JPH05178269A - Inter-flap connecting mechanism for hydrofoil - Google Patents
Inter-flap connecting mechanism for hydrofoilInfo
- Publication number
- JPH05178269A JPH05178269A JP3357870A JP35787091A JPH05178269A JP H05178269 A JPH05178269 A JP H05178269A JP 3357870 A JP3357870 A JP 3357870A JP 35787091 A JP35787091 A JP 35787091A JP H05178269 A JPH05178269 A JP H05178269A
- Authority
- JP
- Japan
- Prior art keywords
- hydrofoil
- flap
- key
- flaps
- key metal
- 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- Withdrawn
Links
Landscapes
- Pivots And Pivotal Connections (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、水中翼船の水中翼に関
し、特にその複数のフラップ間の連結機構に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a hydrofoil of a hydrofoil, and more particularly to a coupling mechanism between a plurality of flaps of the hydrofoil.
【0002】[0002]
【従来の技術】一般に、水中翼船の水中翼は、図6に示
すように、水中翼本体11aに複数のフラップ11,12,13が
回動可能にその基端部を枢着されており、駆動機構17に
よって最内側のフラップ13が回動駆動されると、その動
きが隣接するフラップ12に伝えられ、さらにフラップ11
へ順次伝えられて、各フラップが同時に同量だけ回動で
きるように構成されている。2. Description of the Related Art Generally, in a hydrofoil of a hydrofoil, as shown in FIG. 6, a plurality of flaps 11, 12, 13 are rotatably attached to a hydrofoil body 11a at their base ends. When the innermost flap 13 is rotationally driven by the drive mechanism 17, the movement is transmitted to the adjacent flap 12, and the flap 11
The flaps are sequentially transmitted to each flap so that the flaps can simultaneously rotate by the same amount.
【0003】そのため、従来は3枚のフラップ11,12,13
には各隣接端面にキー金物とキー溝とからなる連結機構
が設けられている。Therefore, conventionally, three flaps 11, 12, 13 are used.
Is provided with a connecting mechanism composed of a key hardware and a key groove on each adjacent end face.
【0004】すなわち、図7,図8に示すように、フラ
ップ12のフラップ13との隣接面にキー金物14が突設さ
れ、一方フラップ13のフラップ12との隣接面にキー金物
15を挿入可能なキー溝15が形成されて、両フラップの連
動機構が構成されている。That is, as shown in FIGS. 7 and 8, a key metal fitting 14 is provided on the surface of the flap 12 adjacent to the flap 13 while a key metal fitting 14 is provided on the surface of the flap 13 adjacent to the flap 12.
A key groove 15 into which 15 can be inserted is formed, and an interlocking mechanism of both flaps is configured.
【0005】なお、キー金物14とキー溝15とが直接接触
することによる摩耗を防止するために、両者間に耐摩耗
材料からなるキーライナー16がはめ込まれている。A key liner 16 made of a wear resistant material is fitted between the key hardware 14 and the key groove 15 in order to prevent the key hardware 14 and the key groove 15 from being directly contacted with each other.
【0006】[0006]
【発明が解決しようとする課題】ところで、従来のもの
では、上述のようにキー金物14とキーライナー16および
キー溝15とは平面接触構造となっており、フラップ間の
角度変化を吸収できる構造となっていない。By the way, in the conventional structure, the key metal article 14, the key liner 16 and the key groove 15 have a plane contact structure as described above, and a structure capable of absorbing an angle change between the flaps. Is not.
【0007】したがって、水中翼船の船体が小さく、フ
ラップに作用する荷重が小さい時には(フラップの変形
により生じる)フラップ間の相対運動も小さく従来の構
造で対応可能であるが、船体が大型化しフラップへの作
用荷重が大きくなるとフラップ間の相対運動も大きくな
り、従来構造ではこの運動を吸収できなくなる。その結
果キー金物の疲労破壊やキーライナーの摩耗が大きくな
る、と言った問題が生じる恐れがある。Therefore, when the hull of the hydrofoil is small and the load acting on the flaps is small, the relative motion between the flaps (caused by the deformation of the flaps) is small and the conventional structure can be used, but the hull becomes large and the flaps are large. When the load acting on the flap becomes large, the relative movement between the flaps also becomes large, and the conventional structure cannot absorb this movement. As a result, there is a possibility that problems such as fatigue damage of the key hardware and increased wear of the key liner may occur.
【0008】本発明は、このような問題点の解決をはか
ろうとするもので、水中翼のフラップ連結構造におい
て、キー溝の断面形状を円形状に形成する一方、キー溝
とキー金物との間に半円柱状のスリーブを嵌入して、両
フラップ間に摺動と回動とが許容される構成とすること
により、キー金物の疲労破壊やキーライナーの摩耗を制
御できるようにした、水中翼のフラップ間連結機構を提
供することを目的とする。The present invention is intended to solve such a problem. In the flap connecting structure of the hydrofoil, the key groove is formed to have a circular cross-section while the key groove and the key metal fitting are formed. By inserting a semi-cylindrical sleeve between them and allowing sliding and rotation between both flaps, it is possible to control fatigue fracture of key hardware and wear of key liner. An object is to provide a connecting mechanism between flaps of a wing.
【0009】[0009]
【課題を解決するための手段】上述の目的を達成するた
め、本発明の水中翼のフラップ間連結機構は、水中翼本
体と、基端部を上記水中翼本体に回動可能に取付けられ
た複数のフラップと、隣接配設された上記フラップの間
の連結機構とをそなえ、同連結機構が、一方の上記フラ
ップの端面に突設された直方体形のキー金物と、他方の
上記フラップの端面に形成されて上記キー金物を嵌挿可
能なキー溝とをそなえるとともに、一対の半円柱形のス
リーブが上記キー金物の上下両面にそれぞれ摺動可能に
装着され、上記キー溝に上記一対の半円柱形のスリーブ
を嵌挿可能な円形の凹部が連設されていることを特徴と
している。In order to achieve the above-mentioned object, the hydrofoil flap-to-flap connecting mechanism of the present invention has a hydrofoil body and a base end portion rotatably attached to the hydrofoil body. A plurality of flaps and a connecting mechanism between adjacent flaps are provided, and the connecting mechanism has a rectangular parallelepiped key metal member projecting from the end surface of one of the flaps and the end surface of the other of the flaps. And a pair of semi-cylindrical sleeves are slidably mounted on the upper and lower surfaces of the key metal piece, respectively, and the key groove is inserted into the key groove. It is characterized in that circular recesses into which a cylindrical sleeve can be inserted are continuously provided.
【0010】[0010]
【作用】上述の本発明の水中翼のフラップ間連結機構で
は、フラップ間の相対運動のうち水平面内の運動は、キ
ー金物と半円柱形スリーブとの間の摺動で吸収でき、ま
た角度変化については、円形状のキー溝内をスリーブが
キー金物と一緒に回転することで吸収できる。In the hydrofoil inter-flap coupling mechanism of the present invention described above, of the relative movements between the flaps, movements in the horizontal plane can be absorbed by sliding between the key metal member and the semi-cylindrical sleeve, and the angle changes. With respect to the above, the sleeve can be absorbed by rotating the sleeve together with the key hardware in the circular key groove.
【0011】[0011]
【実施例】以下、図面により本発明の一実施例としての
水中翼のフラップ間連結機構について説明すると、図1
は水中翼を示した斜視図、図2は水中翼の正面図、図3
はフラップ間連結機構を分解して示す斜視図、図4は図
1のA−A矢視断面図、図5は変形例を図4に対応して
示す断面図である。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A flap interlocking mechanism for hydrofoils as an embodiment of the present invention will be described below with reference to the drawings.
Is a perspective view showing the hydrofoil, FIG. 2 is a front view of the hydrofoil, and FIG.
Is an exploded perspective view of the inter-flap connecting mechanism, FIG. 4 is a sectional view taken along the line AA of FIG. 1, and FIG. 5 is a sectional view showing a modified example corresponding to FIG.
【0012】この実施例の水中翼本体1にも、3枚のフ
ラップ2,3,4がそれらの基端部をヒンジピン8によ
って回動可能に取付けられており、最内側のフラップ2
はストラット10内に装備されたリンク機構によって動か
される金物10aにより、矢印で示すように回動駆動され
る。Also in the hydrofoil main body 1 of this embodiment, three flaps 2, 3 and 4 are rotatably attached at their base ends by a hinge pin 8, and the innermost flap 2 is provided.
Is driven to rotate as shown by an arrow by a metal object 10a which is moved by a link mechanism mounted in the strut 10.
【0013】フラップ2の回動を隣接するフラップ3に
伝えるために、次に述べる連結機構が設けられている。In order to transmit the rotation of the flap 2 to the adjacent flap 3, a connecting mechanism described below is provided.
【0014】図3,図4において、フラップ2のフラッ
プ3と隣接する端面に直方体形のキー金物7が突設さ
れ、このキー金物7の上下両面に半円柱形の一対のスリ
ーブ5,5がそれぞれ摺動可能に取付けられている。In FIGS. 3 and 4, a rectangular parallelepiped key metal fitting 7 is provided on the end surface of the flap 2 adjacent to the flap 3, and a pair of semi-cylindrical sleeves 5 and 5 are provided on the upper and lower surfaces of the key metal fitting 7. Each is slidably mounted.
【0015】一方、フラップ2のフラップ3と隣接する
端面にキー金物7を嵌挿可能なキー溝6が形成され、キ
ー溝6に一対の半円柱形のスリーブ5,5を嵌挿可能な
円形の凹部6aが連設されている。On the other hand, a key groove 6 into which a key metal 7 can be inserted is formed on an end surface of the flap 2 adjacent to the flap 3, and a circular shape into which a pair of semi-cylindrical sleeves 5 and 5 can be inserted into the key groove 6. The recesses 6a are continuously provided.
【0016】そして、キー溝6にスリーブ5,5とキー
金物7とを嵌挿して、フラップ2とフラップ3との連結
が行なわれるようになっている。Then, the sleeves 5 and 5 and the key hardware 7 are fitted into the key groove 6 so that the flap 2 and the flap 3 are connected to each other.
【0017】フラップ3とフラップ4との連結もほぼ同
じ構造の連結機構を介して行なわれる。The flaps 3 and 4 are also connected to each other via a connecting mechanism having substantially the same structure.
【0018】上述の構成において、水中翼に図2の1点
鎖線で示すような変形が生じたとき、変形したときに生
じる水平面内での相対運動(a)はキー金物7と半円柱形
のスリーブ5,5との間の摺動で吸収される。また角度
変化(b)は円形の凹部6a内をスリーブ5,5がキー金物
7と一緒に回転することで、吸収される。In the above structure, when the hydrofoil is deformed as shown by the one-dot chain line in FIG. 2, the relative movement (a) in the horizontal plane caused by the deformation is the key metal 7 and the semi-cylindrical shape. It is absorbed by sliding between the sleeves 5 and 5. The angle change (b) is absorbed by the sleeves 5 and 5 rotating together with the key metal 7 in the circular recess 6a.
【0019】なお、図4に示した例では、スリーブ5に
固型潤滑材を埋め込んだ銅合金製のものを採用して上記
の摺動あるいは回転に対応しているが、図5に示した変
形例では、スリーブ5の内面および外面とこれら両面に
対接するキー金物7およびキー溝6の各面にそれぞれテ
フロン(商品名)ベースのライナー9を貼り付けて摺動
あるいは回転がスムーズに行なわれるようになってい
る。In the example shown in FIG. 4, a sleeve 5 made of a copper alloy in which a solid lubricant is embedded is used to cope with the above sliding or rotation. In a modification, a Teflon (trade name) base liner 9 is attached to each of the inner surface and the outer surface of the sleeve 5 and the surfaces of the key metal 7 and the key groove 6 that are in contact with the both surfaces, so that sliding or rotation can be performed smoothly. It is like this.
【0020】なお、テフロンベースのライナー9は対接
する一方の面だけに貼り付けてもよい。The Teflon-based liner 9 may be attached to only one of the opposing surfaces.
【0021】[0021]
【発明の効果】以上詳述したように、本発明の水中翼の
フラップ間連結機構によれば、次のような効果ないし利
点が得られる。 (1) フラップ間の相対運動が吸収可能となりキー金物の
疲労破断を防止できる。 (2) 摺動面積を大きく取れることから、面圧を小さくで
き摩耗量を小さくすることができる。As described in detail above, according to the inter-flap flap connecting mechanism of the hydrofoil of the present invention, the following effects and advantages are obtained. (1) The relative movement between the flaps can be absorbed, and the fatigue breakage of the key metal can be prevented. (2) Since the sliding area can be increased, the surface pressure can be reduced and the amount of wear can be reduced.
【図1】本発明の一実施例としての水中翼のフラップ間
連結機構をそなえた水中翼を示す斜視図。FIG. 1 is a perspective view showing a hydrofoil provided with an inter-flap coupling mechanism of a hydrofoil as an embodiment of the present invention.
【図2】同水中翼の正面図。FIG. 2 is a front view of the hydrofoil.
【図3】同連結機構を分解して示す斜視図。FIG. 3 is an exploded perspective view showing the connecting mechanism.
【図4】図1のA−A矢視断面図。FIG. 4 is a sectional view taken along the line AA of FIG.
【図5】同変形例を図4に対応して示す断面図。FIG. 5 is a cross-sectional view showing the modified example corresponding to FIG. 4.
【図6】従来の水中翼の平面図。FIG. 6 is a plan view of a conventional hydrofoil.
【図7】図6のB−B矢視断面図。7 is a cross-sectional view taken along the line BB of FIG.
【図8】図6のC−C矢視断面図。8 is a sectional view taken along the line CC of FIG.
1 水中翼本体 2,3,4 フラップ 5 半円柱形のスリーブ 6 キー溝 6a 円形の凹部 7 キー金物 1 Hydrofoil body 2,3,4 flaps 5 Semi-cylindrical sleeve 6 Key groove 6a Circular recess 7 Key hardware
Claims (1)
を上記水中翼本体に回動可能に取付けられた複数のフラ
ップと、隣接配設された上記フラップの間の連結機構と
をそなえ、同連結機構が、一方の上記フラップの端面に
突設された直方体形のキー金物と、他方の上記フラップ
の端面に形成されて上記キー金物を嵌挿可能なキー溝と
をそなえるとともに、一対の半円柱形のスリーブが上記
キー金物の上下両面にそれぞれ摺動可能に装着され、上
記キー溝に上記一対の半円柱形のスリーブを嵌挿可能な
円形の凹部が連設されていることを特徴とする、水中翼
のフラップ間連結機構。1. A hydrofoil comprising a hydrofoil body, a plurality of flaps whose base ends are rotatably attached to the hydrofoil body, and a coupling mechanism between adjacent flaps. , The connecting mechanism has a rectangular parallelepiped key metal piece projectingly provided on one end surface of the flap, and a key groove formed on the other end surface of the flap into which the key metal article can be inserted. The semi-cylindrical sleeves are slidably mounted on the upper and lower surfaces of the key hardware, and the key groove is provided with a series of circular recesses into which the pair of semi-cylindrical sleeves can be inserted. The feature is the connecting mechanism between the flaps of the hydrofoil.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3357870A JPH05178269A (en) | 1991-12-26 | 1991-12-26 | Inter-flap connecting mechanism for hydrofoil |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3357870A JPH05178269A (en) | 1991-12-26 | 1991-12-26 | Inter-flap connecting mechanism for hydrofoil |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH05178269A true JPH05178269A (en) | 1993-07-20 |
Family
ID=18456363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3357870A Withdrawn JPH05178269A (en) | 1991-12-26 | 1991-12-26 | Inter-flap connecting mechanism for hydrofoil |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH05178269A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110406654A (en) * | 2019-09-04 | 2019-11-05 | 西北工业大学 | A kind of insect-based flapping-wing system and hydrodynamic performance test method |
-
1991
- 1991-12-26 JP JP3357870A patent/JPH05178269A/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110406654A (en) * | 2019-09-04 | 2019-11-05 | 西北工业大学 | A kind of insect-based flapping-wing system and hydrodynamic performance test method |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A300 | Application deemed to be withdrawn because no request for examination was validly filed |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 19990311 |