JP7300918B2 - Pilot governor and reverse-acting pressure regulator equipped with it - Google Patents

Pilot governor and reverse-acting pressure regulator equipped with it Download PDF

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JP7300918B2
JP7300918B2 JP2019135656A JP2019135656A JP7300918B2 JP 7300918 B2 JP7300918 B2 JP 7300918B2 JP 2019135656 A JP2019135656 A JP 2019135656A JP 2019135656 A JP2019135656 A JP 2019135656A JP 7300918 B2 JP7300918 B2 JP 7300918B2
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雅之 高野
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Osaka Gas Co Ltd
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Description

本発明は、逆作動型整圧装置として用いるパイロットガバナ、及びそれを備えた逆作動型整圧装置に関する。 The present invention relates to a pilot governor used as a reverse-acting pressure regulating device and a reverse-acting pressure regulating device having the pilot governor.

従来、二次圧が設定圧力よりも上昇・降下した場合に、メインガバナの主弁体の変位を制御できる整圧装置として、逆作動型整圧装置と、それに用いられるパイロットガバナが知られている(特許文献1を参照)。
一方で、制御システムを解析する一つの手法として、正弦波等の入力に対する応答から制御特性を調べる周波数応答解析が知られている。当該周波数応答解析は、電気系・メカトロ系システムで使用される場合が多いが、電気を必要としないフィードバック制御装置であるパイロットガバナ等の整圧器にも当然のことながら適用可能である。例えば、パイロット式ガバナにおいては、入力信号をパイロットに入力する二次圧、出力信号を本体弁下流側配管の二次圧として、パイロットガバナ単体においては、入力信号を二次圧、出力信号を駆動圧として、種々の周波数での入力に対する周波数応答解析を行うことにより、系の安定性を判定できる。
Conventionally, a reverse acting pressure regulator and a pilot governor used therein are known as pressure regulators capable of controlling the displacement of the main valve body of the main governor when the secondary pressure rises or falls below the set pressure. (See Patent Document 1).
On the other hand, as one method of analyzing control systems, frequency response analysis is known, which examines control characteristics from responses to inputs such as sine waves. The frequency response analysis is often used in electrical and mechatronic systems, but it can of course also be applied to pressure regulators such as pilot governors, which are feedback control devices that do not require electricity. For example, in a pilot type governor, the input signal is the secondary pressure that is input to the pilot, and the output signal is the secondary pressure in the main valve downstream piping. As pressure, the stability of the system can be determined by performing a frequency response analysis for inputs at various frequencies.

特開2017-182718号公報JP 2017-182718 A

さて、上述の如く、パイロット式ガバナもしくはパイロットガバナの周波数応答解析を行う場合、周期振動である正弦波等を入力信号として二次圧検知室へ付与する必要がある。しかしながら、特許文献1に示されるような一般に知られる逆作動型整圧装置に用いられるパイロット式ガバナもしくはパイロットガバナは、二次圧検知室に対して駆動圧室から排出された駆動圧が流入してくるため、正確な正弦波を入力信号として付与することができない。例えば、二次圧検知室に連通接続される二次側圧力導入路の管路抵抗を減らすことにより、当該二次側圧力導入路からの駆動圧排出抵抗を小さくできる。しかしながら、当該方法では、二次圧検知室を気密に構成し、その体積を強制的に変化させて圧力として正弦波を与えるような方法は適用できなくなる。 As described above, when conducting frequency response analysis of a pilot type governor or a pilot governor, it is necessary to apply a sine wave or the like, which is periodic vibration, to the secondary pressure detection chamber as an input signal. However, in a pilot type governor or a pilot governor used in a generally known reverse acting pressure regulating device as disclosed in Patent Document 1, the driving pressure discharged from the driving pressure chamber flows into the secondary pressure detection chamber. Therefore, an accurate sine wave cannot be given as an input signal. For example, by reducing the pipeline resistance of the secondary side pressure introducing path that is connected to the secondary pressure detection chamber, the driving pressure discharge resistance from the secondary side pressure introducing path can be reduced. However, in this method, it is not possible to apply a method of airtightly configuring the secondary pressure detection chamber and forcibly changing its volume to give a sine wave as pressure.

本発明は、上述の課題に鑑みてなされたものであり、その目的は、入力として実際の圧力正弦波等を適切に投入できると共にその出力応答としての駆動圧を計測でき、それらの値から制御特性を解析する周波数応答解析を実行可能な逆作動型整圧装置のパイロットガバナ、及びそれを備えた逆作動型整圧装置を提供することにある。 The present invention has been made in view of the above-mentioned problems, and its object is to be able to appropriately apply an actual pressure sine wave or the like as an input, to be able to measure the driving pressure as its output response, and to be able to control from these values. It is an object of the present invention to provide a pilot governor of a reverse-acting pressure regulating device capable of executing frequency response analysis for analyzing characteristics, and a reverse-acting pressure regulating device having the pilot governor.

上記目的を達成するためのパイロットガバナは、
逆作動型整圧装置として用いるパイロットガバナであって、その特徴構成は、
筐体と第1ダイヤフラムとにより区画され二次側圧力導入路が連通接続される第1室と、前記筐体と前記第1ダイヤフラムと第2ダイヤフラムとにより区画され外部へ開放される開放孔が前記筐体に形成される第2室と、前記筐体と前記第2ダイヤフラムと第3ダイヤフラムとにより区画され一次側圧力導入路が連通接続されると共にメインガバナの駆動圧室に駆動圧を導入する駆動圧導入路が連通接続される第3室と、前記第3ダイヤフラムを前記第3室の側へ付勢する第1付勢部材とを備え、
前記第1ダイヤフラムと前記第2ダイヤフラムと前記第3ダイヤフラムとを変位方向で同一の変位量となるよう連結する連結部材と、
前記変位方向において前記第2ダイヤフラムの側から前記一次側圧力導入路の導入端である一次側圧力導入端へ向けて第2付勢部材により付勢されて、前記一次側圧力導入端を開閉して前記一次側圧力導入端から前記第3室へ導入される一次側流体の流入量を調整する排気弁と、
当該排気弁に連結されると共に、前記第2ダイヤフラムに形成される開孔を開閉して前記第3室の側から前記第2室の側へ逃がす排出量を調整する開放弁とを備える点にある。
To achieve the above objectives, the pilot governor should:
A pilot governor used as a reverse acting pressure regulating device, characterized by:
A first chamber partitioned by a housing and a first diaphragm and communicating with a secondary pressure introduction path, and an open hole partitioned by the housing, the first diaphragm and the second diaphragm and open to the outside. A second chamber formed in the housing, and a primary side pressure introduction passage partitioned by the housing, the second diaphragm, and the third diaphragm are connected in communication, and driving pressure is introduced into the driving pressure chamber of the main governor. a third chamber to which a driving pressure introduction passage is connected, and a first biasing member that biases the third diaphragm toward the third chamber,
a connecting member that connects the first diaphragm, the second diaphragm, and the third diaphragm so that they have the same amount of displacement in a displacement direction;
In the displacement direction, the primary side pressure introduction end is opened and closed by being biased by the second biasing member from the side of the second diaphragm toward the primary side pressure introduction end, which is the introduction end of the primary side pressure introduction passage. an exhaust valve for adjusting an inflow amount of the primary side fluid introduced from the primary side pressure introduction end to the third chamber;
an open valve that is connected to the exhaust valve and opens and closes an opening formed in the second diaphragm to adjust the amount of discharge released from the third chamber side to the second chamber side; be.

上記特徴構成を有する3枚のダイヤフラムを有するパイロットガバナは、従来から逆作動型整圧装置として一般的に用いられている2枚のダイヤフラムを有するパイロットガバナと異なる構成を有するが、両者とも、二次圧が上昇すると、すべてのダイヤフラムが下降して、駆動圧が排出(3枚ダイヤフラムの構成の場合には第2室を介して外部へ排出、2枚ダイヤフラムの構成の場合には二次圧検知室へ排出)され、二次圧が低下すると、駆動圧がメインガバナに供給される構成となるため、基本的には、二枚のダイヤフラムを有するパイロットガバナと同様の周波数応答特性を示すものと考えられる。
更に、上記特徴構成を有するパイロットガバナによれば、開放弁を介して第3室から逃がされる排出圧は、第2室へ導かれ第1室へは導かれることはないから、第1室では、当該排出圧に乱されることのない入力として二次圧を導入できる。
結果、上記特徴構成を有するパイロットガバナは、一般的に用いられる逆作動型整圧装置のパイロットガバナの周波数応答特性と略同等の特性が得られるパイロットガバナとして活用することができる。
従って、入力として実際の圧力正弦波等を適切に投入できると共にその出力を駆動圧として、それらの値から制御特性を解析する周波数応答解析を実行可能な逆作動型整圧装置のパイロットガバナを実現できる。
The three-diaphragm pilot governor having the characteristic configuration described above has a different configuration from the two-diaphragm pilot governor generally used as a conventional reverse acting pressure regulating device. When the secondary pressure rises, all the diaphragms descend and the drive pressure is discharged (in the case of a three-diaphragm configuration, it is discharged to the outside via the second chamber, and in the case of a two-diaphragm configuration, the secondary pressure When the secondary pressure drops, the drive pressure is supplied to the main governor, so basically it exhibits the same frequency response characteristics as a pilot governor with two diaphragms. it is conceivable that.
Furthermore, according to the pilot governor having the above characteristic configuration, the exhaust pressure released from the third chamber via the open valve is guided to the second chamber and not to the first chamber. , a secondary pressure can be introduced as an input unperturbed by the discharge pressure.
As a result, the pilot governor having the characteristic structure described above can be utilized as a pilot governor that can obtain substantially the same frequency response characteristic as the pilot governor of a generally used reverse-acting pressure regulating device.
Therefore, a pilot governor for a reverse-acting pressure regulating device can be realized that can appropriately input an actual pressure sine wave, etc. as an input and that can use the output as a driving pressure to perform a frequency response analysis that analyzes the control characteristics from those values. can.

尚、上記特徴構成を有するパイロットガバナは、上述したような従来のパイロットガバナの周波数応答特性を知るための検証用として用いることができる他、逆作動型整圧装置のパイロットガバナとして実用に供することもできる。 The pilot governor having the above characteristic configuration can be used for verification to know the frequency response characteristics of the conventional pilot governor as described above, and can also be put to practical use as a pilot governor for a reverse-acting pressure regulator. can also

本発明に係るパイロットガバナの更なる特徴構成は、
前記連結部材は、内部が中空の中空部材から構成されている点にある。
A further characteristic configuration of the pilot governor according to the present invention is
The connection member is configured by a hollow member having a hollow interior.

本発明に係るパイロットガバナにおいては、3枚のダイヤフラムを連結する連結部材を備える必要があり、当該連結部材は、従来の2枚のダイヤフラムを有するパイロットガバナのダイヤフラムを連結する連結部材よりも、ダイヤフラムの変位方向で大型化する場合が想定される。
上記特徴構成によれば、連結部材を内部が中空に加工された中空部材から構成することで、軽量化を図ることができ、仮に大型になる場合であっても、重量の増加を抑制して、重量増加に伴う周波数応答特性の変動を抑制できる。
In the pilot governor according to the present invention, it is necessary to provide a connecting member that connects the three diaphragms. A case of increasing in size in the direction of displacement is assumed.
According to the above characteristic configuration, the connection member is made of a hollow member whose interior is processed to be hollow, so that weight reduction can be achieved, and even if the size becomes large, the increase in weight can be suppressed. , it is possible to suppress fluctuations in frequency response characteristics due to weight increase.

本発明に係るパイロットガバナの更なる特徴構成は、
前記第1室に対して周期圧力振動を付与する圧力振動付与部と、
前記第1室に導入される前記周期圧力振動を伴う模擬二次圧を計測可能な第1圧力計測部と、
前記駆動圧導入路に導入される前記駆動圧を計測可能な第2圧力計測部とを備える点にある。
A further characteristic configuration of the pilot governor according to the present invention is
a pressure vibration applying unit that applies periodic pressure vibration to the first chamber;
a first pressure measuring unit capable of measuring a simulated secondary pressure accompanied by the periodic pressure oscillation introduced into the first chamber;
and a second pressure measuring section capable of measuring the driving pressure introduced into the driving pressure introducing passage.

上記特徴構成によれば、第1室に対して圧力振動付与部により周期圧力振動を、模擬の二次圧として入力でき、第1圧力計測部にて計測した周期圧力振動と、当該周期圧力振動に伴って発生し第2圧力計測部にて計測される駆動圧とから、パイロットガバナの周波数を応答解析を実行できる。
そして、例えば、複数の周波数毎に、周期圧力振動を伴う模擬二次圧振動の振幅及び位相と、駆動圧振動の振幅及び位相とからボード線図を作成することで、ゲイン余裕及び位相余裕を導出し、それらの値から、系の安定性を好適に判定できる。
尚、当該判定は、実測に基づいた解析による判定であるため、種々の仮定を前提とする数値解析に基づく方法に比べ、より実態に即した判定を行うことができる。
According to the above characteristic configuration, the periodic pressure vibration can be input to the first chamber by the pressure vibration applying unit as the simulated secondary pressure, and the periodic pressure vibration measured by the first pressure measuring unit and the periodic pressure vibration Response analysis can be performed for the frequency of the pilot governor based on the driving pressure that is generated along with and measured by the second pressure measuring unit.
Then, for example, by creating a Bode diagram from the amplitude and phase of the simulated secondary pressure vibration accompanied by the periodic pressure vibration and the amplitude and phase of the driving pressure vibration for each of a plurality of frequencies, the gain margin and the phase margin are calculated. can be derived and from those values the stability of the system can be suitably determined.
Since this determination is based on analysis based on actual measurements, it is possible to make determinations that are more realistic than methods based on numerical analysis that presuppose various assumptions.

本発明に係るパイロットガバナとしては、
前記第1圧力計測部にて計測された前記第1室に導入される模擬二次圧振動の振幅及び位相と、前記第2圧力計測部にて計測された前記駆動圧導入路に導入される駆動圧振動の振幅及び位相とに基づいて周波数応答解析を実行する制御装置を備えることが好ましい。
As a pilot governor according to the present invention,
The amplitude and phase of the simulated secondary pressure vibration introduced into the first chamber measured by the first pressure measuring unit, and the driving pressure introduction path measured by the second pressure measuring unit A controller is preferably provided that performs a frequency response analysis based on the amplitude and phase of the drive pressure oscillation.

ただし、本発明のパイロットガバナは、制御装置を設けていなくても、第1圧力計測部や第2圧力計測部の計測値を、他の演算装置にて解析するような構成を採用しても構わない。 However, even if the pilot governor of the present invention is not provided with a control device, even if it adopts a configuration in which the measured values of the first pressure measurement unit and the second pressure measurement unit are analyzed by another arithmetic device. I do not care.

上記目的を達成するための整圧装置の特徴構成は、これまで説明してきたパイロットガバナを備える点にある。 A characteristic configuration of the pressure regulating device for achieving the above object is that it includes the pilot governor described above.

上記特徴構成によれば、これまで説明してきたパイロットガバナが奏する特異な作用効果を良好に発揮する逆作動型整圧装置を実現できる。 According to the characteristic configuration described above, it is possible to realize a reverse-acting pressure regulator that satisfactorily exhibits the unique effects of the pilot governor described above.

本発明の実施形態に係るパイロットガバナの概略構成図である1 is a schematic configuration diagram of a pilot governor according to an embodiment of the present invention; FIG. 本発明の実施形態に係るパイロットガバナが作動する場合の作用図であるFIG. 4 is an action diagram when the pilot governor according to the embodiment of the present invention operates; パイロットガバナへの入力としての周期圧力振動を伴う模擬二次圧のグラフ図、及び出力としての駆動圧のグラフ図であるFIG. 4 is a graphical representation of the simulated secondary pressure with periodic pressure oscillations as input to the pilot governor, and a graphical representation of the drive pressure as output;

本発明の実施形態に係るパイロットガバナ100、及びそれを備えた逆作動型整圧装置200は、入力として実際の圧力正弦波等を適切に投入できると共にその出力応答としての駆動圧を計測でき、それらの値から制御特性を解析する周波数応答解析を実行可能なものに関する。 The pilot governor 100 according to the embodiment of the present invention and the reverse-acting pressure regulating device 200 equipped with the same can appropriately input an actual pressure sine wave or the like as an input, and can measure the driving pressure as its output response. It relates to being able to perform frequency response analysis that analyzes control characteristics from those values.

逆作動型整圧装置200は、図1に示すように、流体流路L0の二次圧を設定圧力に調整する逆作動型のメインガバナ10と、そのメインガバナ10へ駆動圧を導入するパイロットガバナ100とを備えて構成されている。 As shown in FIG. 1, the reverse-acting pressure regulating device 200 includes a reverse-acting main governor 10 that adjusts the secondary pressure of the fluid flow path L0 to a set pressure, and a pilot that introduces driving pressure to the main governor 10. A governor 100 is provided.

メインガバナ10は、ダイヤフラムプレート14に沿って設けられる主ダイヤフラムD0を備えており、その内部空間が主ダイヤフラムD0にて第5室H5と第6室H6とに区画されている。そして、メインガバナ10は、流体流路L0に設けられる主開口部K0を開閉する主弁体V0を備えており、この主弁体V0は連結棒16にて主ダイヤフラムD0と連結され主ダイヤフラムD0と連動して動く形態で、開閉される構成となっている。また、第5室H5には、主ダイヤフラムD0を主弁体V0の閉弁方向側に付勢する主付勢バネG0が配設されている。 The main governor 10 has a main diaphragm D0 provided along the diaphragm plate 14, and the internal space thereof is divided into a fifth chamber H5 and a sixth chamber H6 by the main diaphragm D0. The main governor 10 includes a main valve body V0 that opens and closes a main opening K0 provided in the fluid flow path L0. It is configured to be opened and closed in a form that moves in conjunction with. A main biasing spring G0 that biases the main diaphragm D0 in the valve closing direction of the main valve body V0 is disposed in the fifth chamber H5.

パイロットガバナ100は、筐体Kと第1ダイヤフラムD1とにより区画され二次側圧力導入路L2が連通接続される第1室H1と、筐体Kと第1ダイヤフラムD1と第2ダイヤフラムD2とにより区画され外部へ開放される開放孔K1が筐体Kに形成される第2室H2と、筐体Kと第2ダイヤフラムD2と第3ダイヤフラムD3とにより区画され一次側圧力導入路L1が連通接続されると共にメインガバナ10の第6室H6(駆動圧室の一例)に駆動圧を導入する駆動圧導入路L4が連通接続される第3室H3と、第3ダイヤフラムD3を第3室H3の側へ付勢する第1付勢部材G1と、第1ダイヤフラムD1と第2ダイヤフラムD2と第3ダイヤフラムD3とを変位方向(図1で矢印Z方向)で同一の変位量となるよう連結する連結部材Rと、変位方向において第2ダイヤフラムD2の側から一次側圧力導入路L1の導入端である一次側圧力導入端L1aへ向けて第2付勢部材G2により付勢されて、一次側圧力導入端L1aを開閉して一次側圧力導入端L1aから第3室H3へ導入される一次側流体の流入量を調整する排気弁V1と、当該排気弁V1に連結されると共に、第2ダイヤフラムD2に形成される開孔DP2aを開閉して第3室H3の側から第2室H2の側へ逃がす排出量を調整する開放弁V2とを有する。
ここで、駆動圧導入路L4は、流路径を絞る絞り39を有する第3流体流路L3を介して、二次側圧力導入路L2に連通接続されている。また、第1付勢部材G1の第3ダイヤフラムD3と逆側の基端側端部は、筐体Kの内周面に設けられた雌螺子部G2bに螺合する形態で設けられる受け皿G2aに当接しており、当該受け皿G2aは雌螺子部G2bへ螺合しながら回転することで、変位方向(図1で矢印Z方向)に移動自在に構成されている。
The pilot governor 100 includes a first chamber H1 partitioned by the housing K and the first diaphragm D1 and connected to the secondary side pressure introduction path L2, and the housing K, the first diaphragm D1 and the second diaphragm D2. A second chamber H2 in which an open hole K1 that is partitioned and opened to the outside is formed in the housing K, and a primary side pressure introduction path L1 that is partitioned by the housing K, the second diaphragm D2, and the third diaphragm D3 are communicated. and a third chamber H3, to which a driving pressure introduction path L4 for introducing driving pressure into a sixth chamber H6 (an example of a driving pressure chamber) of the main governor 10 is communicated and connected; A connection that connects the first biasing member G1 that biases to the side, the first diaphragm D1, the second diaphragm D2, and the third diaphragm D3 so that they have the same amount of displacement in the displacement direction (direction of arrow Z in FIG. 1). The member R is biased by the second biasing member G2 from the side of the second diaphragm D2 in the displacement direction toward the primary pressure introduction end L1a, which is the introduction end of the primary pressure introduction path L1, to introduce the primary pressure. an exhaust valve V1 that opens and closes the end L1a to adjust the amount of inflow of the primary side fluid introduced from the primary side pressure introduction end L1a into the third chamber H3; It also has an open valve V2 that opens and closes the formed opening DP2a to adjust the amount of discharge to escape from the third chamber H3 side to the second chamber H2 side.
Here, the drive pressure introduction path L4 is connected to the secondary side pressure introduction path L2 via a third fluid flow path L3 having a throttle 39 that narrows the flow path diameter. In addition, the end of the first biasing member G1 on the opposite side to the third diaphragm D3 is attached to a receptacle G2a provided so as to be screwed into a female threaded portion G2b provided on the inner peripheral surface of the housing K. The tray G2a is configured to be freely movable in the displacement direction (the arrow Z direction in FIG. 1) by rotating while being screwed into the female screw portion G2b.

尚、第1ダイヤフラムD1には第1ダイヤフラムプレートDP1が設けられ、第2ダイヤフラムD2には第2ダイヤフラムプレートDP2が設けられ、第3ダイヤフラムD3には第3ダイヤフラムプレートDP3が設けられており、連結部材Rは、第1ダイヤフラムプレートDP1と第2ダイヤフラムプレートDP2と第3ダイヤフラムプレートDP3とを連結する形態で設けられている。 The first diaphragm D1 is provided with a first diaphragm plate DP1, the second diaphragm D2 is provided with a second diaphragm plate DP2, and the third diaphragm D3 is provided with a third diaphragm plate DP3. The member R is provided in a form that connects the first diaphragm plate DP1, the second diaphragm plate DP2, and the third diaphragm plate DP3.

上述の構成において第1付勢部材G1及び第2付勢部材G2の付勢力を適切に設定することで、流体流路L0の二次圧P2が設定圧力よりも昇圧した場合、図2(a)に示すように、第1室H1の圧力が昇圧することにより、第1付勢部材G1の付勢力に抗して、第1ダイヤフラムD1と第2ダイヤフラムD2と第3ダイヤフラムD3とが第1付勢部材G1の側へ変位する。これにより、排気弁V1が閉じ側へ動作されると共に開放弁V2が開き側へ動作され、第3室H3への一次圧P1の導入が停止されると共に、第3室H3の圧が第2室H2及び開放孔K1を介して外部へ放出される。これにより、第6室H6の圧は、駆動圧導入路L4、開孔DP2a、開放孔K1を介して、外部へ排出され、第6室H6の圧力は低下し、第5室H5と第6室H6との圧力差により主ダイヤフラムD0が第6室H6側に変位する。よって、メインガバナ10の主弁体V0が閉じ側に動作され、流体流路L0の二次圧P2を低下させて二次圧P2を設定圧力に調整する。
尚、開孔DP2aの開度は、二次圧P2と設定圧力との圧力差が大きいほど大きくなるように構成されている。
By appropriately setting the biasing forces of the first biasing member G1 and the second biasing member G2 in the above-described configuration, when the secondary pressure P2 in the fluid flow path L0 rises above the set pressure, FIG. ), the first diaphragm D1, the second diaphragm D2, and the third diaphragm D3 are pushed against the biasing force of the first biasing member G1 by increasing the pressure in the first chamber H1. It is displaced to the biasing member G1 side. As a result, the exhaust valve V1 is closed and the release valve V2 is opened, thereby stopping the introduction of the primary pressure P1 into the third chamber H3 and reducing the pressure in the third chamber H3 to the second pressure. It is discharged to the outside through the chamber H2 and the open hole K1. As a result, the pressure in the sixth chamber H6 is discharged to the outside through the driving pressure introduction path L4, the opening DP2a, and the opening K1. The main diaphragm D0 is displaced toward the sixth chamber H6 due to the pressure difference with the chamber H6. Therefore, the main valve body V0 of the main governor 10 is operated to the closing side, the secondary pressure P2 in the fluid flow path L0 is decreased, and the secondary pressure P2 is adjusted to the set pressure.
The opening degree of the opening DP2a is designed to increase as the pressure difference between the secondary pressure P2 and the set pressure increases.

一方、流体流路L0の二次圧P2が設定圧力よりも降圧した場合、図2(b)に示すように、二次側圧力導入路L2にて流体流路L0の二次側に連通接続されたパイロットガバナ100の第1室H1の圧力が低下し、第1付勢部材G1の付勢力により第1ダイヤフラムD1と第2ダイヤフラムD2と第3ダイヤフラムD3とが第1室H1の側へ変位する。これにより、排気弁V1が開き側へ動作すると共に開放弁V2が閉じ側へ動作し、一次側圧力導入路L1を介して第3室H3へ流体流路L0の一次側が導入され、第3室H3の圧力が上昇する。そして、その圧力上昇した第3室H3の圧力が駆動圧導入路L4を介してメインガバナ10の第6室H6へ駆動圧として導入され、第6室H6の圧力も上昇し、第5室H5と第6室H6との圧力差により主ダイヤフラムD0が第5室H5側に変位する。よって、メインガバナ10の主弁体V0が開き側に動作され、流体流路L0の二次圧P2を上昇させて二次圧P2を設定圧力に調整する。 On the other hand, when the secondary pressure P2 of the fluid flow path L0 drops below the set pressure, as shown in FIG. The pressure in the first chamber H1 of the pilot governor 100 is lowered, and the biasing force of the first biasing member G1 displaces the first diaphragm D1, the second diaphragm D2, and the third diaphragm D3 toward the first chamber H1. do. As a result, the exhaust valve V1 operates to open and the release valve V2 operates to close, and the primary side of the fluid flow path L0 is introduced into the third chamber H3 via the primary side pressure introduction path L1. H3 pressure rises. Then, the increased pressure of the third chamber H3 is introduced as a driving pressure into the sixth chamber H6 of the main governor 10 via the driving pressure introduction path L4, and the pressure of the sixth chamber H6 also increases, and the pressure of the fifth chamber H5 and the sixth chamber H6, the main diaphragm D0 is displaced toward the fifth chamber H5. Therefore, the main valve body V0 of the main governor 10 is operated to the opening side, the secondary pressure P2 in the fluid flow path L0 is increased, and the secondary pressure P2 is adjusted to the set pressure.

さて、これまで説明してきた3枚のダイヤフラムを有するパイロットガバナ100は、周期圧力振動を伴う模擬二次圧P2を二次圧検知室としての第1室H1へ加えたときに、特許文献1(特開2017-12718号公報)に示される従来の逆作動型整圧装置に用いられる2枚のダイヤフラムを有するパイロットガバナと略同等の周波数応答特性を得られるよう以下のような構成を有している。 Now, the pilot governor 100 having three diaphragms that has been explained so far, when the simulated secondary pressure P2 accompanied by periodic pressure oscillation is applied to the first chamber H1 as the secondary pressure detection chamber, Patent Document 1 ( It has the following configuration so as to obtain substantially the same frequency response characteristics as the pilot governor having two diaphragms used in the conventional reverse acting pressure regulator disclosed in Japanese Patent Application Laid-Open No. 2017-12718. there is

第1ダイヤフラムD1と第2ダイヤフラムD2と第3ダイヤフラムD3の有効受圧面積は、略同等に構成されており、好ましくは、当該有効受圧面積は、従来の逆作動型のパイロットガバナのダイヤフラムの有効受圧面積と等しく構成されている。
また、第1ダイヤフラムD1と第2ダイヤフラムD2と第3ダイヤフラムD3を連結する連結部材Rは、例えば、変位方向(図1で矢印Z方向)に沿って伸びると共に第1ダイヤフラムプレートDP1と第2ダイヤフラムプレートDP2と第3ダイヤフラムプレートDP3とを連結する複数の棒状部材R1(当該実施形態では、2本で、且つ内部が中空の部材)にて構成することができる。
The effective pressure-receiving areas of the first diaphragm D1, the second diaphragm D2, and the third diaphragm D3 are configured to be substantially equal, and preferably, the effective pressure-receiving areas are equal to those of the diaphragms of the conventional reverse-acting pilot governor. Constructed equal to the area.
Further, the connecting member R that connects the first diaphragm D1, the second diaphragm D2 and the third diaphragm D3 extends, for example, along the displacement direction (direction of arrow Z in FIG. 1) and the first diaphragm plate DP1 and the second diaphragm. A plurality of rod-shaped members R1 (in this embodiment, two members with a hollow interior) connecting the plate DP2 and the third diaphragm plate DP3 can be used.

また、二次圧P2と排気弁V1のストロークや振動可能部の質量の関係は、従来のパイロットガバナと略同等の性能が得られる。因みに、振動可能部は、連結部材R、第1ダイヤフラムD1、第2ダイヤフラムD2、第3ダイヤフラムD3を含むものである。より厳密には、上記関係は、排気弁V1、開放弁V2、第1ダイヤフラムD1、第2ダイヤフラムD2、第3ダイヤフラムD3の質量の影響も受けるものである。 In addition, the relationship between the secondary pressure P2, the stroke of the exhaust valve V1, and the mass of the vibrating portion provides substantially the same performance as that of the conventional pilot governor. Incidentally, the vibratable portion includes the connecting member R, the first diaphragm D1, the second diaphragm D2, and the third diaphragm D3. More strictly, the above relationship is also affected by the masses of the exhaust valve V1, open valve V2, first diaphragm D1, second diaphragm D2, and third diaphragm D3.

更に、二次圧計測室としての第1室H1に対して、入力として周期圧力振動を伴う模擬二次圧を導入するべく、二次側圧力導入路L2には、二次側圧力導入路L2の開閉を切り替える開閉弁51が設けられている。
更に、第1室H1に対して、第1室H1に対して周期圧力振動を付与する圧力振動発生装置50(圧力振動付与部の一例)が設けられており、当該圧力振動発生装置50は、第1室H1への圧力導入を制御する圧力導入弁V3と、第1室H1からの圧力排出を制御する圧力排出弁V4とから構成されている。説明を追加すると、圧力導入弁V3は、第1室H1に連通接続されている一次側圧力導入路L1を開閉する形態で設けられ、圧力排出弁V4は、第1室H1に連通接続されている大気開放流路L5を開閉する形態で設けられている。
制御装置Cが、開閉弁51を閉止している状態で、第1圧力センサS1の検知圧力値に基づいて、圧力導入弁V3及び圧力排出弁V4の開閉を交互に切換制御することで、圧力振動を発生させることができる。
Further, in order to introduce a simulated secondary pressure accompanied by periodic pressure oscillation as an input into the first chamber H1 as a secondary pressure measurement chamber, the secondary pressure introduction passage L2 is provided in the secondary pressure introduction passage L2. An on-off valve 51 for switching between opening and closing is provided.
Furthermore, a pressure vibration generator 50 (an example of a pressure vibration applying unit) that applies periodic pressure vibration to the first chamber H1 is provided for the first chamber H1. It is composed of a pressure introduction valve V3 for controlling pressure introduction to the first chamber H1 and a pressure release valve V4 for controlling pressure discharge from the first chamber H1. In addition to the explanation, the pressure introduction valve V3 is provided in a form that opens and closes the primary side pressure introduction path L1 that communicates with the first chamber H1, and the pressure release valve V4 communicates with the first chamber H1. It is provided in such a manner as to open and close the atmosphere release flow path L5.
In a state where the on-off valve 51 is closed, the control device C alternately switches and controls the opening and closing of the pressure introduction valve V3 and the pressure discharge valve V4 based on the pressure value detected by the first pressure sensor S1. Vibration can be generated.

更に、第1室H1に導入される周期圧力振動を伴う模擬二次圧を計測可能な第1圧力センサS1(第1圧力計測部の一例)が、開閉弁51よりも第1室H1の側に設けられている。更に、駆動圧を計測可能な第2圧力センサS2(第2圧力計測部の一例)が、駆動圧導入路L4に設けられ、制御装置Cは、当該第1圧力センサS1及び第2圧力センサS2にて計測された圧力を受信可能に構成されている。
制御装置Cは、第1圧力センサS1にて計測された第1室H1に導入される周期圧力振動を伴う模擬二次圧振動の振幅及び位相と、第2圧力センサS2にて計測された駆動圧振動の振幅及び位相とに基づいて周波数応答解析を実行する。
Furthermore, a first pressure sensor S1 (an example of a first pressure measuring unit) capable of measuring the simulated secondary pressure accompanied by periodic pressure vibration introduced into the first chamber H1 is located on the first chamber H1 side of the on-off valve 51. is provided in Furthermore, a second pressure sensor S2 (an example of a second pressure measuring unit) capable of measuring the driving pressure is provided in the driving pressure introduction path L4, and the controller C controls the first pressure sensor S1 and the second pressure sensor S2. It is configured to be able to receive the pressure measured by.
The control device C controls the amplitude and phase of the simulated secondary pressure vibration accompanied by the periodic pressure vibration introduced into the first chamber H1 measured by the first pressure sensor S1 and the drive pressure measured by the second pressure sensor S2. A frequency response analysis is performed based on the amplitude and phase of the pressure oscillation.

さて、これまで説明してきたパイロットガバナ100の周波数応答解析方法の一例を説明する。 Now, an example of the frequency response analysis method of the pilot governor 100 explained so far will be explained.

操作者は、第1室H1と流体流路L0の二次側とを圧力の伝播を禁止するよう隔離すべく、開閉弁51を閉止する。
次に、制御装置Cが、圧力振動発生装置50に生成する周期圧力振動の周波数を初期値(例えば、複数の周波数の最小値が設定される:一例としては、0.1Hz)を設定され、圧力振動発生装置50が、設定された周波数の周期圧力振動を生成する圧力振動付与工程を実行する。
その後、制御装置Cは、設定された周波数において、第1圧力センサS1により計測された周期圧力振動に伴う模擬二次圧としての圧力を受信する圧力振動計測工程を実行すると共に、第2圧力センサS2により計測された駆動圧を受信する駆動圧計測工程を実行する。
所定の設定された周波数にて、計測される入力としての模擬二次圧と、出力としての駆動圧としては、例えば、図3に示すような値となる。因みに、図3にて設定されている周波数は、0.5Hzである。尚、図3では、実測値がプロットにて表示されると共に、そのサイン近似を曲線にて示している。
The operator closes the on-off valve 51 to isolate the first chamber H1 and the secondary side of the fluid flow path L0 so as to inhibit pressure propagation.
Next, the control device C sets the frequency of the periodic pressure vibration generated in the pressure vibration generator 50 to an initial value (for example, the minimum value of a plurality of frequencies is set: 0.1 Hz as an example), The pressure vibration generator 50 executes a pressure vibration imparting step of generating periodic pressure vibrations with a set frequency.
After that, the control device C performs a pressure vibration measurement step of receiving the pressure as a simulated secondary pressure associated with the periodic pressure vibration measured by the first pressure sensor S1 at the set frequency, and the second pressure sensor S1. A driving pressure measurement step of receiving the driving pressure measured in S2 is executed.
At a predetermined set frequency, the simulated secondary pressure as an input to be measured and the drive pressure as an output have values as shown in FIG. 3, for example. Incidentally, the frequency set in FIG. 3 is 0.5 Hz. In FIG. 3, the measured values are plotted and their sine approximations are shown by curves.

制御装置Cは、圧力振動発生装置50にて生成される周期圧力振動の周波数を段階的に増加させる。尚、ここで、周波数は、設定している周期圧力振動の周波数が所定の上限値に達するまで指数関数的に増加させることが好ましい。
次に、制御装置Cは、周波数毎で計測された周期圧力振動に伴う模擬二次圧振動の振幅及び位相と、駆動圧振動の振幅及び位相とからボード線図を出力する。
具体的には、計測された複数の異なる周波数毎で圧力振動計測工程にて計測された周期圧力振動を伴う模擬二次圧の振幅A1と駆動圧計測工程にて計測された駆動圧の振幅A2との比から導出されるゲインGを複数の周波数毎に出力するゲイン出力工程と、複数の異なる周波数毎で圧力振動計測工程にて計測された周期圧力振動を伴う模擬二次圧の位相と駆動圧計測工程にて計測された駆動圧の位相との差を複数の周波数毎に出力する位相出力工程とを実行し、ゲイン出力工程にて出力されたゲイン及び位相出力工程にて出力された位相の差を、ボード線図上にプロットする。
The control device C increases the frequency of the periodic pressure vibration generated by the pressure vibration generator 50 step by step. Here, it is preferable that the frequency is exponentially increased until the set frequency of the periodic pressure vibration reaches a predetermined upper limit.
Next, the control device C outputs a Bode diagram from the amplitude and phase of the simulated secondary pressure vibration accompanying the periodic pressure vibration measured for each frequency and the amplitude and phase of the driving pressure vibration.
Specifically, the amplitude A1 of the simulated secondary pressure accompanied by the periodic pressure oscillation measured in the pressure oscillation measurement step and the amplitude A2 of the drive pressure measured in the drive pressure measurement step are measured for each of a plurality of different measured frequencies. A gain output step of outputting the gain G derived from the ratio of the , for each of a plurality of frequencies, and a phase and drive of the simulated secondary pressure accompanied by the periodic pressure oscillation measured at each of a plurality of different frequencies in the pressure oscillation measurement step and a phase output step of outputting the difference from the phase of the driving pressure measured in the pressure measurement step for each of a plurality of frequencies, and the gain output in the gain output step and the phase output in the phase output step. Plot the difference on a Bode plot.

制御装置Cは、ゲイン出力工程にて出力されたゲインから導出されるゲイン余裕と、位相出力工程から導出される位相余裕とから作成されるボード線図に基づいて、パイロットガバナ100の安定性を判定する安定性判定工程を実行する。 The control device C calculates the stability of the pilot governor 100 based on the Bode diagram created from the gain margin derived from the gain output in the gain output process and the phase margin derived from the phase output process. Perform a stability determination step to determine.

〔別実施形態〕
(1)第1圧力センサS1は、二次圧検知室としての第1室H1の圧力を直接計測するものであっても構わない。
また、第2圧力センサS2にて計測される駆動圧は、主弁体V0の下流側配管の二次圧としても良い。
[Another embodiment]
(1) The first pressure sensor S1 may directly measure the pressure in the first chamber H1 as the secondary pressure detection chamber.
Further, the driving pressure measured by the second pressure sensor S2 may be the secondary pressure of the downstream pipe of the main valve body V0.

(2)圧力発生装置50の他の構成例としては、例えば、ルーツポンプにより第1室H1の内部圧力を振動させる形や、第1室H1に連通接続するチャンバ室を加熱・冷却してチャンバ内の気体の膨張・収縮により圧力振動を形成させる構成を採用することも可能である。 (2) Other structural examples of the pressure generating device 50 include, for example, a roots pump that vibrates the internal pressure of the first chamber H1, and a chamber that heats and cools the chamber communicating with the first chamber H1. It is also possible to employ a configuration in which pressure vibration is generated by expansion/contraction of the gas inside.

尚、上記実施形態(別実施形態を含む、以下同じ)で開示される構成は、矛盾が生じない限り、他の実施形態で開示される構成と組み合わせて適用することが可能であり、また、本明細書において開示された実施形態は例示であって、本発明の実施形態はこれに限定されず、本発明の目的を逸脱しない範囲内で適宜改変することが可能である。 It should be noted that the configurations disclosed in the above embodiments (including other embodiments, the same shall apply hereinafter) can be applied in combination with configurations disclosed in other embodiments as long as there is no contradiction. The embodiments disclosed in this specification are exemplifications, and the embodiments of the present invention are not limited thereto, and can be modified as appropriate without departing from the object of the present invention.

本発明のパイロットガバナ、及びそれを備えた逆作動型整圧装置は、入力として実際の圧力正弦波等を適切に投入できると共にその出力応答としての駆動圧を計測でき、それらの値から制御特性を解析する周波数応答解析を実行可能な逆作動型整圧装置のパイロットガバナ、及びそれを備えた逆作動型整圧装置として、有効に利用可能である。 The pilot governor of the present invention and the reverse-acting pressure regulating device equipped with the pilot governor can appropriately input an actual pressure sine wave or the like as an input, and can measure the driving pressure as its output response. can be effectively used as a pilot governor of a reverse-acting pressure regulating device capable of executing frequency response analysis, and a reverse-acting pressure regulating device having the pilot governor.

10 :メインガバナ
14 :ダイヤフラムプレート
100 :パイロットガバナ
200 :逆作動型整圧装置
D1 :第1ダイヤフラム
D2 :第2ダイヤフラム
D3 :第3ダイヤフラム
G1 :第1付勢部材
G2 :第2付勢部材
H1 :第1室
H2 :第2室
H3 :第3室
K :筐体
K1 :開放孔
L0 :流体流路
L1 :一次側圧力導入路
L1a :一次側圧力導入端
L2 :二次側圧力導入路
L4 :駆動圧導入路
P1 :一次圧
P2 :二次圧
R :連結部材
V0 :主弁体
V1 :排気弁
V2 :開放弁
10: Main governor 14: Diaphragm plate 100: Pilot governor 200: Reverse acting pressure regulator D1: First diaphragm D2: Second diaphragm D3: Third diaphragm G1: First biasing member G2: Second biasing member H1 : First chamber H2 : Second chamber H3 : Third chamber K : Housing K1 : Open hole L0 : Fluid flow path L1 : Primary side pressure introduction path L1a : Primary side pressure introduction end L2 : Secondary side pressure introduction path L4 : Driving pressure introduction path P1 : Primary pressure P2 : Secondary pressure R : Connecting member V0 : Main valve body V1 : Exhaust valve V2 : Release valve

Claims (5)

逆作動型整圧装置として用いるパイロットガバナであって、
筐体と第1ダイヤフラムとにより区画され二次側圧力導入路が連通接続される第1室と、前記筐体と前記第1ダイヤフラムと第2ダイヤフラムとにより区画され外部へ開放される開放孔が前記筐体に形成される第2室と、前記筐体と前記第2ダイヤフラムと第3ダイヤフラムとにより区画され一次側圧力導入路が連通接続されると共にメインガバナの駆動圧室に駆動圧を導入する駆動圧導入路が連通接続される第3室と、前記第3ダイヤフラムを前記第3室の側へ付勢する第1付勢部材とを備え、
前記第1ダイヤフラムと前記第2ダイヤフラムと前記第3ダイヤフラムとを変位方向で同一の変位量となるよう連結する連結部材と、
前記変位方向において前記第2ダイヤフラムの側から前記一次側圧力導入路の導入端である一次側圧力導入端へ向けて第2付勢部材により付勢されて、前記一次側圧力導入端を開閉して前記一次側圧力導入端から前記第3室へ導入される一次側流体の流入量を調整する排気弁と、
当該排気弁に連結されると共に、前記第2ダイヤフラムに形成される開孔を開閉して前記第3室の側から前記第2室の側へ逃がす排出量を調整する開放弁とを備えるパイロットガバナ。
A pilot governor used as a reverse acting pressure regulator,
A first chamber partitioned by a housing and a first diaphragm and communicating with a secondary pressure introduction path, and an open hole partitioned by the housing, the first diaphragm and the second diaphragm and open to the outside. A second chamber formed in the housing, and a primary side pressure introduction passage partitioned by the housing, the second diaphragm, and the third diaphragm are connected in communication, and driving pressure is introduced into the driving pressure chamber of the main governor. a third chamber to which a driving pressure introduction passage is connected, and a first biasing member that biases the third diaphragm toward the third chamber,
a connecting member that connects the first diaphragm, the second diaphragm, and the third diaphragm so that they have the same amount of displacement in a displacement direction;
In the displacement direction, the primary side pressure introduction end is opened and closed by being biased by the second biasing member from the side of the second diaphragm toward the primary side pressure introduction end, which is the introduction end of the primary side pressure introduction passage. an exhaust valve for adjusting an inflow amount of the primary side fluid introduced from the primary side pressure introduction end to the third chamber;
an open valve connected to the exhaust valve and opening and closing an opening formed in the second diaphragm to adjust the amount of discharge released from the third chamber side to the second chamber side. .
前記連結部材は、内部が中空の中空部材から構成されている請求項1に記載のパイロットガバナ。 2. A pilot governor according to claim 1, wherein said connecting member comprises a hollow member having a hollow interior. 前記第1室に対して周期圧力振動を付与する圧力振動付与部と、
前記第1室に導入される前記周期圧力振動を伴う模擬二次圧を計測可能な第1圧力計測部と、
前記駆動圧導入路に導入される前記駆動圧を計測可能な第2圧力計測部とを備える請求項1又は2に記載のパイロットガバナ。
a pressure vibration applying unit that applies periodic pressure vibration to the first chamber;
a first pressure measuring unit capable of measuring a simulated secondary pressure accompanied by the periodic pressure oscillation introduced into the first chamber;
3. The pilot governor according to claim 1, further comprising a second pressure measuring section capable of measuring the driving pressure introduced into the driving pressure introducing passage.
前記第1圧力計測部にて計測された前記第1室に導入される模擬二次圧振動の振幅及び位相と、前記第2圧力計測部にて計測された前記駆動圧導入路に導入される駆動圧振動の振幅及び位相とに基づいて周波数応答解析を実行する制御装置を備える請求項3に記載のパイロットガバナ。 The amplitude and phase of the simulated secondary pressure vibration introduced into the first chamber measured by the first pressure measuring unit, and the driving pressure introduction path measured by the second pressure measuring unit 4. The pilot governor of claim 3, comprising a controller that performs a frequency response analysis based on the amplitude and phase of the drive pressure oscillation. 請求項1~4の何れか一項に記載のパイロットガバナを備えた逆作動型整圧装置。 A reverse acting pressure regulator comprising the pilot governor according to any one of claims 1 to 4.
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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006285660A (en) 2005-03-31 2006-10-19 Osaka Gas Co Ltd Pressure governing device and characteristic adjustment method therefor
JP2015103013A (en) 2013-11-25 2015-06-04 大阪瓦斯株式会社 Pressure governor device
JP2017182718A (en) 2016-03-31 2017-10-05 大阪瓦斯株式会社 Pressure adjust device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006285660A (en) 2005-03-31 2006-10-19 Osaka Gas Co Ltd Pressure governing device and characteristic adjustment method therefor
JP2015103013A (en) 2013-11-25 2015-06-04 大阪瓦斯株式会社 Pressure governor device
JP2017182718A (en) 2016-03-31 2017-10-05 大阪瓦斯株式会社 Pressure adjust device

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