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JPH03159865A - Air cushion boat - Google Patents

Air cushion boat

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Publication number
JPH03159865A
JPH03159865A JP30106289A JP30106289A JPH03159865A JP H03159865 A JPH03159865 A JP H03159865A JP 30106289 A JP30106289 A JP 30106289A JP 30106289 A JP30106289 A JP 30106289A JP H03159865 A JPH03159865 A JP H03159865A
Authority
JP
Japan
Prior art keywords
boat
air cushion
hull
ram pressure
side walls
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.)
Pending
Application number
JP30106289A
Other languages
Japanese (ja)
Inventor
Yusuke Uzawa
鵜沢 雄介
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP30106289A priority Critical patent/JPH03159865A/en
Publication of JPH03159865A publication Critical patent/JPH03159865A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To provide a hull with shelf-stabilizing property and enhance the boat running performance by embodying a drum to couple the side walls of the hull in the form of a wing of anti-buoyancy type, and thereby balancing the anti-buoyancy given by the drum with the buoyance due to ram pressure. CONSTITUTION:An air cushion boat is composed of a hull 1 as main structure, two side walls 2 functioning as a float, and a drum 3 to couple them. An air cushion layer 5 due to ram pressure is formed in the area bounded by the side walls 2 of the hull 1, wall 2b, drum 3, and the water surface 4, and through utilization of this layer 5 the boat coasts on the water. Therein the drum 3 is embodied in the form of a wing of anti-buoyancy type. That is, a deck 8 and a bottom of this drum 3 are constructed in such a form that the main wings of a plane are inverted up and down. Thereby the anti-buoyancy given by the drum 3 is balanced with the buoyancy due to the ram pressure, which should give the hull 1 self-stabilizing property.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明はエアークッション艇に関し、特に、艇体の両側
壁、この両側壁を連結する連結胴体および水面で囲まれ
る領域にラム圧によりエアークッション層を形威し、こ
のエアークッション層上に乗って水上を航走する際に、
艇体に自己安定性を持たせ、低速時の航走性能、姿勢制
御、直進性能、旋回性能等、操縦性、安全性を向上させ
て航走できるようにしたエアークッション艇に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to an air cushion watercraft, and in particular, air cushioning is provided by ram pressure to an area surrounded by both side walls of the hull, a connecting body connecting the both sides, and the water surface. When sailing on the water while riding on this air cushion layer,
The present invention relates to an air cushion boat that has self-stability in its hull and can sail with improved maneuverability and safety such as low-speed cruising performance, attitude control, straight-line performance, and turning performance.

[従来の技術] 従来から、船が早く走るには水の抵抗を如何に少なくす
るかという課題について開発研究がなされ、水中翼船、
ホーバークラフト、高速滑走艇等が生れ、かなりの戒果
をあげている。これらは何れも艇体を水から浮」ニさせ
て水の抵抗から逃れる方法が採用されている。特にエア
ークッション艇(A.C.V.=エアー・クッション・
ビークル)には、ホーバークラフ1・の他にノ1イドロ
キール(第9図(a))、グランド・エフェクト・ウイ
ング(同図(b))、ラム・ウイング(同図(C))、
チャンネル・フロー・ウイング(同図(d))’:’i
−の種類があり、地表(海面)効果(グランドエフェク
ト)で水の抵抗を少なくしている。
[Prior Art] Research and development has been conducted on the issue of how to reduce water resistance so that ships can run faster, and hydrofoils,
Hovercraft, high-speed gliding boats, etc. were born and have achieved considerable success. All of these methods employ a method of floating the hull above the water to escape water resistance. Especially air cushion boats (A.C.V. = air cushion boat)
In addition to the Hoverclaw 1, the vehicle also includes a No. 1 Hydrokeel (Figure 9 (a)), a ground effect wing (Figure 9 (B)), a Ram Wing (Figure 9 (C)),
Channel flow wing ((d) in the same figure)':'i
There are - types, which reduce water resistance using the ground effect.

これらのエアークッション艇は、乗り心地が良いこと、
燃料消費が少ないこと、速度が比較的早いこと、浮遊物
の影饗を受けないこと、浅い所でも走行できること、小
さい波浪の影響を受けないこと等の利点がある。
These air cushion boats are comfortable to ride,
Advantages include low fuel consumption, relatively high speed, unaffected by floating objects, ability to travel in shallow areas, and unaffected by small waves.

[発明か舶′決しようとする課題] しかしながら、従来のエアークッション艇では、何れも
艇体が水から浮」ニすると艇体の自己安定性がなくなり
縦揺れ(ピッチング)、横揺れ(ローリング)、横風に
流されること等操縦性が悪くなるという根本的な欠陥を
帯有している。しかも、揚力、重力、推力、ラム圧等の
力の釣合か速度によって変化し高速になると動的安定性
を保つのか非常に難しくなる。また波演および向風等の
影響でピッチアップ(急な頭上げ)現象か惹起し航送に
大きな悪影響をもたらす。さらに浮揚した状態では舵(
ラダー)を操作しても艇体は回頭しずらく旋回性能か悪
いというノ(通した%11!,’,j、をイjしている
[Problem to be determined by the invention or the ship] However, in conventional air cushion boats, when the hull floats out of the water, the hull loses its self-stability, resulting in pitching (pitching) and rolling. However, it has fundamental flaws such as poor maneuverability, such as being swept away by crosswinds. Moreover, the balance of forces such as lift, gravity, thrust, and ram pressure changes depending on the speed, making it extremely difficult to maintain dynamic stability at high speeds. In addition, the effects of wave action and headwinds can cause pitch-up (sudden head-up) phenomena, which has a major negative impact on navigation. Furthermore, in a levitating state, the rudder (
Even if you operate the rudder, the boat has difficulty turning and its turning performance is poor.

[発明の目的] 本発明は」二記従来の難点に鑑みなされたもので、艇体
の両側壁、この両側壁を連結する連結胴体および水面で
囲まれる領域にラム圧によりエアークッション層を形威
し、このエアークッション層上に乗って水上を航走する
際に、艇体に自己安定性を持たせ、低速時の航走性能、
姿勢制御、直進性能、旋回性能等、操縦性、安全性を向
」ニさせて航走できるようにしたエアークッション艇を
提(J(せんとするものである。
[Object of the Invention] The present invention has been made in view of the two conventional difficulties, and it forms an air cushion layer by ram pressure on both side walls of the hull, the connecting body connecting the both sides, and the area surrounded by the water surface. When sailing on the water while riding on this air cushion layer, the hull has self-stability, improving sailing performance at low speeds,
We aim to develop an air-cushion boat that can navigate with improved maneuverability and safety, including attitude control, straight-line performance, and turning performance.

[課題を解決する手段] この目的を達威するため、本発明のエアークッション艇
は、艇体の両側壁、この両側壁を連結する連結胴体およ
び水而で囲まれる領域にラム圧によりエアークソション
層を形成し、このエアークッション層−1−に乗って水
上を航走するエアークッション艇において、前記連結胴
体を反揚力型の翼形に形成することにより、前記連結胴
体による反揚力と前記ラム圧による浮揚力との釣合で艇
体に自己安定性を持たせるようにしたものである。
[Means for Solving the Problems] In order to achieve this object, the air cushion boat of the present invention provides air cushioning by ram pressure to both side walls of the hull, the connecting body connecting the both sides, and the area surrounded by water. In an air cushion boat that travels on water riding on this air cushion layer-1-, the connected fuselage is formed into an anti-lift airfoil shape, so that the anti-lift force caused by the connected fuselage and the The hull is made to have self-stability by balancing the buoyancy force generated by the ram pressure.

また、本発明のエアークッション艇は、空中ブロベラを
前記連結胴体」二に設け、前記空中プロペラからの後流
を前記連結胴体の艇底に導入するダクトを形或すること
により、前記ラム圧による浮揚ツノを高めて前記連結胴
体による反揚力と前記ラム圧による浮揚力との釣合で艇
体に自己安定性および航走性能を向上させるようにした
ものである。
Further, in the air cushion boat of the present invention, an aerial blower is provided on the connecting body, and a duct is formed to introduce the slipstream from the aerial propeller to the bottom of the connecting body. The self-stability and cruising performance of the boat body are improved by increasing the buoyancy horn and balancing the counterlifting force generated by the connected fuselage with the buoyancy force generated by the ram pressure.

さらに、本発明のエアークッション艇は、riij記両
側壁の夫々にフィンをその有効面積が可変になるように
枢着することにより、而記艇体の浮揚時の旋回性を向上
させたものである。
Further, in the air cushion watercraft of the present invention, fins are pivotally attached to each of the side walls so that the effective area thereof is variable, thereby improving the turning performance of the watercraft when it is floating. be.

[作用コ 5 このように構威されたエアークッション艇において、空
中プロペラで得られる推進力により速度か上がると、艇
体の両側壁、この両側壁を連結する連結胴体および水面
で囲まれる領域にラム圧(空気の押込み圧力)によりエ
アークッション層が形戊され、このエアークッション層
−1二に乗って艇は水上を航走する。この場合、速度か
増すにつれて、エアーが艇体の艇首から高速流入し、艇
体の両側壁、この両側壁を連結する連結胴体および水面
で囲まれる領域にラム圧が増加し、このためその圧力に
より艇体はそれまでよりも水面から高く持上げられる結
果、浮き過ぎてしまい艇体が不安定になる。しかしなが
ら、連結胴体を反揚力型の翼形に形成することにより、
連結胴体による反揚力とラム圧による浮揚力との釣合で
艇体に自己安定性を持たせることかでき艇は安定して航
走可能である。
[Effect 5] When the speed of an air cushion boat configured in this way increases due to the propulsion force obtained from the aerial propeller, the area surrounded by both side walls of the hull, the connecting body connecting the both sides walls, and the water surface An air cushion layer is formed by ram pressure (pushing pressure of air), and the boat sails on the water riding on this air cushion layer-12. In this case, as the speed increases, air enters the bow of the boat at high speed, increasing the ram pressure in the area bounded by the hull sides, the articulated fuselage connecting the sides, and the water surface, thus increasing the ram pressure. The pressure lifts the boat higher out of the water than before, causing it to float too high and become unstable. However, by forming the connected fuselage into an anti-lift airfoil shape,
The boat body can be given self-stability by balancing the counterlifting force generated by the connected body and the buoyancy force caused by the ram pressure, and the boat can sail stably.

また、連結胴体上に設けられた空中プロペラからの後流
を連結胴体の艇底に導入するダクトを形戊することによ
り、中速時のラム圧による浮揚力6 を高めて連結胴体による反揚力とラム圧による浮揚力と
の釣合で艇体に自己安定性および中速時の航走性能を向
上させることができる。
In addition, by forming a duct that introduces the slipstream from the aerial propeller installed on the connected fuselage to the bottom of the connected fuselage, the buoyancy force due to ram pressure at medium speeds is increased, and the counterlift force due to the connected fuselage is increased. The self-stability of the hull and the cruising performance at medium speeds can be improved by balancing this with the buoyancy force generated by the ram pressure.

さらに、両側壁の夫々にフィンをその有効面積が可変に
なるように枢着することにより、艇体の浮揚時の旋回性
を向上させることかできる。
Furthermore, by pivotally attaching fins to each of the side walls so that the effective area of the fins can be varied, it is possible to improve the turning performance of the boat when it is floating.

[実施例] 以下、本発明の好ましい実施例を図面により説明する。[Example] Preferred embodiments of the present invention will be described below with reference to the drawings.

第1図、第2図に示すように本発明のエアークッション
艇は、艇体1を主構造とし、フロートとして機能する両
側壁2、2と、この両側壁を連結する連結胴体3とから
成る。両側壁2、2にはステップ2aが設けられ、これ
らのステップ2aにはウオール2bが側壁2、2に対し
て流線形となるように延びている。艇体1の艇底9は後
述するラム圧(空気の押込み圧力)Pを生じるように艇
首が上方に曲線状に延びてアッタツクアングルを形威し
両側壁2、2、ウオール2b,2bと」(にほぼ逆レ字
形をなしている。このエアークッション艇は、艇体1の
両側壁2、2、ウオール2b,2b,両側壁2、2を連
結する運結胴休3および水面4で囲まれる領域にラム圧
によりエアークッション層5を形威し、このエアークッ
ション層上に乗って水上を航走するものである。
As shown in FIGS. 1 and 2, the air cushion boat of the present invention has a hull 1 as its main structure, and is composed of both side walls 2, 2 that function as floats, and a connecting body 3 that connects these side walls. . Steps 2a are provided on both side walls 2, 2, and walls 2b extend in these steps 2a in a streamlined manner with respect to the side walls 2, 2. The bottom 9 of the hull 1 has a bow extending upward in a curve to form an attack angle so as to generate a ram pressure (pushing pressure of air) P, which will be described later. This air cushion boat has two walls 2, 2 on both sides of the hull 1, walls 2b, 2b, a docking suspension 3 connecting the side walls 2, 2, and a water surface 4. An air cushion layer 5 is formed by ram pressure in the area surrounded by , and the boat sails on the water while riding on this air cushion layer.

本発明の特徴によれば、エアークッション艇は、連結胴
体3は反揚力型の翼形に形成されている。
According to a feature of the present invention, in the air cushion watercraft, the connected fuselage 3 is formed in the shape of an anti-lift wing.

即ち、連結胴体3はそのデッキ8と艇底9が飛行機の主
翼を上下逆にした形態をしている。これにより、連結胴
体3による反揚力6とラム圧による浮揚力7との釣合で
艇体1に自己安定性を持たせることができる。
That is, the deck 8 and boat bottom 9 of the articulated fuselage 3 are shaped like the main wing of an airplane upside down. Thereby, the hull 1 can be given self-stability by balancing the counterlift force 6 caused by the connecting body 3 and the buoyancy force 7 caused by the ram pressure.

また、第3図、第4図、第6図に示すように、本発明の
エアークッション艇では、空中プロペラ10が連結胴体
3上に設けられ、エアークッション艇の推進力はこれで
得られる。空中プロペラ10は艇体1のデッキ8前方に
設けられたエンジン12で回転駆動される。空中プロペ
ラ10からの後流の一部を連結胴体3の艇底9に導入す
るダクト11が形威されている。ダクト11の人口はデ
ッキ8に蝶番14で枢着された導入板13で形成されて
いる。導入板13はモータ16により開閉制御される。
Further, as shown in FIGS. 3, 4, and 6, in the air cushion boat of the present invention, an aerial propeller 10 is provided on the connected body 3, and the propulsion force of the air cushion boat is obtained by this. The aerial propeller 10 is rotationally driven by an engine 12 provided in front of the deck 8 of the hull 1. A duct 11 is provided which introduces a part of the slipstream from the aerial propeller 10 into the boat bottom 9 of the connected fuselage 3. The population of the duct 11 is formed by an introduction plate 13 which is pivotally connected to the deck 8 with a hinge 14. The introduction plate 13 is controlled to open and close by a motor 16.

連結胴体3の艇底9のラム圧力1)を検出する圧カセン
サ15a,15bからの信号によりドライバ17か働き
、モータ16を駆動する。
The driver 17 is actuated by signals from the pressure sensors 15a, 15b which detect the ram pressure 1) of the boat bottom 9 of the joint body 3, and the motor 16 is driven.

この導入板13がモータl6により開成されると中速時
のラム圧による浮揚力7を高めて連結胴体3による反揚
力6とラム圧Pによる浮揚力7との釣合で艇体に自己安
定性および中速時の航走性能を向上させることができる
When this introduction plate 13 is opened by the motor 16, the buoyancy force 7 due to the ram pressure at medium speed is increased, and the balance between the anti-lift force 6 due to the connected fuselage 3 and the buoyancy force 7 due to the ram pressure P causes the hull to self-stabilize. It is possible to improve speed and cruising performance at medium speeds.

さらに、第1図、第3図、第8図(a)、(b)に示す
ように、本発明のエアークッション艇は、両側壁2、2
の夫々にフイン20をその有効面積が可変になるように
枢着することにより、艇体1の浮揚時の旋回性を向上さ
せることができる。
Further, as shown in FIGS. 1, 3, 8(a) and 8(b), the air cushion boat of the present invention has side walls 2, 2
By pivotally attaching the fins 20 to each of the fins so that the effective area thereof is variable, the turning performance of the hull 1 when floating can be improved.

第5図に示すように、艇体1の艇底9には艇首から艇尾
にかけて左右のラム圧を仕切るセンターキール21が延
在している。センターキール後方にはラダー22が備え
られ、コックピット23に設けられたハンドル(図示せ
ず)により操舵され9 る。なお、第1図〜第4図において25は垂直尾翼であ
る。
As shown in FIG. 5, a center keel 21 extending from the bow to the stern of the boat bottom 9 of the boat body 1 separates left and right ram pressures. A rudder 22 is provided behind the center keel, and is steered by a handle (not shown) provided in a cockpit 23. In addition, in FIGS. 1 to 4, 25 is a vertical tail.

このように構威されたエアークッション艇において、空
中プロペラ10がエンジン12で回動されて艇は走行す
るが、低速では通常の船として航走する。この時の水面
4aを第2図に示す。
In the air cushion boat configured in this manner, the aerial propeller 10 is rotated by the engine 12 to propel the boat, but at low speeds the boat runs like a normal boat. The water surface 4a at this time is shown in FIG.

中速(例えば、3 5 〜4 0 k m / h )
になると、第2図に示すように、エアーが艇体1の艇首
から流入し、艇体1の両側壁2、2、ウオール2b,2
b,両側壁2、2を連結する連結胴体3および水面4で
囲まれる領域にラム圧Pによりエアークッション層5を
形l戊し、このラム圧による浮揚力7が発生して艇はこ
のエアークッション層」二に乗って水上を航走する。速
度を増すごとに浮揚ノノ7が増大し、不安定性も増加す
るが、その速度に達する頃に反揚力型の翼形に形成され
た連結胴体3による反揚力6が発生し、艇体1を押し下
げる作用が働く。この反揚力6は速度の二乗に比例して
増加し、ラム圧による浮揚力7との釣合で艇体1が自己
安定性を持ち高速時での波浪等によるピッ10  − チアップ(急な頭」二げ)現象を抑制することかできる
。高速時での水而4を第2図に示す。
Medium speed (e.g. 35-40 km/h)
Then, as shown in FIG.
b. An air cushion layer 5 is formed by ram pressure P in the area surrounded by the connecting body 3 connecting the side walls 2 and 2 and the water surface 4, and the buoyancy force 7 generated by this ram pressure causes the boat to float on this air. It sails on the water while riding on the "cushion layer". As the speed increases, the buoyancy force 7 increases and the instability also increases, but by the time that speed is reached, a counterlift force 6 is generated by the connected fuselage 3 formed in the shape of a counterlift type airfoil, causing the hull 1 to It works to push it down. This anti-lift force 6 increases in proportion to the square of the speed, and in balance with the buoyancy force 7 caused by the ram pressure, the hull 1 becomes self-stabilizing and is prevented from pitching due to waves etc. at high speed. (2) phenomenon can be suppressed. Figure 2 shows the water flow at high speed.

中速時および追風航走時には、連結胴体3の艇底9のラ
ム圧力Pが低下しており、この圧力Pを検出する圧カセ
ンサ15a,15bからの信号によりドライバ17が働
き、モータ16を駆動する(第3図)。モータ16は導
入板l3を開成し、エンジン12で回転駆動される空中
ブロベラ10からの後流の一部がダク]・11を通って
連結胴体3の艇底9に導入される。中速時のラム圧によ
る浮揚力7を高めて連結胴体3による反揚力6とラム圧
による浮揚力7との釣合で艇体に自己安定性および中速
時の経済航走性能を向上させることができる。
At medium speed and when sailing with a tailwind, the ram pressure P at the bottom 9 of the connected body 3 is decreasing, and the driver 17 is activated by signals from the pressure sensors 15a and 15b that detect this pressure P, and drives the motor 16. (Figure 3). The motor 16 opens the introduction plate 13, and a part of the wake from the aerial blower 10, which is rotationally driven by the engine 12, is introduced into the boat bottom 9 of the connected fuselage 3 through the duct 11. By increasing the buoyancy force 7 due to the ram pressure at medium speeds and balancing the counterlift force 6 due to the connected fuselage 3 and the buoyancy force 7 due to the ram pressure, the self-stability of the hull and the economical cruising performance at medium speeds are improved. be able to.

さらに、一般のエアークッンヨン艇では、第7図(a)
に示すように、艇体が浮揚した状態ではラダー22を操
作しても艇体は回頭しすらく旋回性能が悪い。本発明の
エアークッション艇では、両側壁2、2の夫々にフィン
20(第1図、第3図)をその有効面積が可変になるよ
うに枢着されていることにより、第7図(b)に示すよ
うに、艇体1が浮揚した状態で艇体lは回頭し浮揚時の
旋回性を向上させることかできる。第8図(a)、(b
)に示すように、艇の速度やその他の浮揚状態に応じて
フイン20を手動などにより枢動させ、水面に接する有
効面積が可なとされる。また、住用時には両側壁2、2
の夫々からフイン20を延在させ、不使用時には両側壁
2、2の夫々へフイン20を格納するように枢動するこ
とかできる。
Furthermore, in a general air boat, Fig. 7 (a)
As shown in FIG. 2, when the boat is floating, even if the rudder 22 is operated, the boat does not turn and its turning performance is poor. In the air cushion boat of the present invention, the fins 20 (FIGS. 1 and 3) are pivotally mounted on each of the side walls 2, 2 so that the effective area thereof can be varied, so that the fins 20 (FIGS. ), the boat 1 can turn while the boat 1 is floating, thereby improving the turning performance when the boat is floating. Figure 8(a),(b)
), the effective area in contact with the water surface can be increased by manually pivoting the fins 20 depending on the speed of the boat and other buoyancy conditions. Also, for residential use, both side walls 2, 2
The fins 20 can extend from each of the fins 20, and can be pivoted to be retracted into each of the side walls 2, 2 when not in use.

[発明の効果] 以上の実施例からも明らかなように、本発明のエアーク
ッション艇によれば、艇体の両側壁、この両側壁を連結
する連結胴体および水面で囲まれる領域にラム圧により
エアークッション層を形或し、このエアークッション層
」二に乗って水上を航走するエアークッション艇におい
て、連結胴体を反揚力型の翼形に形成することにより、
連結胴体による反揚力と前記ラム圧による浮揚力との釣
合で艇体に自己安定性を持たせることができる。
[Effects of the Invention] As is clear from the above embodiments, according to the air cushion boat of the present invention, ram pressure is applied to the area surrounded by both side walls of the hull, the connecting body connecting the both side walls, and the water surface. In an air cushion boat that has an air cushion layer and sails on water while riding on this air cushion layer, by forming the connected fuselage into an anti-lift wing shape,
The boat body can be made to have self-stability by balancing the reaction force caused by the connecting body and the buoyancy force caused by the ram pressure.

また、空中プロペラを連結胴体上に設け、空中プロペラ
からの後流を連粘胴体の艇底に導入するダクトを形戊す
ることにより、中速時のラム圧による浮揚力を高めて連
結胴体による反揚力とラム圧による浮揚力との釣合で艇
体に自己安定性および中速時の航走性能を向上させるこ
とができる。
In addition, by installing an aerial propeller on the connected fuselage and forming a duct that introduces the slipstream from the aerial propeller to the bottom of the connected fuselage, the buoyant force generated by the ram pressure at medium speeds is increased and the connected fuselage is By balancing the anti-lift force with the buoyancy force due to ram pressure, the self-stability of the hull and the cruising performance at medium speeds can be improved.

さらに、両側壁の夫々にフィンをその有効面積が可変に
なるようにMatすることにより、艇体の浮揚時の旋回
性を向上させることができる。
Further, by arranging fins on each of the side walls so that the effective area thereof is variable, it is possible to improve the turning performance of the boat when it is floating.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明に係わるエアークッション艇の斜視図、
第2図、第3図は第1図のエアークッション艇を連結胴
体で切断して見た側面図、第4図は第1図のエアークッ
ション艇の部分破断した平面図、第5図は第1図に示す
エアークッション艇の艇首から見た正面図、第6図は第
4図に示すエアークッション艇のY−Y’線における断
面図、第7図(a)、(b)は本発明に係わるエアーク
ッション艇のフィンの動作を示す説明図、第8図(a)
、(b)は本発明に係わるエアークッション艇のフィン
を示す説明図、第9図(a)、(b)13 (C)、(d)はそれぞれ従来のエアークッション艇の
説明図である。 1・・・・・・艇体 2、2・・・・・・両側壁 3・・・・・・連結胴体 4、4a・・・・・・水面 P・・・・・・ラム圧 5・・・・・・ラム圧によるエアークッション層6・・
・・・・連結胴体による反揚力 7・・・・・・ラム圧による浮揚力 9・・・・・・艇底 10・・・・・・空中ブロベラ 11・・・・・・ダクト 20・・・・・・フィン
FIG. 1 is a perspective view of an air cushion boat according to the present invention;
Figures 2 and 3 are side views of the air cushion boat shown in Figure 1 cut away at the connected fuselage, Figure 4 is a partially cutaway plan view of the air cushion boat shown in Figure 1, and Figure 5 is a side view of the air cushion boat shown in Figure 1. Figure 1 is a front view of the air cushion boat seen from the bow; Figure 6 is a sectional view of the air cushion boat shown in Figure 4 taken along line Y-Y'; Figures 7 (a) and (b) are Explanatory diagram showing the operation of the fin of the air cushion boat according to the invention, FIG. 8(a)
, (b) are explanatory views showing the fins of the air cushion watercraft according to the present invention, and FIGS. 9(a), (b), 13 (C), and (d) are explanatory views of the conventional air cushion watercraft, respectively. 1...Hull 2, 2...Both side walls 3...Connected fuselage 4, 4a...Water surface P...Ram pressure 5. ...Air cushion layer 6 due to ram pressure...
... Repulsion force due to the connected fuselage 7 ... Buoyancy force due to ram pressure 9 ... Boat bottom 10 ... Aerial blower 11 ... Duct 20 ... ····fin

Claims (1)

【特許請求の範囲】 1、艇体の両側壁、この両側壁を連結する連結胴体およ
び水面で囲まれる領域にラム圧によりエアークッション
層を形成し、このエアークッション層上に乗って水上を
航走するエアークッション艇において、前記連結胴体を
反揚力型の翼形に形成することにより、前記連結胴体に
よる反揚力と前記ラム圧による浮揚力との釣合で艇体に
自己安定性を持たせるようにしたことを特徴とするエア
ークッション艇。 2、空中プロペラを前記連結胴体上に設け、前記空中プ
ロペラからの後流を前記連結胴体の艇底に導入するダク
トを形成することにより、前記ラム圧による浮揚力を高
めて前記連結胴体による反揚力と前記ラム圧による浮揚
力との釣合で艇体に自己安定性および航走性能を向上さ
せるようにしたことを特徴とする請求項1記載のエアー
クッション艇。 3、前記両側壁の夫々にフィンをその有効面積が可変に
なるように枢着することにより、前記艇体の浮揚時の旋
回性を向上させたことを特徴とする請求項1または2記
載のエアークッション艇。
[Claims] 1. An air cushion layer is formed by ram pressure in the area surrounded by both side walls of the hull, the connecting body connecting these side walls, and the water surface, and the boat rides on the air cushion layer and sails on the water. In a running air cushion boat, by forming the connected fuselage into an anti-lift airfoil shape, the hull has self-stability by balancing the anti-lift force from the connected fuselage with the buoyancy force due to the ram pressure. An air cushion boat characterized by: 2. An aerial propeller is provided on the connected fuselage, and a duct is formed to introduce the slipstream from the aerial propeller to the bottom of the connected fuselage, thereby increasing the buoyant force due to the ram pressure and reducing the reaction by the connected fuselage. 2. The air cushion watercraft according to claim 1, wherein the self-stability and running performance of the boat body are improved by balancing the lifting force with the buoyancy force generated by the ram pressure. 3. The boat according to claim 1 or 2, characterized in that fins are pivotally attached to each of the side walls so that the effective area thereof is variable, thereby improving turning performance when the boat body is floating. air cushion boat.
JP30106289A 1989-11-20 1989-11-20 Air cushion boat Pending JPH03159865A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP30106289A JPH03159865A (en) 1989-11-20 1989-11-20 Air cushion boat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP30106289A JPH03159865A (en) 1989-11-20 1989-11-20 Air cushion boat

Publications (1)

Publication Number Publication Date
JPH03159865A true JPH03159865A (en) 1991-07-09

Family

ID=17892408

Family Applications (1)

Application Number Title Priority Date Filing Date
JP30106289A Pending JPH03159865A (en) 1989-11-20 1989-11-20 Air cushion boat

Country Status (1)

Country Link
JP (1) JPH03159865A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05294277A (en) * 1992-04-21 1993-11-09 Shinrei Zosen Kk Ground effect blade vessel
US5314035A (en) * 1992-08-10 1994-05-24 Schoell Harry L Surface effect vehicle
US5566775A (en) * 1992-08-10 1996-10-22 Schoell; Harry Skirted surface effect vehicle
US6912967B1 (en) * 2003-07-15 2005-07-05 Graham H. Oats Hybrid watercraft
JP2008137506A (en) * 2006-12-01 2008-06-19 Fjc:Kk Vessel

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05294277A (en) * 1992-04-21 1993-11-09 Shinrei Zosen Kk Ground effect blade vessel
US5314035A (en) * 1992-08-10 1994-05-24 Schoell Harry L Surface effect vehicle
US5566775A (en) * 1992-08-10 1996-10-22 Schoell; Harry Skirted surface effect vehicle
US6912967B1 (en) * 2003-07-15 2005-07-05 Graham H. Oats Hybrid watercraft
JP2008137506A (en) * 2006-12-01 2008-06-19 Fjc:Kk Vessel

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