JPH02164657A - Fan duct for small size hovercraft - Google Patents

Fan duct for small size hovercraft

Info

Publication number
JPH02164657A
JPH02164657A JP32131388A JP32131388A JPH02164657A JP H02164657 A JPH02164657 A JP H02164657A JP 32131388 A JP32131388 A JP 32131388A JP 32131388 A JP32131388 A JP 32131388A JP H02164657 A JPH02164657 A JP H02164657A
Authority
JP
Japan
Prior art keywords
fan
air
fan duct
duct
plates
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
JP32131388A
Other languages
Japanese (ja)
Inventor
Takumi Moriwake
巧 守分
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.)
SORETSUKUSU KK
Original Assignee
SORETSUKUSU KK
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 SORETSUKUSU KK filed Critical SORETSUKUSU KK
Priority to JP32131388A priority Critical patent/JPH02164657A/en
Publication of JPH02164657A publication Critical patent/JPH02164657A/en
Pending legal-status Critical Current

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PURPOSE:To simply and exactly divide the air sent from a fan into a propelling air and an air for buoyance by providing partition plates so that the partion plates form a sector by a central point and an outer peripheral circular arc surface of a fan duct. CONSTITUTION:With an air current sent by a fan 2 installed in a fan duct 1, a part of the air current is introduced as a propelling air current (A) into the rear of a hull 3, and the remaining air is introduced as an air current (B) for buoyance into a skirt 5 by means of partition plates 4. In this case, for the partion plates 4, two plates are installed in the axis direction of the fan so that the plates form a sector by a central point and an outer peripheral circular arc surface, and extended from the central direction of the fan 2 to the fan duct 1 and fixed at the leeward direction. A ratio of the air volume for buoyancy to the whole blasted air volume of the fan 2 can thus be exactly set.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は小型ホバークラフトのファンダクトに関するも
のである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a fan duct for a small hovercraft.

(従来の技術) 従来のエンジン−基で浮上と推進を兼ねる型のホバーク
ラフトにおいては直立するファンダクト内に一枚の水平
に設置された仕切り板を設は空気流の何割かを浮上用と
して使うが一般に知られているようl:ファンブレード
の効率は中心から先端まで均一ではなく、そのために従
来のファンダクト内に仕切り板を一枚水平に!2置した
ものでは空気流の何割を浮上用に使うと決めてもその取
り付は位置の設定が非常に困難であった。
(Prior technology) In a conventional engine-based hovercraft that performs both levitation and propulsion, a partition plate installed horizontally in an upright fan duct is used to use a percentage of the air flow for levitation. It is generally known that the efficiency of fan blades is not uniform from the center to the tip, which is why a partition plate is placed horizontally in the conventional fan duct! With the two-position model, even if it was decided to use a percentage of the air flow for levitation, it was very difficult to set the mounting position.

(発明が解決しようとする課M) 本発明は、これら従来技術の問題点を解決するものであ
り、ファンダクト内の空気流から容易に浮上用に使おう
と決定した比率の空気流を取り出せるようにしたもので
ある。
(Problem M to be Solved by the Invention) The present invention solves these problems of the prior art, and makes it possible to easily take out the air flow of the ratio determined to be used for flotation from the air flow in the fan duct. This is what I did.

(課組を解決するための手段) 即ち、本発明はファンダクトの投影面積(全空気流)に
対してその中心点と円弧で形成された任意の角度を持っ
た扇形の投影面II(浮上用空気流)と言う考え方で実
施したものであり一基のファンから推進用と浮上用の二
つの空気流を分離する形式のホバークラフトのファンダ
クト1;おいて、二枚のファン軸方向に設置され、ファ
ンの中心方向からファンダクト方向に伸び、風下方向を
結合した仕切り板を設け、仕切り板によって分離された
空気流を浮上用として使用することを特徴とした小型ホ
バークラフトのファンダクトの構造を要旨とするもので
ある。
(Means for Solving Problems) That is, the present invention provides a fan-shaped projection plane II (levitation This was carried out based on the idea that two air flows for propulsion and levitation are separated from one fan, and two fans are installed in the axial direction in a hovercraft fan duct 1. The structure of a fan duct for a small hovercraft is characterized in that a partition plate is provided that extends from the center of the fan toward the fan duct and connects the leeward direction, and the air flow separated by the partition plate is used for levitation. This is a summary.

(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。(Example) Embodiments of the present invention will be described below with reference to the drawings.

第1図は本発明を実施したホバークラフトのy4WJ図
でファンダクト1の中に設置されたファン2により起こ
された空気流は矢符Aのように一部は推進空気流として
艇体3の後方に、一部は仕切り板4により浮上空気流と
してスカート5内に矢符Bのように導かれる。
Fig. 1 is a y4WJ diagram of a hovercraft in which the present invention is implemented, and the airflow generated by the fan 2 installed in the fan duct 1 is partially behind the hull 3 as a propulsion airflow as shown by arrow A. Then, a part of the air is guided into the skirt 5 as a floating air flow by the partition plate 4 as shown by arrow B.

第2図は本発明の要部拡大した斜視図で仕切り板4の状
態を表し、ファン2によって起こされた空気流の一部は
左右に設けられ風下側を結合された仕切り板4により矢
符Bのように下方に取り込まれ浮上用に使われる。
FIG. 2 is an enlarged perspective view of the main part of the present invention, showing the state of the partition plate 4. A part of the air flow generated by the fan 2 is directed by the partition plate 4 provided on the left and right sides and connected on the leeward side. As shown in B, it is taken downward and used for levitation.

第3図は従来のファンダクトの要部拡大した正面図で仕
切り板4はファンダクトlに対して接線方向に設置され
ていて推進用ダクトAと浮上用ダクトBに各々分離され
ている。
FIG. 3 is an enlarged front view of the main part of a conventional fan duct. A partition plate 4 is installed tangentially to the fan duct 1, and is separated into a propulsion duct A and a floating duct B.

第4図は本発明の要部拡大した正面図でファンダクト1
に対して仕切り板4は扇形で設置されており推進用ダク
ト八と浮上用ダクトBに各々分離されている。
Figure 4 is an enlarged front view of the main parts of the present invention, showing the fan duct 1.
On the other hand, the partition plate 4 is installed in a fan shape and is separated into a propulsion duct 8 and a floating duct B.

第5図は本発明のその池の実施例を示す要部拡大した正
m図でJii影に12r11された仕切り板4の上方に
靜[6を設けており仕切り板4にも静翼の役目を持たす
ことにより推進用ダクトへの送風量を左右均一にするこ
とができる。このことはファンダクト後方に逆進装置を
取り付けた場合非常に有効である。また本発明の仕切り
板4の上部にファン2の回転軸の取り付は部の一端を設
けることも可能である。
Fig. 5 is an enlarged front view of the main part showing the embodiment of the pond of the present invention, and is provided above the partition plate 4 which is shaded 12r11, and the partition plate 4 also plays the role of stator vane. By having this, the amount of air blown to the propulsion duct can be made uniform on the left and right sides. This is very effective when a reversing device is installed behind the fan duct. Further, it is also possible to provide one end of the rotation shaft of the fan 2 on the upper part of the partition plate 4 of the present invention.

また実施例では、すべてファンダクトを垂直に設置した
もので説明しているがファンダクトが水平に設置された
ものでも有効であることは言うまでもない。
Further, in the embodiments, all fan ducts are installed vertically, but it goes without saying that fan ducts installed horizontally are also effective.

(発明の効果) 本発明は、以上説明したように構成されているので、以
下に記載されるような効果を奏する。
(Effects of the Invention) Since the present invention is configured as described above, it produces effects as described below.

ファンの全送風量に対する浮上用空気量の比率を正確に
設定することが出来る。
It is possible to accurately set the ratio of the amount of air for floating to the total amount of air blown by the fan.

そして、ファンダクトの位置を変えることなく仕切り板
の角度を変えることにより浮上用空気量の比率を変える
ことが出来る。
Furthermore, by changing the angle of the partition plate without changing the position of the fan duct, the ratio of the amount of air for floating can be changed.

また、仕切り板を静翼として利用することが出来る。Furthermore, the partition plate can be used as a stationary blade.

また、上方に静翼、もしくは梁を入れることによりファ
ンダクトの補強材として利用出来る。
Also, by inserting stator blades or beams above it, it can be used as a reinforcement material for fan ducts.

さらに、ファンの回転軸の取り付は部としても利用出来
る。
Furthermore, the mounting of the rotation shaft of the fan can also be used as a part.

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

第1図は本発明を実施したホバークラフトの開面図。第
2図はその要部拡大した斜視図、第3図は従来のファン
ダクトの要部拡大した正面図。第4図は本発明のファン
ダクトの要部拡大した正面図、第5図はその他の実施例
のファンダクトの要部拡大した正面図である。 図中の符号を説明すると次のとおりである。
FIG. 1 is an open view of a hovercraft embodying the present invention. FIG. 2 is an enlarged perspective view of the main part of the conventional fan duct, and FIG. 3 is an enlarged front view of the main part of the conventional fan duct. FIG. 4 is an enlarged front view of the essential parts of a fan duct according to the present invention, and FIG. 5 is an enlarged front view of the essential parts of a fan duct according to another embodiment. The symbols in the figure are explained as follows.

Claims (1)

【特許請求の範囲】[Claims] 一基のファンから推進用と浮上用の二つの空気流を分離
する形式の小型ホバークラフトのファンダクトにおいて
、そのファンダクトの中心点とファンダクトの円弧で形
成された扇形を描くような二枚のファン軸方向に設置さ
れファンの中心方向からファンダクト方向に伸び、風下
方向を結合した仕切り板を設け仕切り板によって分離し
た空気流を浮上用として使用することを特徴とした小型
ホバークラフトのファンダクト。
In the fan duct of a small hovercraft, which separates two air flows for propulsion and levitation from one fan, two pieces draw a fan shape formed by the center point of the fan duct and the arc of the fan duct. A fan duct for a small hovercraft characterized by having a partition plate installed in the fan axis direction, extending from the center direction of the fan to the fan duct direction, and connecting the leeward direction, and using the air flow separated by the partition plate for levitation.
JP32131388A 1988-12-19 1988-12-19 Fan duct for small size hovercraft Pending JPH02164657A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP32131388A JPH02164657A (en) 1988-12-19 1988-12-19 Fan duct for small size hovercraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP32131388A JPH02164657A (en) 1988-12-19 1988-12-19 Fan duct for small size hovercraft

Publications (1)

Publication Number Publication Date
JPH02164657A true JPH02164657A (en) 1990-06-25

Family

ID=18131190

Family Applications (1)

Application Number Title Priority Date Filing Date
JP32131388A Pending JPH02164657A (en) 1988-12-19 1988-12-19 Fan duct for small size hovercraft

Country Status (1)

Country Link
JP (1) JPH02164657A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105882340A (en) * 2016-06-12 2016-08-24 中国船舶重工集团公司第七○二研究所 Air-propelled amphibious tidal land ship
CN106080577A (en) * 2016-06-12 2016-11-09 中国船舶重工集团公司第七○二研究所 Air propeller is utilized to advance and the ship of the hull that hovers

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105882340A (en) * 2016-06-12 2016-08-24 中国船舶重工集团公司第七○二研究所 Air-propelled amphibious tidal land ship
CN106080577A (en) * 2016-06-12 2016-11-09 中国船舶重工集团公司第七○二研究所 Air propeller is utilized to advance and the ship of the hull that hovers

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