側部分4bの方が
水中翼外側部分4aよりも5〜20%程度大きく形成され
ている。なお、ここでいう翼角とは、水中翼全体を回動
制御する場合の作動角と、可動フラップを設けた場合の
フラップ作動角とのいずれも含むものとする。
That is, in the first embodiment shown in FIGS. 1 (a) and 1 (b), the outer portion 4a and the inner portion 4b of the hydrofoil 4 have the same chord length, but the width is the hydrofoil. The inner portion 4b is formed to be larger than the hydrofoil outer portion 4a by about 5 to 20%. The blade angle here includes both an operating angle for controlling the rotation of the entire hydrofoil and a flap operating angle for providing a movable flap.

【0012】上述の構成により、この第1実施例では、
航走中にエアクッション室5における高圧空気で同エア
クッション室5内の水面2が押し下げられて船体外側水
面1のレベルよりも低くなっても、すなわち、水中翼内
側部分4bの没水深さが水中翼外側部分4aより浅くな
っても、両部分4a、4bに生じる揚力は同じ翼角制御
でほぼ同等となり、このようにして、支柱6による水中
翼4の取付け部に働く曲げ力が十分に低減されるのであ
る。また、水中翼外側部分4aと水中翼内側部分4bと
は同じ翼弦長さを有しているので、翼角制御のための構
成が簡易化される利点もある。
With the above-mentioned structure, in the first embodiment,
Even when the water surface 2 in the air cushion chamber 5 is pushed down by the high-pressure air in the air cushion chamber 5 during traveling and becomes lower than the level of the water surface 1 on the outer side of the hull, that is, the submersible depth of the inner portion 4b of the hydrofoil is reduced. Even if it becomes shallower than the outer part 4a of the hydrofoil, the lifts generated in both parts 4a, 4b become almost equal by the same blade angle control, and in this way, the bending force exerted on the mounting part of the hydrofoil 4 by the support column 6 is sufficient. It is reduced. Further, since the hydrofoil outer portion 4a and the hydrofoil inner portion 4b have the same chord length, there is also an advantage that the configuration for controlling the blade angle is simplified.

【0013】図2(a),(b)は本発明の第2実施例を示し
ており、船体要部の横断面図としての図2(a)とその水
中翼取付け部の平面図としての図2(b)から明らかなよ
うに、この第2実施例では水中翼外側部分4aと水中翼
内側部分4bとは同じ大きさの翼幅を有しているが、水
中翼内側部分4bの方の方が水中翼外側部分4aよりも
5〜20%大きい翼弦長さを有している。このようにし
て、この第2実施例では水中翼内側部分4bは水中翼外
側部分4aよりも大きい翼面積を有していて、エアクッ
ション室5内の水面2と船体外側水面1とのレベル差に
拘らず水中翼外側部分4aと水中翼内側部分4bとは同
じ翼角制御でほぼ同じ揚力を発生するように構成されて
いる。
FIGS. 2 (a) and 2 (b) show a second embodiment of the present invention. FIG. 2 (a) is a cross-sectional view of the main part of the hull and a plan view of its hydrofoil mounting part. As is apparent from FIG. 2 (b), in this second embodiment, the hydrofoil outer portion 4a and the hydrofoil inner portion 4b have the same wingspan, but the hydrofoil inner portion 4b is the same. Has a chord length which is 5 to 20% larger than the hydrofoil outer portion 4a. Thus, in this second embodiment, the hydrofoil inner portion 4b has a larger blade area than the hydrofoil outer portion 4a, and the level difference between the water surface 2 in the air cushion chamber 5 and the water surface 1 on the outer side of the hull is shown. Regardless, the hydrofoil outer part 4a and the hydrofoil inner part 4b are configured to generate substantially the same lift force with the same blade angle control.

【0014】したがって、この第2実施例の場合も前述
の第1実施例と同様に水中翼4の取付け部に働く曲げ力
を極力低減させる効果が得られるほか、水中翼内側部分
4bのエアクッション室5側への突出量を大きくしない
ですむ利点がある。なお、上述の第1実施例および第2
実施例では、水中翼4が翼角制御を行なえるようにした
ものとして説明したが、各水中翼4を固定式にした場合
も、船体の傾きに応じて各水中翼4に働く水の反力で、
船体の姿勢の復原が行なわれるようになる。
Therefore, in the case of the second embodiment as well, the effect of reducing the bending force acting on the mounting portion of the hydrofoil 4 as much as possible as in the case of the first embodiment described above is obtained, and the air cushion of the hydrofoil inner portion 4b is obtained. There is an advantage that the amount of protrusion to the chamber 5 side does not have to be large. The first embodiment and the second embodiment described above
In the embodiment, the hydrofoil 4 is described as being capable of controlling the blade angle. However, even when each hydrofoil 4 is fixed, the reaction of water acting on the hydrofoil 4 depending on the inclination of the hull is prevented. By force,
The attitude of the hull will be restored.

【0015】図3(a),(b)は本発明の第3実施例として
の水中翼付き側壁型エアクッション船における水中翼の
フラップ角制御状態を示すもので、図3(a)はその水中
翼外側部分のフラップ角制御状態を示す翼断面図、図3
(b)はその水中翼内側部分のフラップ角制御状態を示す
翼断面図である。この第3実施例の水中翼付き側壁型エ
アクッション船は、前述の第1および第2実施例の場合
とほぼ同様の船体構成を有しているが、水中翼4を構成
する水中翼外側部分4aおよび水中翼内側部分4bはほ
ぼ同じ翼面積を有し、共に可動フラップ4af、4bf
をそなえている。
FIGS. 3 (a) and 3 (b) show a flap angle control state of a hydrofoil in a sidewall type air cushion ship with hydrofoil as a third embodiment of the present invention, and FIG. FIG. 3 is a blade cross-sectional view showing a flap angle control state of an outer portion of the hydrofoil.
(b) is a blade cross-sectional view showing a flap angle control state of the inner portion of the hydrofoil. The sidewall-type air cushion ship with hydrofoil of the third embodiment has substantially the same hull structure as in the above-described first and second embodiments, but the hydrofoil outer part constituting the hydrofoil 4 is formed. 4a and hydrofoil inner part 4b have substantially the same blade area, and both movable flaps 4af, 4bf
It has

【0016】そして、航走中におけるエアクッション室
内の水面と船体外側水面とのレベル差に拘らず水中翼外
側部分4aと水中翼内側部分4bとがほぼ同じ揚力を発
生できるように、水中翼外側部分4aにおけるフラップ
4afの作動角αと水中翼内側部分4bにおけるフラッ
プ4bfの作動角βとを別個に制御するフラップ制御系
をそなえている。図4は上記フラップ制御系の一例を示
すブロック図であって、例えば船体が左舷側へ傾斜した
場合、船体姿勢検出計からの検出信号により、左舷水中
翼では正の揚力の発生が要求され、右舷水中翼では負の
揚力の発生が要求されるようになる。
Outside the hydrofoil so that the hydrofoil outer part 4a and the hydrofoil inner part 4b can generate almost the same lift regardless of the level difference between the water surface inside the air cushion chamber and the water surface outside the hull during traveling. A flap control system for separately controlling the operating angle α of the flap 4af in the portion 4a and the operating angle β of the flap 4bf in the hydrofoil inner portion 4b is provided. FIG. 4 is a block diagram showing an example of the flap control system. For example, when the hull inclines to the port side, a detection signal from the hull attitude detector requires the port hydrofoil to generate a positive lift. The starboard hydrofoil will be required to generate negative lift.

【0017】そして、左舷水中翼および右舷水中翼の各
フラップ制御器からの制御信号は、エアクッション室内
の水面と船体外側水面とのレベル差を検出するレベル差
検出計からの検出信号に応じ調整器で調整されて、水中
翼外側部分フラップ用アクチュエータと水中翼内側部分
フラップ用アクチュエータとに別個に送られる。これに
より没水深度の浅い水中翼内側部分のフラップ作動角
は、没水深度の深い水中翼外側部分のフラップ作動角よ
りも大きくなるように制御されて、水中翼内側部分と水
中翼外側部分とはほぼ同じ揚力を発生するようになり、
このようにして水中翼取付け部における曲げ力の低減化
がもたらされるのである。上述のように、この第3実施
例では、フラップ付き水中翼外側部分4aとフラップ付
き水中翼内側部分とについて、フラップ制御系を個別化
することにより、各フラップを同形同大にしながら、内
外水面のレベル差に拘らず同じ揚力を発生できるように
フラップ制御を行なって、水中翼取付け部における過大
な曲げ力の発生を回避できる利点がある。
The control signals from the flap controllers on the port-side hydrofoil and the starboard-side hydrofoil are adjusted according to the detection signal from the level difference detector that detects the level difference between the water surface inside the air cushion chamber and the water surface outside the hull. And is separately fed to the hydrofoil outer partial flap actuator and the hydrofoil inner partial flap actuator. As a result, the flap working angle of the inner part of the hydrofoil with a shallow submersion depth is controlled so as to be larger than the flap working angle of the outer part of the hydrofoil with a deep submersion depth. Will generate almost the same lift,
In this way, the bending force at the hydrofoil attachment is reduced. As described above, in the third embodiment, the flap control system is individualized for the hydrofoil outer portion 4a with flaps and the hydrofoil inner portion with flaps, so that the flaps have the same shape and the same size. There is an advantage that flap control is performed so that the same lift force can be generated regardless of the level difference of the water surface, and generation of an excessive bending force at the hydrofoil mounting portion can be avoided.

【0018】[0018]

【発明の効果】以上詳述したように、本発明の水中翼付
き側壁型エアクッション船によれば、次のような効果が
得られる。 (1) 水中翼外側部分に比べて水中翼内側部分が広い翼面
積を有して、内外水面のレベル差に拘らず両部分が同じ
翼角でほぼ同じ揚力を発生するように構成されているの
で、水中翼取付け部分に過大な曲げ力が発生するのを回
避できる。 (2) 水中翼内側部分が広い翼面積をもつための手段とし
て、同水中翼内側部分が水中翼外側部分よりも大きい翼
幅を有している場合は、両部分の翼弦長さを等しくして
翼角制御のための構成を簡易化することができる。 (3) 水中翼内側部分が広い翼面積をもつための手段とし
て、同水中翼内側部分が水中翼外側部分よりも大きい翼
弦長さを有している場合は、同水中翼内側部分のエアク
ッション室側への突出量を大きくしないですむ利点があ
る。 (4) フラップ付き水中翼外側部分とフラップ付き水中翼
内側部分とについて、フラップ制御系を個別化すること
により、各フラップを同形同大にしながら、内外水面の
レベル差に拘らず同じ揚力を発生できるようにフラップ
制御を行なって、水中翼取付け部における過大な曲げ力
の発生を回避できる利点がある。
As described in detail above, according to the sidewall type air cushion ship with hydrofoil of the present invention, the following effects can be obtained. (1) The inner part of the hydrofoil has a larger blade area than the outer part of the hydrofoil, and both parts generate almost the same lift at the same blade angle regardless of the level difference between the inner and outer water surfaces. Therefore, it is possible to avoid the generation of an excessive bending force in the hydrofoil mounting portion. (2) If the inner part of the hydrofoil has a larger span than the outer part of the hydrofoil, the chord length of both parts should be the same as a means to make the inner part of the hydrofoil have a large blade area. Thus, the configuration for controlling the blade angle can be simplified. (3) If the inner part of the hydrofoil has a larger chord length than the outer part of the hydrofoil, the air of the inner part of the hydrofoil is There is an advantage that the amount of protrusion to the cushion chamber side does not have to be large. (4) By separating the flap control system for the outer part of the hydrofoil with flaps and the inner part of the hydrofoil with flaps, each flap has the same shape and size, but the same lift force is applied regardless of the level difference between the inside and outside water surfaces. There is an advantage in that the flap control is performed so that it can be generated, and the generation of an excessive bending force at the hydrofoil mounting portion can be avoided.

【図面の簡単な説明】[Brief description of drawings]

【図1】(a)は本発明の第1実施例としての水中翼付き
側壁型エアクッション船を示す船体横断面図であり、
(b)はその水中翼取付け部の側面図である。
FIG. 1 (a) is a lateral cross-sectional view of a hull showing a sidewall type air cushion ship with hydrofoils as a first embodiment of the present invention,
(b) is a side view of the hydrofoil attachment part.

【図2】(a)は本発明の第2実施例としての水中翼付き
側壁型エアクッション船の一部の横断面図であり、(b)
はその水中翼取付け部の平面図である。
FIG. 2 (a) is a lateral cross-sectional view of a part of a sidewall type air cushion ship with hydrofoils as a second embodiment of the present invention, and (b).
FIG. 4 is a plan view of the hydrofoil mounting portion.

【図3】本発明の第3実施例としての水中翼付き側壁型
エアクッション船における水中翼を示すもので、(a)は
その水中翼外側部分の翼断面図、(b)はその水中翼内側
部分の翼断面図である。
FIG. 3 shows a hydrofoil in a side wall type air cushion ship with hydrofoil as a third embodiment of the present invention, where (a) is a cross-sectional view of an outer portion of the hydrofoil, and (b) is a hydrofoil thereof. It is a blade cross-sectional view of an inner portion.

【図4】図3の水中翼フラップの制御系を示すブロック
図である。
FIG. 4 is a block diagram showing a control system of the hydrofoil flap of FIG.

【図5】(a)は従来の水中翼付き側壁型エアクッション
船を示す船体横断面図であり、(b)はその水中翼取付け
部の側面図、(c)はその水中翼取付け部の平面図であ
る。
FIG. 5 (a) is a lateral cross-sectional view of a conventional side wall type air cushion ship with hydrofoils, (b) is a side view of the hydrofoil mounting portion, and (c) is the hydrofoil mounting portion. It is a top view.

【符号の説明】[Explanation of symbols]

1 船体外側水面 2 エアクッション室内の水面 3 船体側壁部 4 水中翼 4a 水中翼外側部分 4b 水中翼内側部分 4af,4bf フラップ 5 エアクッション室 6 支柱 1 Water surface outside hull 2 Water surface inside air cushion chamber 3 Side wall part 4 Hull hydrofoil 4a Hydrofoil outer part 4b Hydrofoil inner part 4af, 4bf flap 5 Air cushion chamber 6 Strut

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 左右の船体側壁部の相互間にエアクッシ
ョン室をそなえるとともに、上記船体側壁部の各下端に
別個に支持されて左右に対をなす船体姿勢制御用水中翼
をそなえ、同水中翼が上記船体側壁部の下端への取付け
部から外側方へ延在する水中翼外側部分と上記取付け部
から内側方へ延在する水中翼内側部分とで構成されて、
航走中における上記エアクッション室内の水面と船体外
側水面とのレベル差に拘らず上記の水中翼外側部分と水
中翼内側部分とが同じ翼角でほぼ同等の揚力を発生すべ
く、上記水中翼内側部分が上記水中翼外側部分よりも広
い翼面積を有していることを特徴とする、水中翼付き側
壁型エアクッション船。
Claims: 1. An air cushion chamber is provided between the left and right side wall portions of the hull, and a pair of left and right hull attitude controlling hydrofoils are separately supported at the lower ends of the side wall portions of the hull to form a pair of water vessels. The wing is composed of a hydrofoil outer portion extending outward from the attachment portion to the lower end of the hull side wall portion and a hydrofoil inner portion extending inward from the attachment portion,
In order to generate almost the same lift at the same blade angle as the hydrofoil outer part and the hydrofoil inner part, regardless of the level difference between the water surface inside the air cushion chamber and the water surface outside the hull during sailing, the hydrofoil A side wall type air cushion ship with hydrofoils, characterized in that the inner part has a larger wing area than the hydrofoil outer part.
【請求項2】 請求項1に記載の水中翼付き側壁型エア
クッション船において、上記水中翼内側部分が上記水中
翼外側部分よりも大きい翼幅を有していることを特徴と
する、水中翼付き側壁型エアクッション船。
2. The hydrofoil according to claim 1, wherein the hydrofoil inner side portion has a larger wingspan than the hydrofoil outer side portion. Side wall type air cushion ship.
【請求項3】 請求項1に記載の水中翼付き側壁型エア
クッション船において、上記水中翼内側部分が上記水中
翼外側部分よりも大きい翼弦長さを有していることを特
徴とする、水中翼付き側壁型エアクッション船。
3. The sidewall-type air cushion ship with hydrofoil according to claim 1, wherein the hydrofoil inner portion has a chord length larger than that of the hydrofoil outer portion. Sidewall type air cushion ship with hydrofoils.
【請求項4】 左右の船体側壁部の相互間にエアクッシ
ョン室をそなえるとともに、上記船体側壁部の各下端に
別個に支持されて左右に対をなす船体姿勢制御用水中翼
をそなえ、同水中翼が上記船体側壁部の下端への取付け
部から外側方へ延在するフラップ付き水中翼外側部分と
上記取付け部から内側方へ延在するフラップ付き水中翼
内側部分とで構成されて、航走中における上記エアクッ
ション室内の水面と船体外側水面とのレベル差に拘らず
上記の水中翼外側部分と水中翼内側部分とがほぼ同等の
揚力を発生すべく、上記水中翼外側部分におけるフラッ
プの作動角と上記水中翼内側部分におけるフラップの作
動角とを別個に制御するフラップ制御系が設けられたこ
とを特徴とする、水中翼付き側壁型エアクッション船。
4. An air cushion chamber is provided between the left and right side wall portions of the hull, and the pair of left and right hull attitude controlling hydrofoils are separately supported at the lower ends of the side wall portions of the hull, and the pair of underwater water vessels are provided. The wing is composed of a hydrofoil outer part with flaps that extends outward from the attachment to the lower end of the side wall of the hull, and a hydrofoil inner part with flaps that extends inward from the attachment, In order for the hydrofoil outer part and the hydrofoil inner part to generate almost the same lift, regardless of the level difference between the water surface inside the air cushion chamber and the water surface outside the hull, the operation of the flaps on the hydrofoil outer part A side wall type air cushion ship with hydrofoils, characterized in that a flap control system for separately controlling an angle and an operating angle of the flap in the hydrofoil inner part is provided.
JP12091293A 1993-04-23 1993-04-23 Side wall type air cushion hydrofoil craft Withdrawn JPH06305413A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12091293A JPH06305413A (en) 1993-04-23 1993-04-23 Side wall type air cushion hydrofoil craft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12091293A JPH06305413A (en) 1993-04-23 1993-04-23 Side wall type air cushion hydrofoil craft

Publications (1)

Publication Number Publication Date
JPH06305413A true JPH06305413A (en) 1994-11-01

Family

ID=14798075

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12091293A Withdrawn JPH06305413A (en) 1993-04-23 1993-04-23 Side wall type air cushion hydrofoil craft

Country Status (1)

Country Link
JP (1) JPH06305413A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1326744C (en) * 2004-03-23 2007-07-18 重庆大学 Minitype ship with hidden wings
JP2008201220A (en) * 2007-02-19 2008-09-04 Honda Motor Co Ltd Outboard propulsion unit

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1326744C (en) * 2004-03-23 2007-07-18 重庆大学 Minitype ship with hidden wings
JP2008201220A (en) * 2007-02-19 2008-09-04 Honda Motor Co Ltd Outboard propulsion unit

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