JPH023972Y2 - - Google Patents

Info

Publication number
JPH023972Y2
JPH023972Y2 JP12409784U JP12409784U JPH023972Y2 JP H023972 Y2 JPH023972 Y2 JP H023972Y2 JP 12409784 U JP12409784 U JP 12409784U JP 12409784 U JP12409784 U JP 12409784U JP H023972 Y2 JPH023972 Y2 JP H023972Y2
Authority
JP
Japan
Prior art keywords
air
chamber
hollow
air chamber
ship
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
Application number
JP12409784U
Other languages
Japanese (ja)
Other versions
JPS6138265U (en
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 filed Critical
Priority to JP12409784U priority Critical patent/JPS6138265U/en
Publication of JPS6138265U publication Critical patent/JPS6138265U/en
Application granted granted Critical
Publication of JPH023972Y2 publication Critical patent/JPH023972Y2/ja
Granted legal-status Critical Current

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  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Fluid-Damping Devices (AREA)
  • Vibration Prevention Devices (AREA)

Description

【考案の詳細な説明】 〈考案の技術分野〉 本考案はホバークラフトと称する水陸両用艇、
つまりエアークツシヨン艇に関する。
[Detailed description of the invention] <Technical field of the invention> The invention is an amphibious craft called a hovercraft.
In other words, it's about air-cussion boats.

〈考案の背景〉 従来この種エアークツシヨン艇は、船体上へ、
船体に推力および浮力を発生させるエアー発生機
構、および船底の外周縁に沿つて、前記エアー発
生機構に連通したスカート状の中空エアーチヤン
バーを配設してなり、前記エアー発生機構からの
エアーの一部を中空エアーチヤンバーに導入し、
中空チヤンバーの内側面に列設した噴出口および
底面に列設した噴出孔よりエアーを噴出し、該中
空チヤンバーに囲まれた船底下に浮揚用圧力エア
ー溜りが生じることによつて空気浮上し、推進す
る。
<Background of the invention> Conventionally, this type of air-cussion boat has a
An air generation mechanism that generates thrust and buoyancy in the hull, and a skirt-shaped hollow air chamber that communicates with the air generation mechanism is disposed along the outer periphery of the bottom of the ship, and the air generation mechanism generates air from the air generation mechanism. Introducing a part into the hollow air chamber,
Air is ejected from the jet ports arranged on the inner side of the hollow chamber and the jet holes arranged on the bottom surface, and a buoyant pressure air pool is created under the bottom of the ship surrounded by the hollow chamber, thereby causing air levitation, Promote.

ところが、前記中空エアーチヤンバーに列設し
た噴出口は、船底に近いチヤンバーの両側面の上
部に単に孔を穿設しただけのため、直線走行の場
合は問題はないが、船体が左旋回により横すべり
した場合、第3図に示す如く、旋回により浮揚用
圧力エアー室4に海水波が生じ、このとき、噴出
口37から中空チヤンバー3内に相当量の水が侵
入し、陸上の場合は石、砂が侵入する。このよう
に中空エアーチヤンバー内へ水等が侵入すると完
全に浮上困難となり、特に水面走行では、侵入し
た水の重量によつて中空エアーチヤンバー3が水
中に位置し、摩擦牴抗が増加してスピードダウン
乃至走行不能となる。また陸上走行では、地面と
の接触により忽にして摩擦乃至破損する。
However, since the jet ports arranged in the hollow air chamber are simply holes drilled in the upper part of both sides of the chamber near the bottom of the ship, there is no problem when traveling in a straight line, but when the ship turns left, In the event of a sideslip, as shown in Figure 3, seawater waves are generated in the buoyancy pressure air chamber 4 due to the rotation, and at this time, a considerable amount of water enters the hollow chamber 3 from the spout 37, and if it is on land, it will cause a rock formation. , sand intrudes. If water or the like enters the hollow air chamber in this way, it becomes difficult to float completely, and especially when driving on water, the hollow air chamber 3 is located underwater due to the weight of the water that has entered, increasing frictional resistance. The vehicle speeds down or becomes impossible to drive. Furthermore, when traveling on land, contact with the ground causes friction or damage.

〈考案の目的〉 本考案は極めて簡単な構成により、旋回走行
時、中空エアーチヤンバー内への水、砂の侵入を
完全に防止し、安定走行を実現できる新規な浮揚
エアー噴出装置を提供することを目的とする。
<Purpose of the invention> The present invention provides a novel floating air blowing device that has an extremely simple configuration and can completely prevent water and sand from entering the hollow air chamber during turning, thereby realizing stable running. The purpose is to

〈考案の構成および作用効果〉 上記目的を達成するため、本考案では、スカー
ト状中空エアーチヤンバーの各噴出口にそれぞれ
可撓性ノズルの基端を連設し、先端噴射口をそれ
ぞれ船底に近接且つ斜めに対向させてなる。上記
構成によると、旋回走行により浮揚用圧力エアー
室に海水波が生じたとき、かりに高波と雖どもノ
ズルの噴射口に至らず、従つて、中空エアーチヤ
ンバー内への水、砂の侵入を完全に防止できる。
従つて、船体は直進、旋回の何れの走行において
も常時エアー浮上して安定走行を実現する効果を
有す。
<Configuration and effects of the invention> In order to achieve the above object, in the present invention, the base end of a flexible nozzle is connected to each jet port of the skirt-like hollow air chamber, and the tip jet port is connected to the bottom of the ship. They are placed close and diagonally opposite each other. According to the above configuration, when seawater waves are generated in the flotation pressure air chamber due to turning, the high waves do not reach the nozzle injection port, thus preventing water and sand from entering the hollow air chamber. Completely preventable.
Therefore, the hull always floats in the air and has the effect of realizing stable running whether traveling straight or turning.

〈実施例の説明〉 第1図はエアークツシヨン艇の全体側面図を示
し、船体1には、その船尾11にエアー発生機構
2、船底12の外周縁に沿い1周するスカート状
の中空エアーチヤンバー3を配設している。
<Description of Embodiments> FIG. 1 shows an overall side view of an air-cushion watercraft, in which a hull 1 includes an air generation mechanism 2 at the stern 11, and a skirt-shaped hollow air that goes around the outer periphery of the bottom 12. Chamber 3 is installed.

前記エアー発生機構2は、船体1に架設した円
筒ダクト21中へプロペラ22を軸承配備し、該
プロペラ22の回転軸を直接或いは伝動手段を介
して回転駆動装置(図示せず)に連繋してなり、
プロペラ22の回転によりダクト21内に高速エ
アー流を発生させる。円筒ダクト21において、
プロペラ22の下流側には、ダクト21の一部を
占有してエアー流入口23が開設され、該流入口
23は通路24を介して中空エアーチヤンバー3
に連通している。
The air generation mechanism 2 has a propeller 22 disposed in a cylindrical duct 21 installed in the hull 1, and a rotating shaft of the propeller 22 is connected to a rotational drive device (not shown) directly or through a transmission means. Become,
The rotation of the propeller 22 generates a high-speed air flow within the duct 21. In the cylindrical duct 21,
An air inlet 23 is provided on the downstream side of the propeller 22 by occupying a part of the duct 21, and the air inlet 23 is connected to the hollow air chamber 3 through a passage 24.
is connected to.

中空エアーチヤンバー3は、ゴム或いは合成樹
脂材によつて耐通気性の表面処理を施こした可撓
性シート材からなる筒材31を船底12の外周部
に沿いスカート状に配設したもので、前記筒材3
1は、船底外周部13の傾斜に適合した傾斜部3
2の下端に対称的に傾斜した囲い部33および囲
い部33の下端に水平底部34および該底部34
を側壁部35を介して前記傾斜部32の上端に連
続させた筒状をなし、傾斜部32を船底の外周部
13に一体に取付けている。該中空エアーチヤン
バー3の底部34には、周方向に適当間隔を存し
てエアー噴出孔36を穿設すると共に、囲い部3
3の上部には、周方向に等間隔を存してエアー噴
出口37を開設し、各噴出口に本考案に係るエア
ー噴出装置を構成する。即ち、本案は、前記各噴
出口37に対し、それぞれエアー通過時にV状を
なす可撓性ノズル38の基端を連設し、先端噴射
口39を互いに船底12に近接且つ斜めに対向す
るようにしてなるもので、該ノズルは、可撓性資
材を一定形態に裁断してV状筒に縫成したもので
ある。尚、前記ノズル38の設置数、間隔、筒径
および底部34のエアー噴出孔36の位置、間
隔、設置数、孔径等は、船体1の重量、エアー圧
力、走行時の姿勢等に基づき設定する。
The hollow air chamber 3 has a cylindrical member 31 made of a flexible sheet material whose surface has been treated with air resistance using rubber or synthetic resin material and arranged in a skirt shape along the outer periphery of the ship's bottom 12. Then, the cylinder material 3
1 is a sloped portion 3 adapted to the slope of the outer peripheral portion 13 of the bottom of the ship;
2 and a horizontal bottom 34 at the lower end of the enclosure 33;
It has a cylindrical shape that is continuous with the upper end of the inclined part 32 via a side wall part 35, and the inclined part 32 is integrally attached to the outer peripheral part 13 of the bottom of the ship. The bottom part 34 of the hollow air chamber 3 is provided with air jet holes 36 at appropriate intervals in the circumferential direction, and the surrounding part 3
3, air jet ports 37 are provided at equal intervals in the circumferential direction, and each jet port constitutes an air jet device according to the present invention. That is, in the present invention, the base end of a flexible nozzle 38 that forms a V shape when air passes through is connected to each of the jet ports 37, and the tip jet ports 39 are arranged close to the bottom 12 and diagonally opposite each other. The nozzle is made by cutting a flexible material into a certain shape and sewing it into a V-shaped tube. The number, spacing, and diameter of the nozzles 38 installed, and the position, spacing, number, and diameter of the air jet holes 36 in the bottom 34 are set based on the weight of the hull 1, air pressure, posture during traveling, etc. .

然して、エアー発生機構2が動作するとき、ダ
クト21内に生じるエアー流の一部は流入口23
より通路24を経て中空エアーチヤンバー3内へ
流入し、エアー流の残りはダクト21より後方へ
勢い噴出し、噴出反力が船体1に推力としてゆ
く。前記中空エアーチヤンバー3内にエアーが充
満し且つ圧力が上昇した時、エアー圧力はチヤン
バー3内で調整され各可撓性ノズル38よりチヤ
ンバー3に囲まれた船底12下の圧力エアー室4
に噴出する。チヤンバー3内および圧力エアー室
4の圧力が徐々に上昇して船体1が浮上し、第1
図に示す如く、チヤンバー3がエアー膨脹し切つ
た後、更にチヤンバー3内へ流入するエアーはチ
ヤンバー底部34の噴出孔36より下方へ噴出
し、斯る噴出によるエアー室5内の圧力低下によ
り船体1が下がり、再びエアーチヤンバー3から
のエアー噴出によりエアー室4内の圧力が上昇し
て船体1が浮上する繰返し動作によつて、船体1
はエアー浮上し、前記ダクト21からの噴出反力
によつて推進するのである。旋回走行によいて、
エアー室4に高波が生じるが、可撓性ノズル38
の噴射口39は船底12近傍に開口しているた
め、高波は届かず、従つて水面走行では水、陸上
走行では砂等の侵入は全くなく、構成簡易にして
所期の目的を達成した効果を有す。
Therefore, when the air generation mechanism 2 operates, a part of the air flow generated in the duct 21 flows through the inlet 23.
The remaining air flow flows into the hollow air chamber 3 through the passage 24, and the rest of the air flow is ejected rearward from the duct 21, and the ejection reaction force is applied to the hull 1 as a thrust force. When the hollow air chamber 3 is filled with air and the pressure rises, the air pressure is regulated within the chamber 3 and sent from each flexible nozzle 38 to the pressure air chamber 4 below the ship's bottom 12 surrounded by the chamber 3.
gushes out. The pressure inside the chamber 3 and the pressure air chamber 4 gradually increases, the hull 1 rises, and the first
As shown in the figure, after the chamber 3 is fully inflated with air, the air further flowing into the chamber 3 is ejected downward from the ejection hole 36 in the chamber bottom 34, and the pressure in the air chamber 5 due to this ejection is reduced, causing the hull 1 lowers, the pressure inside the air chamber 4 rises again due to the air jet from the air chamber 3, and the hull 1 rises.
is floated by air and propelled by the ejection reaction force from the duct 21. Due to turning movement,
High waves occur in the air chamber 4, but the flexible nozzle 38
Since the injection port 39 opens near the bottom 12 of the ship, high waves do not reach it, and therefore there is no intrusion of water when traveling on water or sand when traveling on land, which has the effect of simplifying the configuration and achieving the intended purpose. has.

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

第1図は全体の側面図、第2図は第1図A−A
線に沿う概略断面図、第3図は説明用概略断面図
である。 1……船底、12……船底、2……エアー発生
機構、3……中空エアーチヤンバー、37……噴
出口、38……ノズル、39……噴射口、4……
圧力エアー室。
Figure 1 is the overall side view, Figure 2 is Figure 1 A-A
FIG. 3 is a schematic cross-sectional view along the line, and FIG. 3 is a schematic cross-sectional view for explanation. DESCRIPTION OF SYMBOLS 1...Bottom, 12...Bottom, 2...Air generation mechanism, 3...Hollow air chamber, 37...Ejection port, 38...Nozzle, 39...Ejection port, 4...
Pressure air chamber.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 船体1に推力および浮力を発生させるエアー発
生機構2と、該エアー発生機構2に連通して船底
の外周縁に沿いスカート状に配設され、底面には
船底12の近傍に等間隔複数のエアー噴出口37
を開設した中空エアーチヤンバー3とを備え、該
チヤンバー3に囲まれた船底下に浮揚用圧力エア
ー室4を形成するようにしたエアークツシヨン艇
において、前記各エアー噴出口37にはそれぞれ
可撓性ノズル38の基端が連設され、先端噴射口
39を船底12に近接且つ斜めに対向して成るを
特徴とするエアークツシヨン艇における浮揚エア
ー噴出装置。
An air generation mechanism 2 that generates thrust and buoyancy in the hull 1, and a plurality of air generators connected to the air generation mechanism 2 and arranged in a skirt shape along the outer periphery of the bottom of the ship, and arranged near the bottom 12 at equal intervals. Spout 37
In the air traction boat, which is equipped with a hollow air chamber 3 having a hollow air chamber 3, and a pressure air chamber 4 for flotation is formed under the bottom surrounded by the chamber 3, each air outlet 37 has a A floating air jetting device for an aircraft, characterized in that flexible nozzles 38 are connected at their base ends, and their tip jetting ports 39 are located close to and diagonally opposed to the ship's bottom 12.
JP12409784U 1984-08-13 1984-08-13 Floating air jet device in air cushion boat Granted JPS6138265U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12409784U JPS6138265U (en) 1984-08-13 1984-08-13 Floating air jet device in air cushion boat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12409784U JPS6138265U (en) 1984-08-13 1984-08-13 Floating air jet device in air cushion boat

Publications (2)

Publication Number Publication Date
JPS6138265U JPS6138265U (en) 1986-03-10
JPH023972Y2 true JPH023972Y2 (en) 1990-01-30

Family

ID=30682828

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12409784U Granted JPS6138265U (en) 1984-08-13 1984-08-13 Floating air jet device in air cushion boat

Country Status (1)

Country Link
JP (1) JPS6138265U (en)

Also Published As

Publication number Publication date
JPS6138265U (en) 1986-03-10

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