JP4384925B2 - Membrane gas meter membrane support structure - Google Patents

Membrane gas meter membrane support structure Download PDF

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JP4384925B2
JP4384925B2 JP2004028232A JP2004028232A JP4384925B2 JP 4384925 B2 JP4384925 B2 JP 4384925B2 JP 2004028232 A JP2004028232 A JP 2004028232A JP 2004028232 A JP2004028232 A JP 2004028232A JP 4384925 B2 JP4384925 B2 JP 4384925B2
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membrane
shaft
short
bearing
notch
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JP2005221319A (en
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恵 岩川
訓弘 藤本
滋 田川
富美夫 井上
二郎 水越
昇 磯野
豊 寺西
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Osaka Gas Co Ltd
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Osaka Gas Co Ltd
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Description

本発明は計量手段として、膜の往復運動を翼の揺動運動に変える機構を有する膜式ガスメーターの膜支持構造に関する。   The present invention relates to a membrane support structure for a membrane gas meter having a mechanism for changing a reciprocating motion of a membrane into a swinging motion of a blade as a metering means.

従来の膜式ガスメーターの作動原理を説明すると、まず図11に示すように、ガスがメーター本体1の入口2よりバルブ3、分配室4を通過して、前後の計量室5,6の一方に突入し、さらに各計量室5,6は膜7によって前部屋8,9、後部屋10,11に仕切ってあり、このうち、ガスが突入した部屋は圧力差によって膜7が移動して広くなり、一方、膜7の移動によって狭くなった部屋のガスが再度、分配室4、バルブ3を経て出口12に排出される。また、膜7の往復運動は図2に示すように、ガスが突入した計量室5,6内の翼13の揺動運動に変えられた後に計量室5,6外のリンク機構14に伝えられ、最終的にメーター支持部(図示省略)が駆動する。さらに、図12の(イ)から(ニ)に示すようにリンク機構14の動きに伴ってバルブ3が所定角度に回転すると、バルブ3と分配室4との連通の仕方が変わり、入口2に連通する計量室5,6の部屋が切り換わると共に、出口12に連通する部屋が切り換わる。従って、ガスの使用によってガスの出入りする部屋が図12の(イ)、(ロ)、(ハ)、(ニ)の順番に変わり、それに伴って、前後の膜7が順々に往復運動することになり、ガスの計量が行われる。
尚、図11と図12の各図は対応している。
The operation principle of the conventional membrane gas meter will be explained. First, as shown in FIG. 11, the gas passes through the valve 3 and the distribution chamber 4 from the inlet 2 of the meter body 1 and enters one of the front and rear measuring chambers 5 and 6. Each of the measuring chambers 5 and 6 is further divided into front chambers 8 and 9 and rear chambers 10 and 11 by a membrane 7, and among these chambers, the membrane 7 moves and widens due to a pressure difference. On the other hand, the gas in the room narrowed by the movement of the membrane 7 is discharged again to the outlet 12 through the distribution chamber 4 and the valve 3. Further, as shown in FIG. 2, the reciprocating motion of the membrane 7 is transmitted to the link mechanism 14 outside the measuring chambers 5 and 6 after being changed to the swinging motion of the blades 13 in the measuring chambers 5 and 6 into which gas has entered. Finally, the meter support (not shown) is driven. Further, as shown in FIGS. 12A to 12D, when the valve 3 rotates to a predetermined angle in accordance with the movement of the link mechanism 14, the way of communication between the valve 3 and the distribution chamber 4 changes, and the inlet 2 The rooms of the measuring chambers 5 and 6 that communicate with each other are switched, and the room that communicates with the outlet 12 is switched. Accordingly, the room where the gas enters and exits changes in the order of (a), (b), (c), and (d) in FIG. 12 with the use of the gas, and the front and rear membranes 7 reciprocate in sequence accordingly. As a result, gas is metered.
11 and FIG. 12 correspond to each other.

ここで膜7の往復運動は前述したように、翼13の揺動運動を変えられるが、該膜7の支持構造は図13乃至図15に示すように、膜7を挟持する一対の膜板15,15に軸受16を固定し、翼13の先の短軸17a,17bに軸受16を嵌め合わせて係合した構造となっている。また、軸受16の軸通し穴18a,18bがほぼC字状をなしていた。   Here, the reciprocating motion of the membrane 7 can change the swinging motion of the blade 13 as described above, but the supporting structure of the membrane 7 is a pair of membrane plates sandwiching the membrane 7 as shown in FIGS. The bearing 16 is fixed to 15 and 15, and the bearing 16 is fitted and engaged with the short shafts 17 a and 17 b at the tip of the blade 13. Further, the shaft through holes 18a and 18b of the bearing 16 were substantially C-shaped.

ここで使用される軸受16は一般に、両短軸17a,17bをそれぞれスナップ式に押し込んで嵌め合わせられるように、該軸受16の上下に設けている両軸通し穴18a,18bにおいて、双方が着脱可能となる切欠を上下同一の幅でそれぞれ設けているものであった。このようにすると、軸受16と翼13の短軸17a、17bとのそれぞれの係合状態が弱く、例えば、ガスメーターの現場設置時や或いは搬送途中等に外部からの強い衝撃が加わった場合には、軸受16から短軸17a,17bが不意に離脱する不都合があった。また軸受16は、膜7の運動を短軸17a,17bに伝える役割を果たすので、その軸通し穴18a,18bの形状が短軸17a,17bの動きを左右することになる。そして従来の軸通し穴18a,18bの形状は、軸受16と短軸17a,17bとの嵌め合わせを容易とするために、各切欠19a,19bの幅をある程度広く形成しており、しかも、両短軸17a,17bの往復する方向と一致する位置に前記切欠19a,19bに短軸17a,17bが当たり、これが翼13側に伝達した場合には、翼13揺動時のがたつきが大きくなり、結果的に、計量誤差が生じる問題点があった。
特開2003−14521号公報(第1頁目、図1)
The bearing 16 used here is generally attached and detached at both shaft through-holes 18a and 18b provided above and below the bearing 16 so that both the short shafts 17a and 17b can be fitted into each other by snapping. The possible notches were respectively provided with the same width in the upper and lower sides. In this way, the engagement state between the bearing 16 and the short shafts 17a and 17b of the blade 13 is weak. For example, when a strong impact is applied from the outside when the gas meter is installed on the site or during transportation. The short shafts 17a and 17b are unexpectedly detached from the bearing 16. Further, the bearing 16 plays a role of transmitting the movement of the film 7 to the short shafts 17a and 17b. Therefore, the shape of the shaft through holes 18a and 18b affects the movement of the short shafts 17a and 17b. The shapes of the conventional shaft through holes 18a and 18b are such that the widths of the notches 19a and 19b are formed to be somewhat wide in order to facilitate the fitting of the bearing 16 and the short shafts 17a and 17b. When the short shafts 17a and 17b hit the notches 19a and 19b at positions corresponding to the reciprocating direction of the short shafts 17a and 17b, and the short shafts 17a and 17b are transmitted to the blade 13, the rattling of the blade 13 is large. As a result, there is a problem that a measurement error occurs.
Japanese Patent Laying-Open No. 2003-14521 (first page, FIG. 1)

本発明は、ガスメーター本体からの膜の不意な離脱を防止し、しかも、該膜側に固定した軸受から、翼軸への力の伝わり方を、膜の往動時と復動時とにおいて均一にすることを目的としている。   The present invention prevents unintentional detachment of the membrane from the gas meter main body, and the force transmitted from the bearing fixed to the membrane side to the blade axis is uniform during forward and backward movement of the membrane. The purpose is to be.

本発明のうち請求項1記載の発明は、メーター本体の前後に計量室を有し、各計量室内に翼軸の一部を突入し、該翼軸に固定した翼が前後に揺動し、さらに翼に軸受を連結し、膜を挟持した一対の膜板に軸受を固定し、各計量室内を膜が往復運動する膜式ガスメーターの膜支持構造であって、翼は、その先部における上部と下部にそれぞれ相反する方向に短軸を突出し、また軸受はコ字状をなし、上下に対向する各係合片には、前記両短軸をそれぞれ係合する各軸通し穴は切欠を有したC字状に形成し、前記各切欠のうち、いずれか一方側の切欠は、短軸による軸通し穴の貫通方向への差込みが可能である共に、該短軸の切欠からの抜け出しが不能な幅に形成してあり、また他方側の切欠は、短軸をスナップ式に着脱できる幅に形成していることを特徴とする。   The invention according to claim 1 of the present invention has measuring chambers in front and rear of the meter body, and a part of the blade shaft is inserted into each measuring chamber, and the blade fixed to the blade shaft swings back and forth. Further, the bearing is connected to the wing, the bearing is fixed to a pair of membrane plates sandwiching the membrane, and the membrane support structure of the membrane gas meter in which the membrane reciprocates in each measuring chamber. And the lower part protrudes in opposite directions, the bearing has a U-shape, and each of the engaging pieces that are vertically opposed to each other has a notch in each through hole that engages both the short axes. The notch on either side of the notches can be inserted into the through-hole of the shaft through the short shaft and cannot be removed from the notch of the short shaft. The width of the notch on the other side is such that the short shaft can be snapped on and off. And wherein the door.

軸通し穴に設ける切欠の形状は、軸通し穴の貫通方向に沿って一直線状の切り込みを設けるものが一般的であるが、例えば、波形をなすものであってもよく、その形状を特に限定するものではない。また両切欠の幅は、一方側を他方側よりも狭く形成するが、具体的な切欠の幅としては、一方はスナップ式に着脱できる程度とし、他方は、軸通し穴に短軸を嵌め合わせた際に容易に外れない程度の幅であればよい。   The shape of the notch provided in the through hole is generally provided with a straight cut along the through direction of the through hole. However, for example, the shape may be a waveform, and the shape is particularly limited. Not what you want. The width of both cutouts is narrower on one side than the other, but the specific cutout width is such that one can be snapped on and off, and the other is fitted with a short shaft in the through hole. It is sufficient that the width is such that it cannot be easily removed.

そして上記のように形成されたガスメーターは、一方の翼の短軸を切欠の幅の狭い方の軸通し穴に差し込んでいることで、不意な外力では容易に外れない構造となっており、また他方の翼軸は、切欠の幅を広くした軸通し穴に対して、スナップ式に嵌め合わせができ、これにより、切欠の幅の狭い方に短軸を差し込んだ後に、幅の広い方にスナップ式に嵌め込む手順をとることで、翼と膜との着脱が容易となる。   The gas meter formed as described above has a structure in which the short axis of one wing is inserted into the narrower through-hole of the notch so that it cannot be easily removed by an unexpected external force. The other wing shaft can be snap-fitted into the through-hole with the wider notch, so that after inserting the short shaft into the narrower notch, snap into the wider one. By taking the procedure of fitting into the equation, the wing and the membrane can be easily attached and detached.

また本発明のうち請求項2記載の発明では、前記各切欠は、両短軸の往復動方向と相違する箇所に設けているので、膜の往復動時に両短軸が各切欠に当たらず、この結果、当該各切欠による僅かな凹みによる両短軸のがたつきが生じない。
ここで切欠を設ける箇所は、膜の往復動の際に、両短軸の往復動方向と一致しない箇所であれば、係合片のどこに設けてもよい。
Further, in the invention according to claim 2 of the present invention, since each notch is provided at a location different from the reciprocating direction of both short axes, both the short axes do not hit each notch during the reciprocating movement of the membrane, As a result, the short shafts do not rattle due to slight recesses caused by the respective notches.
Here, the portion where the notch is provided may be provided anywhere on the engagement piece as long as it does not coincide with the reciprocating direction of both short axes during the reciprocating motion of the membrane.

本発明のうち請求項1記載の発明によれば、上下それぞれの軸通し穴の一方の切欠の幅を短軸の抜け出しが不能となるように狭く、そして、他方の切欠の幅を短軸がスナップ式に嵌め込まれるように広く形成しているので、翼と軸受との係合がしやすく、しかも、翼が軸受から容易に離脱しにくい構成となるので、ガスメーター設置時、あるいは該ガスメーターの搬送時等においてもしっかりと係合状態を保つ。   According to the first aspect of the present invention, the width of one notch in each of the upper and lower shaft through holes is made narrow so that the minor axis cannot be pulled out, and the width of the other notch is made shorter than the minor axis. Since it is widely formed so that it can be fitted into a snap type, it is easy to engage the blade with the bearing, and the blade is not easily detached from the bearing, so when installing the gas meter or transporting the gas meter It keeps the engaged state firmly even at times.

本発明のうち請求項2記載の発明によれば、請求項1記載の発明の効果に加えて、膜の往復運動時に両短軸が軸通し穴の切欠によってできた凹みに当たらないので、膜の往復運動時のがたつきが生じず、この結果、一層の計量精度の向上が見込まれる。   According to the invention of the second aspect of the present invention, in addition to the effect of the invention of the first aspect, the two short axes do not hit the dent formed by the notch of the through-hole during the reciprocating movement of the film. As a result, the measurement accuracy is expected to be further improved.

以下、本発明の膜式ガスメーターの膜支持構造を各図面に基づいて説明する。
尚、従来例と共通する構成要素には同一の符号を付けるものとする。
Hereinafter, the membrane support structure of the membrane gas meter of the present invention will be described with reference to the drawings.
In addition, the same code | symbol shall be attached | subjected to the component which is common in a prior art example.

まず膜支持構造は、膜7の往復運動を翼13の揺動運動に変えるもので、図9又は図10に示すように、計量室5,6外から計量室5,6内に翼軸20の一部を突入し、翼軸20に翼13を固定し、翼13の先の短軸17a、17bに軸受16を係合し、一対の膜板15,15に挟持された膜6に軸受16を固定している。
尚、翼軸20の上部はリンク機構14に固定されており、翼軸20の回転に伴ってリンク機構14が動く構造となっている。
First, the membrane support structure changes the reciprocating motion of the membrane 7 into the swinging motion of the blade 13, and as shown in FIG. 9 or 10, the blade shaft 20 extends from the outside of the measuring chambers 5 and 6 into the measuring chambers 5 and 6. Is inserted into the blade shaft 20, the blade 13 is fixed to the blade shaft 20, the bearing 16 is engaged with the short shafts 17 a and 17 b at the tip of the blade 13, and the bearing is fixed to the film 6 sandwiched between the pair of film plates 15 and 15. 16 is fixed.
The upper part of the blade shaft 20 is fixed to the link mechanism 14, and the link mechanism 14 moves as the blade shaft 20 rotates.

そして軸受16は図5に示すように、仲介片21の上下から係合片22を横向きに突出したコ字状となっており、両係合片22a,22bにC字状をなす軸通し穴18a,18bを対向して開け、膜7側に固定する雄ネジ23を仲介片21の中間高さ部分から係合片22a,22bとは反対側に向けて突出している(図4参照)。また、図4に示すように雄ネジ23にねじ込んだナット24と仲介片21の間に、膜板15,15に挟持された膜7を固定する。   As shown in FIG. 5, the bearing 16 has a U-shape in which the engagement piece 22 protrudes laterally from the upper and lower sides of the mediating piece 21, and the engagement holes 22a and 22b have C-shaped shaft through holes. 18a and 18b are opened facing each other, and a male screw 23 for fixing to the membrane 7 side protrudes from the intermediate height portion of the mediating piece 21 toward the opposite side to the engaging pieces 22a and 22b (see FIG. 4). Further, as shown in FIG. 4, the membrane 7 sandwiched between the membrane plates 15 and 15 is fixed between the nut 24 screwed into the male screw 23 and the mediating piece 21.

また翼13は図1乃至図4に示すように、平面視すると膜7の皿形状に合わせて屈曲しており、図6のように翼軸20側よりも先部側が低くなっており、先部に係合した軸受16が膜7の中央部に配置される(図9参照)。先部の縦桟27の上側と下側には、それぞれ短軸17a,17bが相反する方向、つまり上側の短軸17aは縦桟27から上方に向けて、一方、下側の短軸17bは縦桟27から下方に向けてそれぞれ突出している。さらに、上側の短軸17aの先端はテーパ状に細くなっており、軸通し穴18aへの差し込みが容易なものとなっている。   As shown in FIGS. 1 to 4, the wing 13 is bent in accordance with the dish shape of the membrane 7 in plan view, and the tip side is lower than the wing shaft 20 side as shown in FIG. The bearing 16 engaged with the portion is disposed at the center of the membrane 7 (see FIG. 9). On the upper side and the lower side of the front vertical bar 27, the short axes 17a and 17b are opposite to each other, that is, the upper short axis 17a is directed upward from the vertical bar 27, while the lower short axis 17b is Each projecting downward from the vertical beam 27. Furthermore, the tip of the upper short shaft 17a is tapered so that it can be easily inserted into the through hole 18a.

翼13に軸受16を係合する場合はまず図7(イ)のように、軸受16の上側の係合片22aの軸通し穴18aを、翼13における縦桟27の上側の短軸17aに下方側から差し込み、次いで図7(ロ)のように、下側の係合片22bの軸通し穴18bに下側の短軸17bをスナップ式に嵌め込む手順をとる。そして図7(ハ)のように、上側の短軸17aを基点にして、そのまま下側の軸通し穴18bの切欠19bに向けて下側の短軸17bを押し込むことで、上側の係合片22aにおいては、短軸17aが係合片22aの弾性を利用して軸通し穴18aの切欠19aを僅かに押し広げるので、図7(ニ)のように、下側の軸通し穴18bと短軸17bとが切欠19bを介してスナップ式に嵌め込まれ、翼13と軸受16との係合がなされる。   When engaging the bearing 16 with the blade 13, first, as shown in FIG. 7A, the shaft through hole 18 a of the engagement piece 22 a on the upper side of the bearing 16 is connected to the short shaft 17 a on the upper side of the vertical beam 27 in the blade 13. As shown in FIG. 7 (b), a procedure is adopted in which the lower short shaft 17b is snapped into the shaft through hole 18b of the lower engaging piece 22b as shown in FIG. Then, as shown in FIG. 7C, with the upper short shaft 17a as a base point, the lower short shaft 17b is pushed into the notch 19b of the lower shaft through hole 18b as it is, so that the upper engagement piece In 22a, the short shaft 17a uses the elasticity of the engaging piece 22a to slightly expand the notch 19a of the shaft through hole 18a, so that the short shaft through hole 18b and the short shaft through hole 18b are short as shown in FIG. The shaft 17b is snapped through the notch 19b, and the blade 13 and the bearing 16 are engaged.

また、各軸通し穴18a,18bに係合された両短軸17a,17bのうち、まず上側の短軸17aと軸通し穴18aとの係合状態は図8(イ)のように、切欠19aの幅が狭いために、該切欠19aからの短軸17aの離脱が不能となっている。次に、下側の短軸17bと軸通し穴18bとの係合状態は図8(ロ)のように、短軸17bの軸径を切欠19bの幅よりも僅かに大きく形成し、切欠19bの幅が上側の切欠19aに比べて広く形成してある。従って、係合する際には、係合片22bの有する弾性によって切欠19bの周辺部分が一時的に変形し、短軸17bが軸通し穴18bに嵌り込んでいる。さらに、切欠19a,19bの位置は、膜7の往復動方向と一致しない箇所に設けてある。また本実施形態では、図3に示すように翼軸20側に向けて切欠19a,19bが設けてあることで、膜7の往復時における前記両短軸17a,17bと各切欠19a,19bとの当接がなく、この結果、膜7の往復運動の際のがたつきが生じないことから、高精度の計量が見込まれる。   Of the short shafts 17a and 17b engaged with the shaft through holes 18a and 18b, the engagement state between the upper short shaft 17a and the shaft through hole 18a is notched as shown in FIG. Since the width of 19a is narrow, the short shaft 17a cannot be detached from the notch 19a. Next, as shown in FIG. 8 (b), the lower short shaft 17b and the shaft through hole 18b are engaged with each other so that the shaft diameter of the short shaft 17b is slightly larger than the width of the notch 19b. Is wider than the upper notch 19a. Therefore, when engaging, the peripheral portion of the notch 19b is temporarily deformed by the elasticity of the engaging piece 22b, and the short shaft 17b is fitted into the through hole 18b. Further, the positions of the notches 19a and 19b are provided at locations that do not coincide with the reciprocating direction of the membrane 7. Further, in the present embodiment, as shown in FIG. 3, the notches 19a and 19b are provided toward the blade shaft 20 side, so that the short shafts 17a and 17b and the notches 19a and 19b when the membrane 7 reciprocates are provided. As a result, there is no rattling during the reciprocating motion of the membrane 7, so that highly accurate weighing is expected.

次に膜7は、弾性を有する素材で皿状に形成され、その外周縁部を前後から挟持してシールし、挟持された部分以外がガスの圧力によって前後に往復運動する。また、膜7と膜板15の中央部には、軸受16の雄ネジ23を通す抜穴(図示は省略)が開けてある。   Next, the membrane 7 is formed in a dish shape with an elastic material, and the outer peripheral edge portion is sandwiched and sealed from the front and rear, and the portions other than the sandwiched portion reciprocate back and forth by the pressure of the gas. Further, a hole (not shown) through which the male screw 23 of the bearing 16 is passed is formed in the center of the membrane 7 and the membrane plate 15.

本発明の膜式ガスメーターの膜支持構造の縦断面図である。It is a longitudinal cross-sectional view of the film | membrane support structure of the film | membrane type gas meter of this invention. 同じく、本発明の膜式ガスメーターの膜支持構造の縦断面図である。Similarly, it is a longitudinal cross-sectional view of the membrane support structure of the membrane gas meter of the present invention. 本発明の膜式ガスメーターの膜支持構造の横断面図である。It is a cross-sectional view of the membrane support structure of the membrane gas meter of the present invention. 図3中Aを拡大して示す説明図である。It is explanatory drawing which expands and shows A in FIG. 本発明の膜式ガスメーターの軸受を示す斜視図である。It is a perspective view which shows the bearing of the film | membrane type gas meter of this invention. 本発明の膜式ガスメーターの翼を示す側面図である。It is a side view which shows the wing | blade of the membrane type gas meter of this invention. (イ)(ロ)(ハ)(ニ)は翼の短軸と軸受との係合の手順を示す説明図である。(A), (B), (C), and (D) are explanatory views showing a procedure of engagement between the short shaft of the blade and the bearing. (イ)は、図7(ニ)中のC−C線横断面図。(ロ)は、図7中のD−D線横断面である。(A) is the CC sectional view taken on the line in FIG.7 (d). (B) is a cross section taken along the line DD in FIG. 本発明の膜式ガスメーターの全体を示す一部を切欠した正面図である。It is the front view which notched a part which shows the whole film | membrane type gas meter of this invention. 本発明の膜式ガスメーターの全体を示す一部を切欠した側面図である。It is the side view which notched a part which shows the whole film | membrane type gas meter of this invention. (イ)(ロ)(ハ)(ニ)はガスの出入りする部屋が切り換わることを示す断面図である。(A), (B), (C), and (D) are cross-sectional views showing that the room where gas enters and exits is switched. (イ)(ロ)(ハ)(ニ)はリンク機構の動き及びバルブの回転運動と翼の揺動運動との関係を示す説明図である。(A), (B), (C), and (D) are explanatory views showing the relationship between the movement of the link mechanism and the rotational movement of the valve and the swinging movement of the blade. 従来の膜式ガスメーターの膜支持構造を示す横断面図である。It is a cross-sectional view showing a membrane support structure of a conventional membrane gas meter. (イ)は、従来の膜式ガスメーターの翼の側面図。(ロ)は(イ)中のB−B線断面図である。(A) is a side view of a wing of a conventional membrane gas meter. (B) is a sectional view taken along line BB in (A). 従来の膜式ガスメーターの膜支持構造の翼と軸受とを分解した平面図である。It is the top view which decomposed | disassembled the wing | blade and bearing of the film | membrane support structure of the conventional film | membrane type gas meter.

符号の説明Explanation of symbols

1 メーター本体
5,6 計量室
7 膜
13 翼
15 膜板
16 軸受
17a,17b 短軸
18a,18b 軸通し穴
19a,19b 切欠
20 翼軸
22a,22b 係合片
DESCRIPTION OF SYMBOLS 1 Meter main body 5,6 Measuring chamber 7 Membrane 13 Wing 15 Membrane plate 16 Bearing 17a, 17b Short shaft 18a, 18b Shaft through hole 19a, 19b Notch 20 Blade shaft 22a, 22b Engagement piece

Claims (2)

メーター本体(1)の前後に計量室(5,6)を有し、各計量室(5,6)内に翼軸(20)の一部を突入し、該翼軸(20)に固定した翼(13)が前後に揺動し、さらに翼(13)に軸受(16)を連結し、膜(7)を挟持した一対の膜板(15)に軸受(16)を固定し、各計量室(5,6)内を膜(7)が往復運動する膜式ガスメーターの膜支持構造であって、
翼(13)は、その先部における上部と下部にそれぞれ相反する方向に短軸(17a,17b)を突出し、
また軸受(16)はコ字状をなし、上下に対向する各係合片(22a,22b)には、前記両短軸(17a,17b)をそれぞれ係合する各軸通し穴(18a,18b)は切欠(19a,19b)を有したC字状に形成し、
前記各切欠(19a,19b)のうち、いずれか一方側の切欠(19a)は、短軸(17a)による軸通し穴(18a)の貫通方向への差込みが可能である共に、該短軸(17a)の切欠(19a)からの抜け出しが不能な幅に形成してあり、また他方側の切欠(19b)は、短軸(17b)をスナップ式に着脱できる幅に形成していることを特徴とする膜式ガスメーターの膜支持構造。
There are measuring chambers (5, 6) before and after the meter body (1), and a part of the blade shaft (20) is inserted into each measuring chamber (5, 6) and fixed to the blade shaft (20). The wing (13) swings back and forth, the bearing (16) is connected to the wing (13), and the bearing (16) is fixed to a pair of membrane plates (15) sandwiching the membrane (7). A membrane-type gas meter membrane support structure in which the membrane (7) reciprocates in the chamber (5, 6),
The wing (13) protrudes the short axis (17a, 17b) in the opposite direction to the upper part and the lower part at the tip part,
The bearing (16) is U-shaped, and the shaft through holes (18a, 18b) for engaging the short shafts (17a, 17b) with the engaging pieces (22a, 22b) facing vertically are respectively provided. ) Is formed in a C shape with notches (19a, 19b),
Of the notches (19a, 19b), the notch (19a) on either side can be inserted into the through-hole (18a) through the shaft through hole (18a) by the short shaft (17a). 17a) is formed in such a width that it cannot be removed from the notch (19a), and the notch (19b) on the other side is formed in such a width that the short shaft (17b) can be attached and detached in a snap manner. The membrane support structure of the membrane gas meter.
前記各切欠(19a,19b)は、両短軸(17a,17b)の往復動方向と相違する箇所に設けていることを特徴とする請求項1記載の膜支持構造。
The membrane support structure according to claim 1, wherein each of the notches (19a, 19b) is provided at a location different from the reciprocating direction of both short axes (17a, 17b).
JP2004028232A 2004-02-04 2004-02-04 Membrane gas meter membrane support structure Expired - Lifetime JP4384925B2 (en)

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