JPH1035481A - Air cushion ship with means for adjusting internal pressure in stern seal - Google Patents

Air cushion ship with means for adjusting internal pressure in stern seal

Info

Publication number
JPH1035481A
JPH1035481A JP21514396A JP21514396A JPH1035481A JP H1035481 A JPH1035481 A JP H1035481A JP 21514396 A JP21514396 A JP 21514396A JP 21514396 A JP21514396 A JP 21514396A JP H1035481 A JPH1035481 A JP H1035481A
Authority
JP
Japan
Prior art keywords
stern seal
internal pressure
air
air cushion
stern
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Withdrawn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
JP21514396A
Other languages
Japanese (ja)
Inventor
Naoji Toki
直二 土岐
Akira Ishikawa
暁 石川
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 JP21514396A priority Critical patent/JPH1035481A/en
Publication of JPH1035481A publication Critical patent/JPH1035481A/en
Withdrawn legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To prevent increase of resistance caused by the interference of waves generated in an air cushion chamber under the low speed condition with a stern seal by reducing pneumatic pressure in the air bag-like stern seal lower than pneumatic pressure in planned speed during sailing with ship speed lower than the planned speed. SOLUTION: High pressure air sent through a duct 7 out of a feed fan 4 driven by an engine is supplied from a new charge port 6 to an engine cushion chamber 3. Also, the high pressure air is supplied from the same feed fan 4 through a duct 7a to an air bag-like stern seal 2a. A movable damper 9a as a means to adjust the internal pressure in the stern seal is provided on the way of the duct 7a. In the low speed sailing, a controller 13 controls a movable damper 9a through an operating mechanism 14 on the basis of a detecting signal from a ship speed sensor 12 to adjust the internal pressure in the stern seal 2a to a value lower than a predetermined value balancing with planned speed, preferably adjust temporarily the internal pressure lower than that in the air cushion chamber 3.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、船体下部に形成さ
れたエアクッション室の空気圧で船体を浮上させ抵抗の
少ない状態で航行しうるエアクッション船に関し、特に
エアバッグ状の船尾シールの空気圧を調整できるように
したものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an air cushion ship capable of navigating with low resistance by lifting the hull by the air pressure of an air cushion chamber formed at the lower part of the hull, and more particularly to reducing the air pressure of an airbag-shaped stern seal. It is designed to be adjustable.

【0002】[0002]

【従来の技術】海上を高速で航走するエアクッション船
としては、図5に示すような側壁型のものが一般に採用
されており、両船側部1,1と可撓性の船尾シール2a
および船首シール2bとで囲まれたエアクッション室3
がウェットデッキ5の下方に形成され、同エアクッショ
ン室3に、給気口6を通じて高圧の空気が供給されるよ
うになっている。
2. Description of the Related Art As an air cushion ship that sails at high speed on the sea, a side wall type ship as shown in FIG. 5 is generally adopted, and both sides 1, 1 and a flexible stern seal 2a are provided.
And air cushion chamber 3 surrounded by bow seal 2b
Are formed below the wet deck 5, and high-pressure air is supplied to the air cushion chamber 3 through the air supply port 6.

【0003】すなわち、図6に示すように、エンジン10
で作動する給気ファン4からダクト7および給気口6を
通じてエアクッション室3へ給気されるが、同給気ファ
ン4から送り出される高圧空気はダクト7aおよび給気
口6aを通じてエアバッグ状の船尾シール2aにも供給
されるようになっている。
[0003] That is, as shown in FIG.
Is supplied to the air cushion chamber 3 through the duct 7 and the air supply port 6 from the air supply fan 4 which operates in the above-described manner, and the high-pressure air sent out from the air supply fan 4 is supplied into the air bag-like form through the duct 7a and the air supply port 6a. It is also supplied to the stern seal 2a.

【0004】そして、船尾シール2aの内部にはエアク
ッション室3の空気圧よりも高圧の空気が蓄えられ、そ
の圧力差により船尾シール2aは所定の形状に保たれる
ようになっており、上記圧力差は給気ファン4から高圧
空気を導くダクト7,7aの流通抵抗を適切に設定する
ことによって保たれる。
[0004] Air having a pressure higher than the air pressure of the air cushion chamber 3 is stored inside the stern seal 2a, and the pressure difference keeps the stern seal 2a in a predetermined shape. The difference is maintained by appropriately setting the flow resistance of the ducts 7 and 7a that guide the high-pressure air from the air supply fan 4.

【0005】[0005]

【発明が解決しようとする課題】ところで、前述のよう
な従来のエアクッション船の平水中における抵抗特性を
模型実験により求めたところ、図7に示すような結果が
得られた。図7のグラフから明らかなように、船速の比
較的低いところで過渡的に抵抗の大きくなる部分8があ
り、その原因について究明した結果、次のようなことが
明らかになった。すなわち、図8に示すように、航走中
におけるエアクッション室3内の水面15には、計画速力
では波を生じることが無く、この水面15に適した船尾シ
ール2aの内部の空気圧で同船尾シール2aの形状が設
定されているが、計画速力に到達する前の低速状態では
エアクッション室3内の水面に破線で示すような波15a
を生じて船尾シール2aの下端部と干渉し、これにより
抵抗が一時的にに増大することが判明した。
The resistance characteristics of the conventional air cushion ship in plain water as described above were determined by a model test, and the results shown in FIG. 7 were obtained. As is apparent from the graph of FIG. 7, there is a portion 8 where the resistance transiently increases at a relatively low ship speed, and as a result of investigating the cause, the following has been clarified. That is, as shown in FIG. 8, the water surface 15 in the air cushion chamber 3 during the cruising does not generate waves at the planned speed, and the stern is formed by the air pressure inside the stern seal 2a suitable for the water surface 15. Although the shape of the seal 2a is set, in a low-speed state before reaching the planned speed, a wave 15a as shown by a broken line is formed on the water surface in the air cushion chamber 3.
And interfered with the lower end of the stern seal 2a, thereby temporarily increasing the resistance.

【0006】そこで本発明は上述の知見に基づき、航走
を開始してから計画速力に到達する前の低速状態でエア
クッション室内に生じる波と船尾シールとの干渉に起因
する抵抗の増大を防止できるようにした船尾シール内圧
調整手段付きエアクッション船を提供することを課題と
する。
Accordingly, the present invention, based on the above findings, prevents an increase in resistance due to interference between a wave generated in the air cushion chamber and a stern seal in a low speed state after starting cruising and before reaching a planned speed. An object of the present invention is to provide an air cushion ship with stern seal internal pressure adjusting means that can be made.

【0007】[0007]

【課題を解決するための手段】前述の課題を解決するた
め、本発明の船尾シール内圧調整手段付きエアクッショ
ン船は、船体の下部に両船側部と可撓性の船尾シールお
よび船首シールとで囲まれたエアクッション室をそなえ
るエアクッション船において、上記船尾シールがエアバ
ッグ状に形成され、計画速力よりも低い船速で航走する
際に上記エアクッション室内の水面に生じる波が上記エ
アバッグ状の船尾シールの下端部と干渉するのを抑制す
べく、同船尾シールの内部の空気圧を低船速時には計画
速力の際の空気圧よりも低下させる船尾シール内圧調整
手段が設けられたことを特徴としている。
SUMMARY OF THE INVENTION In order to solve the above-mentioned problems, an air cushion ship with stern seal internal pressure adjusting means of the present invention comprises a stern seal, a flexible stern seal and a bow seal at the lower part of the hull. In an air cushion ship having an enclosed air cushion chamber, the stern seal is formed in the shape of an airbag, and waves generated on the water surface in the air cushion chamber when sailing at a boat speed lower than a planned speed are generated by the airbag. In order to suppress interference with the lower end of the stern seal, a stern seal internal pressure adjusting means is provided for reducing the air pressure inside the stern seal at a low ship speed from the air pressure at the planned speed. And

【0008】上述の本発明のエアクッション船では、計
画速力よりも低い船速で航走する際に、船尾シール内の
空気圧が、船尾シール内圧調整手段により計画速力の際
の空気圧よりも低い状態に調整されて、同船尾シールの
エアバッグとしての膨らみが減少し、エアクッション室
内の高圧空気は船尾シールを押し上げて後方へ流れ出す
ので、エアクッション室内の水面に低速航走時の波を生
じても、同船尾シールの下端部が波と干渉するのを緩和
され、これにより船速の低いところで過渡的に抵抗の増
大を招いていた従来の不具合が解消するようになる。
In the above-described air cushion ship of the present invention, the state in which the air pressure in the stern seal is lower than the air pressure at the planned speed by the stern seal internal pressure adjusting means when the ship is sailing at a speed lower than the planned speed. The stern seal reduces the inflation as an airbag, and the high-pressure air in the air cushion room pushes up the stern seal and flows backward, causing waves during low-speed cruising on the water surface in the air cushion room. In addition, the lower end of the stern seal can be prevented from interfering with the waves, thereby solving the conventional problem that caused the resistance to increase transiently at low ship speeds.

【0009】そして、上記船尾シール内圧調整手段が、
給気ファンから上記船尾シールへ至るダクトの途中に設
けられた可動ダンパーとして構成されると、同可動ダン
パーにより船尾シール内への給気量が的確に調整され、
これにより船尾シールの内圧が低速航行時には適切に低
減されるようになる。
The stern seal internal pressure adjusting means includes:
When configured as a movable damper provided in the middle of the duct from the air supply fan to the stern seal, the amount of air supplied into the stern seal is accurately adjusted by the movable damper,
As a result, the internal pressure of the stern seal is appropriately reduced during low-speed navigation.

【0010】また、上記船尾シール内圧調整手段が、上
記船尾シールへ給気する給気ファンの可調整式インレッ
トガイドベーンとして構成されてもよく、この場合も船
尾シールの内圧が的確に調整され、低速航行時には船尾
シール下端部がエアクッション室内の水面の波と干渉し
ないように、船尾シールの内圧が低減される。
Further, the stern seal internal pressure adjusting means may be configured as an adjustable inlet guide vane of an air supply fan for supplying air to the stern seal. In this case, the internal pressure of the stern seal is also adjusted accurately. During low speed navigation, the internal pressure of the stern seal is reduced so that the lower end of the stern seal does not interfere with waves on the water surface in the air cushion chamber.

【0011】さらに、上記船尾シール内圧調整手段が、
上記船尾シールへ給気する給気ファンの駆動用エンジン
の出力調整手段として構成される場合も、低速航走時に
は船尾シールの内圧を的確に減少させて、同船尾シール
の下端部とエアクッション室内の波との干渉が防止され
るようになる。
Further, the stern seal internal pressure adjusting means includes:
When configured as an output adjusting means of an engine for driving an air supply fan for supplying air to the stern seal, the internal pressure of the stern seal is accurately reduced during low-speed cruising, so that the lower end of the stern seal and the air cushion chamber are provided. Interference with other waves is prevented.

【0012】また、上記船尾シール内圧調整手段を、船
速センサからの検出信号に応じて制御する制御装置が設
けられると、低速航行時に船尾シール内圧を低下させる
調整が自動的に行なわれるようになり、これにより船尾
シール下端部とエアクッション室内の波との干渉が適切
に防止されるようになる。
If a control device is provided for controlling the stern seal internal pressure adjusting means in accordance with the detection signal from the hull speed sensor, the adjustment for reducing the stern seal internal pressure during low speed navigation is automatically performed. As a result, the interference between the lower end of the stern seal and the waves in the air cushion chamber is appropriately prevented.

【0013】[0013]

【発明の実施の形態】以下、図面により本発明の実施の
形態について説明すると、図1は本発明の第1実施形態
としての船尾シール内圧調整手段付きエアクッション船
の要部を示す縦断面図、図2は本発明の第2実施形態と
しての船尾シール内圧調整手段付きエアクッション船の
要部を示す縦断面図、図3は本発明の第3実施形態とし
ての船尾シール内圧調整手段付きエアクッション船の要
部を示す縦断面図、図4は本発明の第4実施形態として
の船尾シール内圧調整手段付きエアクッション船の要部
を示す縦断面図である。
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a longitudinal sectional view showing an essential part of an air cushion ship with stern seal internal pressure adjusting means according to a first embodiment of the present invention. FIG. 2 is a longitudinal sectional view showing an essential part of an air cushion ship with stern seal internal pressure adjusting means according to a second embodiment of the present invention, and FIG. 3 is an air with stern seal internal pressure adjusting means as a third embodiment of the present invention. FIG. 4 is a longitudinal sectional view showing a main part of a cushion ship, and FIG. 4 is a longitudinal sectional view showing a main part of an air cushion ship with stern seal internal pressure adjusting means as a fourth embodiment of the present invention.

【0014】まず本発明の第1実施形態としての船尾シ
ール内圧調整手段付きエアクッション船について説明す
ると、本実施形態の場合も、図5に示した一般的なエア
クッション船と同様に、両船側部1,1と可撓性の船尾
シール2aおよび船首シール2bとで囲まれたエアクッ
ション室3がウェットデッキ5の下方に形成され、同エ
アクッション室3に、給気口6を通じて高圧の空気が供
給されるようになっている。
First, an air cushion ship with stern seal internal pressure adjusting means as a first embodiment of the present invention will be described. In the case of this embodiment as well, like the general air cushion ship shown in FIG. An air cushion chamber 3 surrounded by the parts 1, 1 and the flexible stern seal 2a and the bow seal 2b is formed below the wet deck 5, and high-pressure air is supplied to the air cushion chamber 3 through an air supply port 6. Is supplied.

【0015】すなわち、図1に示すように、エンジン10
で駆動される給気ファン4からダクト7を介して送り出
される高圧空気が給気口6からエアクッション室3へ供
給される。また同じ給気ファン4からダクト7aを通じ
エアバッグ状の船尾シール2aにも高圧空気が供給され
る。
That is, as shown in FIG.
The high-pressure air sent out from the air supply fan 4 driven by the air through the duct 7 is supplied from the air supply port 6 to the air cushion chamber 3. High-pressure air is also supplied from the same air supply fan 4 to the stern seal 2a in the form of an airbag through the duct 7a.

【0016】そして、各ダクト7,7aの流通抵抗を適
切に設定することにより、船尾シール2aの内圧がエア
クッション室3の内圧よりも高くなるようにされ、これ
により船尾シール2aの形状が保たれるようになってい
る。
By appropriately setting the flow resistance of each duct 7, 7a, the internal pressure of the stern seal 2a is made higher than the internal pressure of the air cushion chamber 3, thereby maintaining the shape of the stern seal 2a. It is designed to drip.

【0017】本実施形態では、特にこのエアクッション
船が計画速力よりも低い船速で航行する際にエアクッシ
ョン室3の内部で水面に生じる波(図8の破線15参照)
に対し船尾シール2aの下端部が干渉しないように、す
なわち図7に示す抵抗の局部的な増大部分8を生じない
ように、図1に示すごとく、船尾シール2aの内部の空
気圧を低船速時には計画速力の際の空気圧よりも低下さ
せる船尾シール内圧調整手段として、ダクト7aの途中
に可動ダンパー9aが設けられている。なお本実施形態
ではエアクッション室3へ通じるダクトの途中にも可動
ダンパー9が設けられている。
In the present embodiment, especially when the air cushion ship sails at a speed lower than the planned speed, a wave generated on the water surface inside the air cushion chamber 3 (see a broken line 15 in FIG. 8).
In order to prevent the lower end of the stern seal 2a from interfering, that is, to cause a local increase 8 in the resistance shown in FIG. 7, the air pressure inside the stern seal 2a is reduced at a low ship speed as shown in FIG. A movable damper 9a is provided in the middle of the duct 7a as a means for adjusting the stern seal internal pressure which sometimes lowers the air pressure at the planned speed. In the present embodiment, a movable damper 9 is also provided in the middle of the duct leading to the air cushion chamber 3.

【0018】さらに本実施形態では船速センサ12からの
検出信号に基づき可動ダンパー9aの操作機構14を制御
して船尾シール2aの内圧を一時的に低下させる制御装
置13が設けられている。
Further, in this embodiment, there is provided a control device 13 for controlling the operation mechanism 14 of the movable damper 9a based on the detection signal from the boat speed sensor 12 to temporarily reduce the internal pressure of the stern seal 2a.

【0019】模型実験結果を示す図10から明らかなよ
うに、船尾シールの空気圧が計画速力に見合う所定の値
の場合の平水中抵抗特性(実線グラフ)と、船尾シール
の空気圧をエアクッション室内の圧力よりも低くした場
合の平水中抵抗特性(破線グラフ)とからみて、船速が
a〜bの領域では破線グラフの抵抗特性をもつようにし
た方が有利である。したがって、制御装置13は、船速セ
ンサ12からの検出信号に基づき、船速がa〜bの領域で
は操作機構14を介し可動ダンパー9aを制御して、船尾
シール2aの内圧を計画速力に見合う所定値よりも低く
するように調整し、好ましくはエアクッション室3の内
圧よりも一時的に低くするように調整する。
As is clear from FIG. 10 showing the results of the model test, the underwater resistance characteristics (solid line graph) when the air pressure of the stern seal is a predetermined value corresponding to the planned speed, and the air pressure of the stern seal in the air cushion chamber are shown. In view of the underwater resistance characteristics when the pressure is lower than the pressure (broken line graph), it is more advantageous to have the resistance characteristics as indicated by the broken line graph in the region where the boat speed is ab. Therefore, the control device 13 controls the movable damper 9a via the operating mechanism 14 in the region where the boat speed is ab in accordance with the detection signal from the boat speed sensor 12, and matches the internal pressure of the stern seal 2a with the planned speed. The pressure is adjusted to be lower than a predetermined value, and preferably, the pressure is temporarily lowered to be lower than the internal pressure of the air cushion chamber 3.

【0020】このようにして、本実施形態の船尾シール
内圧調整手段付きエアクッション船では、計画速力より
も低い船速で航走する際に、船尾シール2a内の空気圧
が、船尾シール内圧調整手段としての可動ダンパー9a
により計画速力の際の空気圧よりも低い状態に調整され
て、同船尾シール2aのエアバッグとしての膨らみが、
図9に示すように点線図示の状態から実線図示の状態に
減少し、エアクッション室3内の高圧空気は船尾シール
2aを押し上げて後方へ流れ出るので、エアクッション
室3内の水面に低速航走時の波を生じても、同船尾シー
ル2aの下端部と波との干渉が回避され、これにより船
速の低いところで過渡的に抵抗の増大を招いていた従来
の不具合が解消するようになる。
As described above, in the air cushion ship with the stern seal internal pressure adjusting means of the present embodiment, the air pressure in the stern seal 2a is reduced by the air pressure in the stern seal internal pressure adjusting means when traveling at a ship speed lower than the planned speed. Movable damper 9a as
Is adjusted to a state lower than the air pressure at the time of the planned speed, so that the stern seal 2a inflates as an airbag,
As shown in FIG. 9, the state shown by the dotted line is reduced to the state shown by the solid line, and the high-pressure air in the air cushion chamber 3 pushes up the stern seal 2a and flows backward. Even when the time wave occurs, the interference between the wave and the lower end of the stern seal 2a is avoided, thereby solving the conventional problem that caused the resistance to increase transiently at a low ship speed. .

【0021】そして、船尾シール内圧調整手段が、本実
施形態のごとく、給気ファン10から船尾シール2aへ至
るダクト7aの途中に設けられた可動ダンパー9aとし
て構成されると、同可動ダンパー9aにより船尾シール
2a内への給気量が的確に調整され、これにより船尾シ
ール2aの内圧が低速航行時には適切に低減されるよう
になる。
When the stern seal internal pressure adjusting means is configured as a movable damper 9a provided in the middle of a duct 7a from the air supply fan 10 to the stern seal 2a as in the present embodiment, the movable damper 9a The amount of air supplied into the stern seal 2a is accurately adjusted, so that the internal pressure of the stern seal 2a is appropriately reduced during low-speed navigation.

【0022】次に本発明の第2実施形態では、図2に示
すように、第1実施形態と同様に船体下部にエアクッシ
ョン室3を形成されたエアクッション船において、エア
バッグ状の船尾シール2aの内圧調整手段が、エンジン
10で駆動される給気ファン4aの可調整式インレットガ
イドベーン11aとして構成されている。
Next, in a second embodiment of the present invention, as shown in FIG. 2, in an air cushion ship having an air cushion chamber 3 formed in the lower part of the hull similarly to the first embodiment, an air bag-shaped stern seal is provided. The internal pressure adjusting means of 2a is an engine
It is configured as an adjustable inlet guide vane 11a of an air supply fan 4a driven by 10.

【0023】なお、本実施形態では、エンジン10で駆動
される他の給気ファン4からダクト7および給気口6を
介してエアクッション室3への給気が行なわれ、その給
気ファン4にも可調整式インレットガイドベーン11aが
設けられている。
In the present embodiment, air is supplied from another air supply fan 4 driven by the engine 10 to the air cushion chamber 3 through the duct 7 and the air supply port 6. Also, an adjustable inlet guide vane 11a is provided.

【0024】上述の構成により、この第2実施形態の場
合も、計画速力より低い船速で航走する際には船尾シー
ル用の給気ファン4aにおける可調整式インレットガイ
ドベーン11aを絞って船尾シール2aの内圧を低下させ
る操作が行われ、これにより船尾シール2aの下端部が
エアクッション室3内の水面の波と干渉するのを防止す
ることができる。したがって、図10に示す船速a〜b
の範囲(低速状態)では、破線グラフの特性をもたせる
ことができ、抵抗の局部的な増大部分を回避することが
できる。
With the above-described structure, also in the second embodiment, when the ship is running at a ship speed lower than the planned speed, the adjustable inlet guide vane 11a of the air supply fan 4a for the stern seal is throttled to reduce the stern. An operation of lowering the internal pressure of the seal 2a is performed, whereby the lower end of the stern seal 2a can be prevented from interfering with waves on the water surface in the air cushion chamber 3. Therefore, the ship speeds a to b shown in FIG.
In the range (low speed state), the characteristics of the dashed line graph can be provided, and a local increase in resistance can be avoided.

【0025】図3に示す本発明の第3実施形態では、前
述の第2実施形態と同様にエアバッグ状の船尾シール2
aの内圧調整手段として、エンジン10で駆動される給気
ファン4aの可調整式インレットガイドベーン11aが設
けられるほか、その操作の自動化をはかるため、船速セ
ンサ12からの検出信号に応じ可調整式インレットガイド
ベーン11aの操作機構14を制御する制御装置13が設けら
れている。このようにして、この第3実施形態では、船
尾シール2aの内圧を、計画速力よりも低い船速時に一
時的に低下させて、抵抗特性における局部的な増大部分
(図10の符号8参照)を回避する操作が、自動的に行
なわれるようになる。
In a third embodiment of the present invention shown in FIG. 3, an airbag-shaped stern seal 2 is provided as in the above-described second embodiment.
As means for adjusting the internal pressure of a, an adjustable inlet guide vane 11a of the air supply fan 4a driven by the engine 10 is provided. In addition, in order to automate the operation, the adjustable guide guide vane 11a is adjusted according to a detection signal from the boat speed sensor 12. A control device 13 for controlling an operation mechanism 14 of the type inlet guide vane 11a is provided. In this manner, in the third embodiment, the internal pressure of the stern seal 2a is temporarily reduced at a boat speed lower than the planned speed, and a local increase in resistance characteristics (see reference numeral 8 in FIG. 10). Is automatically performed.

【0026】次に図4に示す本発明の第4実施形態で
は、前述の第2実施形態と同様に船体下部にエアクッシ
ョン室3を形成されたエアクッション船において、エア
バッグ状の船尾シール2aへダクト7aを介し高圧空気
を供給する給気ファン4aの駆動用エンジン10aが、出
力を調整されるようになっており、これにより船尾シー
ル2aの内圧が調整される。
Next, in a fourth embodiment of the present invention shown in FIG. 4, in an air cushion ship having an air cushion chamber 3 formed in the lower part of the hull similarly to the second embodiment described above, an air bag-shaped stern seal 2a is provided. The output of the driving engine 10a of the air supply fan 4a that supplies high-pressure air through the air duct 7a is adjusted, whereby the internal pressure of the stern seal 2a is adjusted.

【0027】すなわち、船尾シール内圧調整手段とし
て、給気ファン4aの駆動用エンジン10aの出力調整手
段が設けられている。なお、本実施形態ではエアクッシ
ョン室3の圧力と船尾シール2aの内圧との関係を調整
できるようにするため、エアクッション室3に高圧空気
を送る給気ファン4とその駆動用エンジン10とが、船尾
シール系とは別個に設けられている。
That is, as the stern seal internal pressure adjusting means, an output adjusting means of the driving engine 10a of the air supply fan 4a is provided. In the present embodiment, in order to adjust the relationship between the pressure of the air cushion chamber 3 and the internal pressure of the stern seal 2a, the air supply fan 4 that sends high-pressure air to the air cushion chamber 3 and the engine 10 for driving the air supply chamber are used. The stern seal system is provided separately.

【0028】この第4実施形態の場合も、低速航走時に
船尾シール2aの内圧を低下させたいときは船尾シール
用のファン駆動エンジン10aの出力を下げ、船速が高速
になって船尾シール2aの内圧を上げたいときには設計
状態でファン駆動用エンジン10aの運転が行なわれる。
Also in the case of the fourth embodiment, when it is desired to reduce the internal pressure of the stern seal 2a during low speed traveling, the output of the stern seal fan drive engine 10a is reduced, and the stern seal 2a When it is desired to increase the internal pressure, the fan drive engine 10a is operated in a designed state.

【0029】この第4実施形態の場合もファン駆動用エ
ンジン10aの運転制御の自動化が可能であり、船速セン
サからの検出信号に応じ制御装置を介してファン駆動用
エンジン10aを制御することができ、これにより低速航
行時には船尾シール2aの内圧を下げて、同シールの下
端部とエアクッション室3内の波との干渉が適切に防止
されるようになる。
Also in the case of the fourth embodiment, it is possible to automate the operation control of the fan driving engine 10a, and it is possible to control the fan driving engine 10a via a control device according to a detection signal from a boat speed sensor. As a result, the internal pressure of the stern seal 2a is reduced during low-speed navigation, so that interference between the lower end of the seal and the wave in the air cushion chamber 3 is appropriately prevented.

【0030】[0030]

【発明の効果】以上詳述したように、本発明の船尾シー
ル内圧調整手段付き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) 計画速力よりも低い船速で航走する際に、船尾シー
ル内の空気圧が、船尾シール内圧調整手段により計画速
力の際の空気圧よりも低い状態に調整されて、同船尾シ
ールのエアバッグとしての膨らみが減少し、エアクッシ
ョン室内の高圧空気は船尾シールを押し上げて後方へ流
れ出るので、エアクッション室内の水面に低速航走時の
波を生じても、同船尾シールの下端部が波と干渉するの
を緩和され、これにより船速の低いところで過渡的に抵
抗の増大を招いていた従来の不具合が解消するようにな
る。 (2) 上記船尾シール内圧調整手段が、給気ファンから上
記船尾シールへ至るダクトの途中に設けられた可動ダン
パーとして構成されると、同可動ダンパーにより船尾シ
ール内への給気量が的確に調整され、これにより船尾シ
ールの内圧が低速航行時には適切に低減されるようにな
る。 (3) 上記船尾シール内圧調整手段が、上記船尾シールへ
給気する給気ファンの可調整式インレットガイドベーン
として構成されてもよく、この場合も船尾シールの内圧
が的確に調整され、低速航行時には船尾シール下端部が
エアクッション室内の水面の波と干渉しないように、船
尾シールの内圧が低減される。 (4) 上記船尾シール内圧調整手段が、上記船尾シールへ
給気する給気ファンの駆動用エンジンの出力調整手段と
して構成される場合も、低速航走時には船尾シールの内
圧を的確に減少させて、同船尾シールの下端部とエアク
ッション室内の波との干渉が防止されるようになる。 (5) 上記船尾シール内圧調整手段を、船速センサからの
検出信号に応じて制御する制御装置が設けられると、低
速航行時に船尾シール内圧を低下させる調整が自動的に
行なわれるようになり、これにより船尾シール下端部と
エアクッション室内の波との干渉が適切に防止されるよ
うになる。
As described above, according to the air cushion ship with the stern seal internal pressure adjusting means of the present invention, the following effects can be obtained. (1) When sailing at a ship speed lower than the planned speed, the air pressure in the stern seal is adjusted to be lower than the air pressure at the planned speed by Since the inflation as a bag is reduced, and the high-pressure air in the air cushion room pushes up the stern seal and flows backward, even if a low-speed cruising wave occurs on the water surface in the air cushion room, the lower end of the stern seal has a wave. This alleviates the conventional problem that has caused a transient increase in resistance at low ship speeds. (2) When the stern seal internal pressure adjusting means is configured as a movable damper provided in the middle of the duct from the air supply fan to the stern seal, the movable damper can accurately supply air into the stern seal. It is adjusted so that the internal pressure of the stern seal is appropriately reduced at low speeds. (3) The stern seal internal pressure adjusting means may be configured as an adjustable inlet guide vane of an air supply fan for supplying air to the stern seal, and also in this case, the internal pressure of the stern seal is accurately adjusted, and Sometimes the internal pressure of the stern seal is reduced so that the lower end of the stern seal does not interfere with the waves on the water surface in the air cushion chamber. (4) Even when the stern seal internal pressure adjusting means is configured as an output adjusting means of an engine for driving an air supply fan for supplying air to the stern seal, the internal pressure of the stern seal is accurately reduced during low speed traveling. Thus, interference between the lower end of the stern seal and the waves in the air cushion chamber is prevented. (5) If a control device is provided for controlling the stern seal internal pressure adjusting means in accordance with a detection signal from the ship speed sensor, adjustment to reduce the stern seal internal pressure during low-speed navigation will be automatically performed, As a result, interference between the lower end of the stern seal and the waves in the air cushion chamber can be appropriately prevented.

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

【図1】本発明の第1実施形態としての船尾シール内圧
調整手段付きエアクッション船の要部を示す縦断面図で
ある。
FIG. 1 is a longitudinal sectional view showing a main part of an air cushion ship with stern seal internal pressure adjusting means as a first embodiment of the present invention.

【図2】本発明の第2実施形態としての船尾シール内圧
調整手段付きエアクッション船の要部を示す縦断面図で
ある。
FIG. 2 is a longitudinal sectional view showing a main part of an air cushion ship with stern seal internal pressure adjusting means as a second embodiment of the present invention.

【図3】本発明の第3実施形態としての船尾シール内圧
調整手段付きエアクッション船の要部を示す縦断面図で
ある。
FIG. 3 is a longitudinal sectional view showing a main part of an air cushion ship with stern seal internal pressure adjusting means as a third embodiment of the present invention.

【図4】本発明の第4実施形態としての船尾シール内圧
調整手段付きエアクッション船の要部を示す縦断面図で
ある。
FIG. 4 is a longitudinal sectional view showing a main part of an air cushion ship with stern seal internal pressure adjusting means as a fourth embodiment of the present invention.

【図5】エアクッション船を斜め下方からみた斜視図で
ある。
FIG. 5 is a perspective view of the air cushion ship as viewed obliquely from below.

【図6】従来のエアクッション船の要部を示す縦断面図
である。
FIG. 6 is a longitudinal sectional view showing a main part of a conventional air cushion ship.

【図7】従来のエアクッション船の平水中抵抗特性を模
型実験結果として示すグラフである。
FIG. 7 is a graph showing the resistance characteristics of a conventional air cushion ship in plain water as model test results.

【図8】従来のエアクッション船の低速航行時の状態を
示す説明図である。
FIG. 8 is an explanatory diagram showing a state of a conventional air cushion ship during low-speed navigation.

【図9】本発明のエアクッション船の低速航行時の状態
を示す説明図である。
FIG. 9 is an explanatory diagram showing a state of the air cushion ship of the present invention when traveling at a low speed.

【図10】本発明のエアクッション船の船尾シール内圧調
整による平水中抵抗特性を模型実験結果として示すグラ
フである。
FIG. 10 is a graph showing, as a model test result, resistance characteristics in plain water by adjusting the internal pressure of the stern seal of the air cushion ship of the present invention.

【符号の説明】[Explanation of symbols]

1 船側部 2a 船尾シール 2b 船首シール 3 エアクッション室 4,4a 給気ファン 5 ウェットデッキ 6 給気口 7,7a ダクト 8 局部的な抵抗増大部分 9,9a 可動ダンパー 10,10a 給気ファン駆動用エンジン 11,11a 可調整式インレットガイドベーン 12 船速センサ 13 制御装置 14 操作機構 15 エアクッション室内の水面 15a 波 DESCRIPTION OF SYMBOLS 1 Ship side part 2a Stern seal 2b Bow seal 3 Air cushion room 4,4a Air supply fan 5 Wet deck 6 Air supply port 7,7a Duct 8 Local resistance increase part 9,9a Movable damper 10,10a For air supply fan drive Engine 11, 11a Adjustable inlet guide vane 12 Ship speed sensor 13 Control device 14 Operating mechanism 15 Water surface in air cushion room 15a Wave

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 船体の下部に両船側部と可撓性の船尾シ
ールおよび船首シールとで囲まれたエアクッション室を
そなえるエアクッション船において、上記船尾シールが
エアバッグ状に形成され、計画速力よりも低い船速で航
走する際に上記エアクッション室内の水面に生じる波が
上記エアバッグ状の船尾シールの下端部と干渉するのを
抑制すべく、同船尾シールの内部の空気圧を低船速時に
は計画速力の際の空気圧よりも低下させる船尾シール内
圧調整手段が設けられたことを特徴とする、船尾シール
内圧調整手段付きエアクッション船。
1. An air cushion ship having an air cushion chamber at the lower part of a hull surrounded by both side portions and a flexible stern seal and a bow seal, wherein the stern seal is formed in the shape of an airbag, and In order to prevent waves generated on the water surface in the air cushion chamber from interfering with the lower end of the airbag-shaped stern seal when traveling at a lower ship speed, the air pressure inside the stern seal is lowered. An air cushion ship with stern seal internal pressure adjusting means, characterized in that stern seal internal pressure adjusting means for lowering the air pressure at a speed lower than the planned speed is provided.
【請求項2】 上記船尾シール内圧調整手段が、給気フ
ァンから上記船尾シールへ至るダクトの途中に設けられ
た可動ダンパーとして構成されたことを特徴とする、請
求項1に記載の船尾シール内圧調整手段付きエアクッシ
ョン船。
2. The stern seal internal pressure according to claim 1, wherein the stern seal internal pressure adjusting means is configured as a movable damper provided in the middle of a duct from an air supply fan to the stern seal. Air cushion ship with adjustment means.
【請求項3】 上記船尾シール内圧調整手段が、上記船
尾シールへ給気する給気ファンの可調整式インレットガ
イドベーンとして構成されたことを特徴とする、請求項
1に記載の船尾シール内圧調整手段付きエアクッション
船。
3. The stern seal internal pressure adjustment according to claim 1, wherein the stern seal internal pressure adjusting means is configured as an adjustable inlet guide vane of an air supply fan for supplying air to the stern seal. Air cushion ship with means.
【請求項4】 上記船尾シール内圧調整手段が、上記船
尾シールへ給気する給気ファンの駆動用エンジンの出力
調整手段として構成されたことを特徴とする、請求項1
に記載の船尾シール内圧調整手段付きエアクッション
船。
4. The stern seal internal pressure adjusting means is configured as an output adjusting means of an engine for driving an air supply fan for supplying air to the stern seal.
An air cushion ship with a stern seal internal pressure adjusting means according to the above.
【請求項5】 上記船尾シール内圧調整手段を、船速セ
ンサからの検出信号に応じて制御する制御装置が設けら
れたことを特徴とする、請求項1〜4のいずれか1つに
記載の船尾シール内圧調整手段付きエアクッション船。
5. A control device according to claim 1, further comprising a control device for controlling said stern seal internal pressure adjusting means in accordance with a detection signal from a boat speed sensor. Air cushion ship with stern seal internal pressure adjusting means.
JP21514396A 1996-07-26 1996-07-26 Air cushion ship with means for adjusting internal pressure in stern seal Withdrawn JPH1035481A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21514396A JPH1035481A (en) 1996-07-26 1996-07-26 Air cushion ship with means for adjusting internal pressure in stern seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21514396A JPH1035481A (en) 1996-07-26 1996-07-26 Air cushion ship with means for adjusting internal pressure in stern seal

Publications (1)

Publication Number Publication Date
JPH1035481A true JPH1035481A (en) 1998-02-10

Family

ID=16667404

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21514396A Withdrawn JPH1035481A (en) 1996-07-26 1996-07-26 Air cushion ship with means for adjusting internal pressure in stern seal

Country Status (1)

Country Link
JP (1) JPH1035481A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103407443A (en) * 2013-07-11 2013-11-27 哈尔滨工程大学 Hovercraft navigation safety coordination and control method
CN106114487A (en) * 2016-08-31 2016-11-16 何洪波 A kind of high stationarity aircushion vehicle guiding device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103407443A (en) * 2013-07-11 2013-11-27 哈尔滨工程大学 Hovercraft navigation safety coordination and control method
CN106114487A (en) * 2016-08-31 2016-11-16 何洪波 A kind of high stationarity aircushion vehicle guiding device

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