JPH049611Y2 - - Google Patents
Info
- Publication number
- JPH049611Y2 JPH049611Y2 JP10492084U JP10492084U JPH049611Y2 JP H049611 Y2 JPH049611 Y2 JP H049611Y2 JP 10492084 U JP10492084 U JP 10492084U JP 10492084 U JP10492084 U JP 10492084U JP H049611 Y2 JPH049611 Y2 JP H049611Y2
- Authority
- JP
- Japan
- Prior art keywords
- bellows
- pilot
- pressure
- valve
- spring
- 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
Links
- 238000006073 displacement reaction Methods 0.000 claims description 5
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 2
- 244000208734 Pisonia aculeata Species 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
Landscapes
- Control Of Fluid Pressure (AREA)
Description
【考案の詳細な説明】
〈関係技術分野〉
減圧弁の作動部分のうち、とくに頻繁動作が強
いられて破損又は故障を生じ易いパイロツトの改
良に関連している。[Detailed description of the invention] <Related technical field> Among the operating parts of a pressure reducing valve, this invention relates to the improvement of the pilot, which is particularly prone to breakage or malfunction due to frequent operation.
〈従来技術とその問題点〉
減圧弁の主弁作動は、通常ダイヤフラムまたと
きにベローズの2次圧応動変位をパイロツト弁の
動作に導いて1次圧を主弁の操作ピストンに作用
させる自力制御とされるが、ダイヤフラムはその
弾性限度内における変位をあまり長くとることが
できないことから、パイロツト弁の操作機構(以
下単にパイロツトと呼ぶ)が大型になり、これに
反してベローズははるかに小径になし得るとはい
え、過大な圧縮の下ではやはり永久変形を生じる
うれいなしとしない。ここに過大な圧縮は、主弁
の弁座洩れによるような、2次圧の過上昇によつ
てその2次圧がパイロツトの受圧面としてのベロ
ーズに作用することに由来する。<Prior art and its problems> The main valve operation of a pressure reducing valve is usually self-controlled by guiding the secondary pressure response displacement of the diaphragm or sometimes the bellows to the operation of the pilot valve, and applying the primary pressure to the operating piston of the main valve. However, since the diaphragm cannot be displaced for a very long time within its elastic limit, the pilot valve operating mechanism (hereinafter simply referred to as the pilot) has to be large, and the bellows, on the other hand, has a much smaller diameter. Although this is possible, permanent deformation may occur under excessive compression. The excessive compression is caused by an excessive rise in secondary pressure, such as due to leakage from the valve seat of the main valve, which acts on the bellows, which serves as a pressure receiving surface of the pilot.
〈目的〉
ベローズの上記過大な圧縮による破損を防止す
ることを目指した開発成果を提案するところにあ
る。<Purpose> The purpose is to propose a development result aimed at preventing damage to bellows caused by excessive compression.
〈構成〉
上記目的は、2次圧に応動する伸縮可動端にて
パイロツト弁のステムを向かい合うベローズと、
該2次圧と対抗する向きの偏倚力をスプリングス
テーを介し該伸縮可動端に作用させるコイルスプ
リングそして該スプリングの偏倚力を調整可能に
設定するねじばめスリーブおよびスピンドル結合
とから成る減圧弁のパイロツトにおいて、該スピ
ンドルの先端と、スプリングステーとに、それら
の間でベローズ可動端の最大許容変位を制限す
る、突き合わせ面をそなえることによつて、全部
に成就される。<Configuration> The above purpose is to provide a bellows that faces the stem of the pilot valve at its telescopic movable end that responds to secondary pressure;
A pressure reducing valve comprising a coil spring that applies a biasing force in a direction opposed to the secondary pressure to the telescopic movable end via a spring stay, and a screw-fit sleeve and spindle coupling that adjustably set the biasing force of the spring. This is accomplished entirely in the pilot by providing the spindle tip and the spring stay with abutment surfaces which limit the maximum permissible displacement of the bellows movable end therebetween.
この構成については、パイロツト弁、ベロー
ズ、コイルスプリング、そしてスリーブおよびス
ピンドル結合を含む軸心の向きを、減圧弁本体の
ボンネツト取付け面と平行に配列することが実施
上とくに好ましく、ダイヤフラムのベローズによ
る代替と相まつて減圧弁全体の著しい小型化に役
立つ。 Regarding this configuration, it is particularly preferable in practice to align the axis including the pilot valve, bellows, coil spring, and sleeve and spindle coupling parallel to the bonnet mounting surface of the pressure reducing valve body. Together with this, it helps to significantly reduce the size of the entire pressure reducing valve.
〈図示に従う具体例〉
第1図に減圧弁の全体を断面で示し第2図には
要部詳細を示した。<Specific example according to the illustrations> FIG. 1 shows the entire pressure reducing valve in cross section, and FIG. 2 shows details of the main parts.
図中1は減圧弁本体、2はボンネツト、また3
はボトムフランジ、そして4は主弁、5は主弁
座、6はリターンスプリング、また7は主弁4の
操作ピストン、8はシリンダライナである。 In the figure, 1 is the pressure reducing valve body, 2 is the bonnet, and 3
is a bottom flange, 4 is a main valve, 5 is a main valve seat, 6 is a return spring, 7 is an operating piston of the main valve 4, and 8 is a cylinder liner.
ボンネツト2はシリンダライナ8の開口を覆う
シリンダヘツドを兼ねて弁本体1に対し気密に取
付け、その取付け面と平行な軸心上にアジヤスト
カバー9と、ねじプラグ10とを気密に取付け
て、その内部に以下のパイロツト機構を組み込
む。 The bonnet 2 also serves as a cylinder head that covers the opening of the cylinder liner 8 and is airtightly attached to the valve body 1, and the adjuster cover 9 and the threaded plug 10 are airtightly attached on the axis parallel to the mounting surface. The following pilot mechanism is incorporated inside it.
すなわち11はパイロツト弁、12はパイロツ
ト弁座、13はパイロツトスプリング、そして1
4はベローズ、15はコイルスプリング、16は
スプリングステー、17はねじスリーブ、18は
スピンドル、19はロツクナツト、20はストレ
ーナ、21はキヤツプである。 That is, 11 is a pilot valve, 12 is a pilot valve seat, 13 is a pilot spring, and 1 is a pilot valve.
4 is a bellows, 15 is a coil spring, 16 is a spring stay, 17 is a threaded sleeve, 18 is a spindle, 19 is a lock nut, 20 is a strainer, and 21 is a cap.
ベローズ14はその開放端をガスケツトで挟ん
でアジヤストカバー9によりボンネツト2に固定
するがその内部にスプリングステー16と、これ
を介してベローズ14の他端つまり伸縮可動端に
ばね偏倚力を作用させるコイルスプリング15、
このばね偏倚力を調整可能に設定するねじスリー
ブ17およびスピンドル18を内蔵させ、ねじス
リーブ17の左向き推進にてコイルスプリング1
5のスプリングステー16を介した伸縮可動端に
対する偏倚力を増強し、逆の右向き引き戻しによ
る偏倚力の減少の調整をスピンドル18の回転に
よつて行い、設定位置をロツクナツト19により
固定する。 The bellows 14 is fixed to the bonnet 2 by an adjuster cover 9 with its open end sandwiched between gaskets, but there is a spring stay 16 inside, and a spring biasing force is applied to the other end of the bellows 14, that is, the movable end of the bellows 14 through this. coil spring 15,
A screw sleeve 17 and a spindle 18 are built in to adjust this spring biasing force, and when the screw sleeve 17 is pushed leftward, the coil spring 1 is
The biasing force against the telescopic movable end via the spring stay 16 of No. 5 is increased, and the reduction of the biasing force due to reverse rightward pullback is adjusted by rotating the spindle 18, and the set position is fixed by the lock nut 19.
ベローズ14の伸縮可動端の外面には減圧弁本
体1の2次側圧力をボンネツト2に開穿した通路
孔Aを通して導くことにより、操業上必要とされ
る任意の2次圧がベローズ14の有効受圧面に働
き、これに対して上記偏倚力がつり合うべき設定
圧力の調節を行うことにより、設定圧力以上の2
次圧力はコイルスプリング15による偏倚力を圧
倒してベローズ14の圧縮を生じる。 By guiding the secondary side pressure of the pressure reducing valve main body 1 through the passage hole A opened in the bonnet 2 to the outer surface of the telescopic movable end of the bellows 14, any secondary pressure required for operation can be applied to the effective pressure of the bellows 14. By adjusting the set pressure that acts on the pressure-receiving surface and against which the above-mentioned biasing force should be balanced, it is possible to
The next pressure overwhelms the biasing force due to coil spring 15 and causes compression of bellows 14.
これに反して2次圧が設定値よりも低くなると
偏倚力がベローズ14に働く推力に打ち勝つて伸
長し、その伸縮可動端と向かい合うパイロツト弁
11のステムと付き合わさつてパイロツトスプリ
ング13に抗しパイロツト弁11を押し開く。 On the other hand, when the secondary pressure becomes lower than the set value, the biasing force overcomes the thrust force acting on the bellows 14 and expands, and the telescopic movable end engages with the stem of the pilot valve 11 opposite, resisting the pilot spring 13 and causing the pilot to close. Push valve 11 open.
ここにボンネツト2に開穿した、通路孔Bおよ
びCを通して減圧弁本体1の1次側圧力をシリン
ダライナ8の内部に導入し、主弁4に対してはる
かに受圧面積の大きい操作ピストン7により主弁
4に働く1次側圧力を圧倒してその弁座5に対す
る離座開弁を生じさせる。 The primary side pressure of the pressure reducing valve body 1 is introduced into the cylinder liner 8 through the passage holes B and C opened in the bonnet 2, and the pressure is introduced into the cylinder liner 8 by the operating piston 7, which has a much larger pressure receiving area than the main valve 4. The primary side pressure acting on the main valve 4 is overwhelmed to cause the valve seat 5 to be unseated and opened.
その結果2次側圧力が上昇するとそれに応じて
ベローズ14が圧縮変位してパイロツト弁11が
復元着座することとなり、操作ピストン7に対す
る1次側圧力の適用がやむので、主弁4の再着座
閉弁がもたらされる。 As a result, when the secondary side pressure rises, the bellows 14 is compressed and displaced accordingly, and the pilot valve 11 is restored to its seat, and the application of the primary side pressure to the operating piston 7 is stopped, so that the main valve 4 is reseated and closed. A valve is provided.
以上の作動は、2次側圧力の変動に応じそれを
打ち消すような主弁4の動作が繰り返され、2次
側圧力を設定値に保持する自力的制御が続行され
るのはいうまでもない。 Needless to say, in the above operation, the operation of the main valve 4 is repeated to cancel out fluctuations in the secondary side pressure, and self-controlled control to maintain the secondary side pressure at the set value continues. .
ここに2次圧の異常な上昇がたとえば操業中止
の際に主弁4の主弁漏れのごときによつて生じる
機会なしとしないが、このときベローズ14が過
圧縮により永久変形を来して、パイロツトの調整
機能が失調する原因となる。 There is a chance that an abnormal increase in the secondary pressure may occur, for example, due to leakage of the main valve 4 when the operation is stopped, but in this case, the bellows 14 is permanently deformed due to overcompression. This may cause the pilot's adjustment function to deteriorate.
これに対処するためスピンドル18の先端とス
プリングステー16とに、それらの間でベローズ
14の可動端にその弾性限界から許される最大変
位を制限する突き合わせ面18aと16aとを設
ける。 To cope with this, abutting surfaces 18a and 16a are provided at the tip of the spindle 18 and the spring stay 16, which limit the maximum displacement allowed by the elastic limit of the movable end of the bellows 14 between them.
なお図中18b,16bは、スピンドル18の
先端突起とスプリングステー16に穿つた受け孔
であつてセンタリングに役立つ。 In the figure, 18b and 16b are receiving holes bored in the tip projection of the spindle 18 and the spring stay 16, which are useful for centering.
〈効果〉
ベローズの伸縮変位にて2次圧に応動する減圧
弁のパイロツト作動を導く際、不時に生起する2
次圧の過大上昇によるベローズの過圧縮に由来す
るベローズの破損を有利に回避して、適切な減圧
弁の作動を長期にわたる耐久性の下に確保するこ
とができる。<Effect> When guiding the pilot operation of the pressure reducing valve that responds to the secondary pressure by the expansion and contraction displacement of the bellows, 2.
Breakage of the bellows due to overcompression of the bellows due to an excessive increase in the next pressure can be advantageously avoided, thereby ensuring proper operation of the pressure reducing valve with long-term durability.
第1図は断面図、第2図は要部の詳細図であ
る。
11……パイロツト弁、14……ベローズ、1
5……コイルスプリング、16……スプリングス
テー、17……ねじスリーブ、18……スピンド
ル、16a,18a……突き合わせ面。
FIG. 1 is a sectional view, and FIG. 2 is a detailed view of the main parts. 11... Pilot valve, 14... Bellows, 1
5... Coil spring, 16... Spring stay, 17... Threaded sleeve, 18... Spindle, 16a, 18a... Butt surface.
Claims (1)
弁のステムと向かい合うベローズと、該2次圧
と対抗する向きの偏倚力をスプリングステーを
介し該伸縮可動端に作用させるコイルスプリン
グ、そして該スプリングの偏倚力を調整可能に
設定するねじばめスリーブおよびスピンドル結
合とから成る減圧弁のパイロツトにおいて、 該スピンドルの先端とスプリングステーと
に、それらの間でベローズ可動端の最大許容変
位を制限する突き合わせ面をそなえる ことを特徴とする、減圧弁のパイロツト用ベロ
ーズ保護装置。 (2) パイロツト弁、ベローズ、コイルスプリング
そしてスリーブおよびスピンドル結合を含む軸
心の向きが、減圧弁本体のボンネツト取付け面
と平行な配列である、(1)に記載した減圧弁のパ
イロツト。[Claims for Utility Model Registration] (1) A bellows that faces the stem of the pilot valve at its telescopically movable end that responds to secondary pressure, and a biasing force that opposes the secondary pressure to the telescopically movable body through a spring stay. In the pilot of a pressure reducing valve consisting of a coil spring acting on the end, and a threaded sleeve and spindle connection for adjustable setting of the biasing force of the spring, the end of the spindle and the spring stay have a bellows between them. A bellows protection device for a pilot of a pressure reducing valve, characterized by having an abutment surface that limits the maximum permissible displacement of the movable end. (2) The pilot of the pressure reducing valve described in (1), wherein the axis including the pilot valve, bellows, coil spring, sleeve and spindle coupling is aligned parallel to the bonnet mounting surface of the pressure reducing valve body.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10492084U JPS6119809U (en) | 1984-07-10 | 1984-07-10 | Bellows protection device for pilot of pressure reducing valve |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10492084U JPS6119809U (en) | 1984-07-10 | 1984-07-10 | Bellows protection device for pilot of pressure reducing valve |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6119809U JPS6119809U (en) | 1986-02-05 |
JPH049611Y2 true JPH049611Y2 (en) | 1992-03-10 |
Family
ID=30664259
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10492084U Granted JPS6119809U (en) | 1984-07-10 | 1984-07-10 | Bellows protection device for pilot of pressure reducing valve |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6119809U (en) |
-
1984
- 1984-07-10 JP JP10492084U patent/JPS6119809U/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS6119809U (en) | 1986-02-05 |
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