JPH07260026A - Flow adjusting device - Google Patents

Flow adjusting device

Info

Publication number
JPH07260026A
JPH07260026A JP6075399A JP7539994A JPH07260026A JP H07260026 A JPH07260026 A JP H07260026A JP 6075399 A JP6075399 A JP 6075399A JP 7539994 A JP7539994 A JP 7539994A JP H07260026 A JPH07260026 A JP H07260026A
Authority
JP
Japan
Prior art keywords
flow rate
adjusting device
core member
line
pressure
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
JP6075399A
Other languages
Japanese (ja)
Inventor
Masakuni Kainuma
正邦 海沼
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.)
Fujikura Composites Inc
Original Assignee
Fujikura Rubber 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 Fujikura Rubber Ltd filed Critical Fujikura Rubber Ltd
Priority to JP6075399A priority Critical patent/JPH07260026A/en
Publication of JPH07260026A publication Critical patent/JPH07260026A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To obtain a flow adjusting device wherein pressure-flow rate curved line shows steep rising. CONSTITUTION:In a flow adjusting device composed of a core member 3 wherein a plurality of blade-like protrusions 31 are axially provided oh the outer periphery, elastic rings 2 arranged on the periphery of the core member 3, and a casing into which the core member 3 and the elastic rings 2 are fitted, and provided with an opening through which fluid is made pass in the axial direction of the core member 3, a ridge line L1 on the blade-like protrusion tip is forwardly inclined in the passing direction of the fluid in relation to the axial direction L2 by the specific angle THETA. The angle of the line of ridge on the blade protrusion tip is changed, thereby the specific flow rate can be made in the small pressure range, and the application for a flow adjusting device requiring steep rising is made possible. Moreover, the advantage wherein the flow adjusting device having the desired pressure-flow rate curved line can be easily manufactured is generated by measuring the relationship between the angle of the line of image and the rising of the flow rate.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の技術分野】本発明は流量調節装置、さらに詳細
には流体圧力の負荷に対し、所定の流量にすばやく応答
できる流量調整装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a flow rate control device, and more particularly to a flow rate control device capable of quickly responding to a predetermined flow rate in response to a fluid pressure load.

【0002】[0002]

【従来技術および問題点】流量調節装置は、図6に断面
図を示すように断面階段状で、上部開口11と下部開口
12を有するケーシング1内に、弾性リング2を配する
とともに、このケーシング1の前記下部開口12より芯
部材3を嵌め合わせた構造になっている(特公昭51−
23060号参照)。
2. Description of the Related Art As shown in the sectional view of FIG. 6, a flow rate adjusting device has a stepwise cross section, and an elastic ring 2 is arranged in a casing 1 having an upper opening 11 and a lower opening 12, and this casing is also used. 1 has a structure in which the core member 3 is fitted through the lower opening 12 (Japanese Examined Patent Publication No. 51-
23060).

【0003】前記芯部材3はその周方向に複数の羽状突
起31(図2、図3参照)を有しており、前記弾性リン
グ2がこの羽状突起31の外周を取り囲んだ構造になっ
ている。
The core member 3 has a plurality of wing-shaped projections 31 (see FIGS. 2 and 3) in the circumferential direction, and the elastic ring 2 surrounds the wing-shaped projections 31. ing.

【0004】このような流量調整装置に下部開口12方
向より所定の流体圧力がかかると、前記弾性リング2と
羽状突起31間および弾性リング2と羽状突起31が形
成する凹部33の間より流体が流れ、ほぼ流体圧力に比
例して流量が大きくなってくる(図4の実線および破線
の流量−圧力曲線で矢印で示した範囲)。
When a predetermined fluid pressure is applied to the flow rate adjusting device from the direction of the lower opening 12, the elastic ring 2 and the wing-shaped projection 31 and the recess 33 formed by the elastic ring 2 and the wing-shaped projection 31 are pressed. The fluid flows, and the flow rate increases substantially in proportion to the fluid pressure (the range indicated by the arrows in the flow rate-pressure curves of the solid line and the broken line in FIG. 4).

【0005】さらに流体圧力が上昇すると弾性リング2
は芯部材3方向に変形する。このとき芯部材3の外周に
は羽状突起31が設けられているため、前記弾性リング
2はこの羽状突起31の外形に沿って変形し、弾性リン
グ2と凹部33と羽状突起31の間隙34に流体流路を
形成することになり、所定の流量に到達した後は、弾性
リングは水圧変動と流体の芯部材方向への流体力学的な
力との合力を受けて間隙34を増減し結果的に一定の調
節幅で流量を安定化させることができる。
When the fluid pressure further increases, the elastic ring 2
Deforms in the direction of the core member 3. At this time, since the wing-shaped projections 31 are provided on the outer periphery of the core member 3, the elastic ring 2 is deformed along the outer shape of the wing-shaped projections 31, and the elastic ring 2, the recess 33 and the wing-shaped projections 31 are separated. After the fluid flow path is formed in the gap 34, and after reaching the predetermined flow rate, the elastic ring is increased or decreased in the gap 34 in response to the resultant force of the hydraulic pressure fluctuation and the hydrodynamic force of the fluid toward the core member. As a result, the flow rate can be stabilized with a constant adjustment width.

【0006】一方、流体圧力が小さくなると、弾性リン
グ2の復元力によって間隙34の断面積が増加し、流体
流路が広がることによって一定流量を確保できる。
On the other hand, when the fluid pressure decreases, the cross-sectional area of the gap 34 increases due to the restoring force of the elastic ring 2 and the fluid flow path widens, so that a constant flow rate can be secured.

【0007】上述のような流量調整装置においては、従
来においては流体圧力−流量の関係は図4の破線に示す
ように、なだらかな曲線を描くことが知られている。す
なわち、所定の流量に到達するまでは、流体圧力の増加
にともない、比例的とまではいえないまでも徐々に流量
が大きくなり、相当圧力が高まってから所定の流量に達
した後圧力変動に対しても流量がほぼ安定化するように
なっている。
In the flow rate adjusting device as described above, it has been conventionally known that the fluid pressure-flow rate relationship draws a gentle curve as shown by the broken line in FIG. That is, until reaching the predetermined flow rate, the flow rate gradually increases, if not proportionally, with the increase of the fluid pressure, and after the equivalent pressure increases, it reaches the predetermined flow rate, and then there is a pressure fluctuation. On the contrary, the flow rate is almost stabilized.

【0008】上述のような、なだらかな立ち上がり部分
を有する流量調整装置では所定の流量を得るために相当
圧力を高くする必要があった。産業用または家庭用とし
て要求される用途に応じて、例えば図4の実線に示すよ
うな急峻な立ち上がりの(流量−圧力の比例部分が狭
い)、すなわち小さな圧力範囲内で所定の流量になるよ
うな流量調整装置が求められてきた。
In the flow rate adjusting device having the smooth rising portion as described above, it is necessary to raise the corresponding pressure to obtain a predetermined flow rate. Depending on the application required for industrial or household use, for example, a sharp rise as shown by the solid line in FIG. 4 (the proportional portion of the flow rate-pressure is narrow), that is, a predetermined flow rate is achieved within a small pressure range. There has been a demand for a new flow control device.

【0009】本発明は上述の問題点に鑑みなされたもの
であり、圧力−流量曲線が急峻な立ち上がりを示す流量
調整装置を提供することを目的とする。
The present invention has been made in view of the above problems, and an object of the present invention is to provide a flow rate adjusting device in which a pressure-flow rate curve shows a steep rise.

【0010】[0010]

【問題点を解決するための手段】上述の目的を達成する
ため、本発明による流量調整装置は、外周に複数の羽状
突起を軸方向に有する芯部材とこの芯部材の周囲に配さ
れる弾性リングと、このような芯部材および弾性リング
が嵌め込まれ、前記芯部材の前記軸方向に流体を通過さ
せるための開口を有するケーシングとからなる流量調整
装置において、前記羽状突起先端部の稜線は前記軸方向
に対し、流体の通過方向に所定角度Θ前傾していること
を特徴とする。
In order to achieve the above-mentioned object, a flow rate adjusting device according to the present invention is arranged around a core member having a plurality of wing-shaped projections on its outer periphery in the axial direction and around this core member. In a flow rate adjusting device comprising an elastic ring and a casing having such a core member and the elastic ring fitted therein, and having an opening for allowing passage of a fluid in the axial direction of the core member, a ridgeline of the tip end portion of the wing-shaped projection. Is inclined forward by a predetermined angle Θ in the fluid passage direction with respect to the axial direction.

【0011】本発明者によれば、羽状突起先端部の稜線
の角度を変化せしめることにより、流体の圧力に対する
流量の立ち上がりを急激にすることが可能になることを
見いだしなされたものであり、上述のような急峻な立ち
上がりを要求される流量調節装置に適用することが可能
になる。さらに、前記稜線の角度と流量の立ち上がりの
関係を測定することによって、所望の圧力−流量曲線の
流量調整装置を簡単に製造可能になるという利点も生じ
る。
The present inventor has found that the rise of the flow rate with respect to the fluid pressure can be made rapid by changing the angle of the ridgeline at the tip of the wing-shaped projection. The present invention can be applied to a flow rate control device that requires a sharp rise as described above. Further, by measuring the relationship between the angle of the ridge and the rise of the flow rate, there is an advantage that a flow rate adjusting device having a desired pressure-flow rate curve can be easily manufactured.

【0012】[0012]

【実施例】図1は本発明の流量調整装置の断面図、図2
は平面図、図3は底面図を示すものであるが、この実施
例より明らかなように、流量調整装置は上部開口11と
下部開口12を有するケーシング1内に、弾性リング2
を配するとともに、このケーシング1の前記下部開口1
2より芯部材3を嵌め合わせた構造になっている。
DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a sectional view of a flow rate adjusting device of the present invention, and FIG.
FIG. 3 is a plan view and FIG. 3 is a bottom view. As is apparent from this embodiment, the flow rate adjusting device includes a casing 1 having an upper opening 11 and a lower opening 12, and an elastic ring 2
And the lower opening 1 of this casing 1
The core member 3 has a structure in which the core member 3 is fitted together.

【0013】前記芯部材3はその周方向に複数の羽状突
起31(図1、図2、図3参照)を有しており、前記弾
性リング2がこの羽状突起31の外周を取り囲んだ構造
になっている。
The core member 3 has a plurality of wing-shaped projections 31 (see FIGS. 1, 2 and 3) in the circumferential direction thereof, and the elastic ring 2 surrounds the outer circumference of the wing-shaped projections 31. It is structured.

【0014】このような流量調整装置に下部開口12方
向より所定の流体圧力がかかると、図2のA−A断面図
である図1より明らかなように、前記弾性リング2と羽
状突起31間および弾性リング2と羽状突起31が形成
する凹部33の間より流体が流れ、ほぼ流体圧力に比例
して流量が大きくなってくる(図4の実線の流量−圧力
曲線で矢印で示した範囲)。
When a predetermined fluid pressure is applied to such a flow rate adjusting device from the direction of the lower opening 12, as is apparent from FIG. 1 which is a sectional view taken along the line AA of FIG. Fluid flows between the elastic ring 2 and the recess 33 formed by the wing-shaped projections 31, and the flow rate increases in proportion to the fluid pressure (indicated by the arrow in the solid-line flow rate-pressure curve in FIG. 4). range).

【0015】さらに流体圧力が上昇すると弾性リング2
は芯部材3方向に変形する。このとき芯部材3の外周に
は羽状突起31が設けられているため、前記弾性リング
2はこの羽状突起31の外形に沿って弾性リング2は徐
々にではあるが変形をしはじめる。さらに、圧力が高ま
ると、弾性リングの内側に形成されている間隙34の流
体流路は徐々に狭くなり、流量が所定の値以上に達した
時点で水圧変動に対して調節機能を発揮し、流量は所定
の値近くでほぼ一定となる(図4において、実線矢印以
外の範囲)。
When the fluid pressure further increases, the elastic ring 2
Deforms in the direction of the core member 3. At this time, since the wing-shaped projections 31 are provided on the outer periphery of the core member 3, the elastic ring 2 starts to deform gradually along the outer shape of the wing-shaped projections 31. Further, when the pressure is increased, the fluid passage of the gap 34 formed inside the elastic ring is gradually narrowed, and when the flow rate reaches a predetermined value or more, it exerts an adjusting function for water pressure fluctuation, The flow rate becomes almost constant near a predetermined value (in FIG. 4, a range other than the solid arrow).

【0016】本発明において、前記羽状突起31先端部
の稜線32(ラインL1に相当する)を前記軸L2(ラ
インL2の角度=ラインL3の角度)方向に対し、流体
の通過方向に所定角度Θ前傾せしめている。すなわち、
ラインL1とラインL3との角度ΘはラインL1が軸L
2方向に傾斜することにより形成されている。この範囲
は、流量制御装置の寸法、形などに依存するが、2〜3
0°内に最適角度Θが存在することが判明した。Θが2
°より小さいと、立ち上がりにおける流体圧力−流量曲
線に顕著な変化が見られず、一方、Θが30°を越える
と図5のD(波線にて表示)のように流量が一定値に達
せず使用に供することができない。
In the present invention, the ridgeline 32 (corresponding to the line L1) at the tip of the wing-shaped projection 31 is set at a predetermined angle in the fluid passage direction with respect to the axis L2 (angle of the line L2 = angle of the line L3) direction. Θ It is leaning forward. That is,
As for the angle Θ between the line L1 and the line L3, the line L1 is the axis L.
It is formed by inclining in two directions. This range depends on the size, shape, etc. of the flow control device, but is 2-3
It was found that there is an optimum angle Θ within 0 °. Θ is 2
If it is less than °, no remarkable change is observed in the fluid pressure-flow rate curve at the rising, while if Θ exceeds 30 °, the flow rate does not reach a constant value as shown by D (shown by the wavy line) in Fig. 5. Cannot be used.

【0017】このように羽状突起31の先端部稜線32
を傾斜せしめることによって、当初の圧力に対し流量が
急激に増加する形状(急峻な立ち上がり)を有する流体
圧力−流量曲線を実現することが可能になる(図4の実
線の流体圧力−流量曲線)。
As described above, the ridgeline 32 at the tip of the wing-shaped projection 31 is formed.
It is possible to realize a fluid pressure-flow rate curve having a shape (a steep rise) in which the flow rate sharply increases with respect to the initial pressure by inclining (the fluid pressure-flow rate curve of the solid line in FIG. 4). .

【0018】具体例として、d1=10.5mm、Θ=
8°の芯部材を使用し、流体圧力−流量曲線を測定した
結果、図5に示す結果を得た。実線Cは本発明の圧力調
整装置の流体圧力−流量曲線、破線Aは従来の圧力調整
装置(Θ=1.5°)の流体圧力−流量曲線である。こ
の図から明らかなように、本発明による圧力調整装置に
おいては、流体圧力−流量曲線の立ち上がりが急峻で、
より小さな圧力で所定の流量に達することが可能にな
る。
As a concrete example, d1 = 10.5 mm, Θ =
As a result of measuring a fluid pressure-flow rate curve using an 8 ° core member, the results shown in FIG. 5 were obtained. A solid line C is a fluid pressure-flow rate curve of the pressure adjusting device of the present invention, and a broken line A is a fluid pressure-flow rate curve of a conventional pressure adjusting device (Θ = 1.5 °). As is clear from this figure, in the pressure regulator according to the present invention, the rise of the fluid pressure-flow rate curve is steep,
It is possible to reach a given flow rate with less pressure.

【0019】本発明によれば、羽状突起の形状および稜
線の角度の流体圧力−流量曲線を種々測定しておけば、
前述のような流量調整装置を設計するに当たり、また所
望の立ち上がり曲線を提供するに当たり、極めて簡便に
実行可能になるという利点がある。
According to the present invention, various fluid pressure-flow rate curves of the shape of the wing and the angle of the ridge are measured,
In designing the flow rate adjusting device as described above and providing a desired rising curve, there is an advantage that it can be executed very easily.

【0020】[0020]

【発明の効果】以上説明したように、本発明による流量
調整装置は羽状突起先端部の稜線の角度を変化せしめる
ことにより、小さな圧力範囲で所定の流量にすることが
可能であり、上述のような急峻な立ち上がりを要求され
る流量調節装置に適用することが可能になる。さらに、
本発明によれば、前記稜線の角度と流量の立ち上がりの
関係を測定することによって、所望の圧力−流量曲線の
流量調整装置を簡単に製造可能になるという利点も生じ
る。
As described above, the flow rate adjusting device according to the present invention can achieve a predetermined flow rate in a small pressure range by changing the angle of the ridgeline at the tip of the wing-shaped projection. The present invention can be applied to a flow rate control device that requires such a sharp rise. further,
According to the present invention, by measuring the relationship between the angle of the ridge and the rise of the flow rate, there is an advantage that a flow rate adjusting device having a desired pressure-flow rate curve can be easily manufactured.

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

【図1】本発明による流量調整装置の一実施例の図2に
おけるA−A断面図。
FIG. 1 is a sectional view taken along the line AA in FIG. 2 showing an embodiment of a flow rate adjusting device according to the present invention.

【図2】前記実施例の平面図。FIG. 2 is a plan view of the embodiment.

【図3】前記実施例の底面図。FIG. 3 is a bottom view of the embodiment.

【図4】流体圧力−流量の関係を模式的に示す図。FIG. 4 is a diagram schematically showing the relationship between fluid pressure and flow rate.

【図5】流体圧力−流量の関係の測定図。FIG. 5 is a measurement diagram of a relationship between fluid pressure and flow rate.

【図6】従来の圧力調整装置の断面図。FIG. 6 is a sectional view of a conventional pressure adjusting device.

【符号の説明】[Explanation of symbols]

1 ケーシング 11 上部開口 12 下部開口 2 弾性リング 3 芯部材 31 羽状突起 32 稜線 DESCRIPTION OF SYMBOLS 1 Casing 11 Upper opening 12 Lower opening 2 Elastic ring 3 Core member 31 Feather-shaped projection 32 Ridge line

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】外周に複数の羽状突起を軸方向に有する芯
部材とこの芯部材の周囲に配される弾性リングと、この
ような芯部材および弾性リングが嵌め込まれ、前記芯部
材の前記軸方向に流体を通過させるための開口を有する
ケーシングとからなる流量調整装置において、前記羽状
突起先端部の稜線は前記軸方向に対し、流体の通過方向
に所定角度Θ前傾していることを特徴とする流量調整装
置。
1. A core member having a plurality of wing-shaped projections on its outer circumference in the axial direction, an elastic ring arranged around the core member, and such a core member and an elastic ring are fitted into the core member, In a flow rate adjusting device including a casing having an opening for passing a fluid in an axial direction, a ridgeline of the tip end portion of the wing-shaped projection is inclined forward by a predetermined angle Θ in the passage direction of the fluid with respect to the axial direction. Flow rate adjusting device characterized by.
JP6075399A 1994-03-22 1994-03-22 Flow adjusting device Pending JPH07260026A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6075399A JPH07260026A (en) 1994-03-22 1994-03-22 Flow adjusting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6075399A JPH07260026A (en) 1994-03-22 1994-03-22 Flow adjusting device

Publications (1)

Publication Number Publication Date
JPH07260026A true JPH07260026A (en) 1995-10-13

Family

ID=13575069

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6075399A Pending JPH07260026A (en) 1994-03-22 1994-03-22 Flow adjusting device

Country Status (1)

Country Link
JP (1) JPH07260026A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998021419A1 (en) * 1996-11-12 1998-05-22 Star Bright Pty. Limited Flow regulator
JP2009530548A (en) * 2006-03-13 2009-08-27 ヨセフ ベレツナイ Control valve with molded packing element

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998021419A1 (en) * 1996-11-12 1998-05-22 Star Bright Pty. Limited Flow regulator
JP2009530548A (en) * 2006-03-13 2009-08-27 ヨセフ ベレツナイ Control valve with molded packing element

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