JPH0259416B2 - - Google Patents
Info
- Publication number
- JPH0259416B2 JPH0259416B2 JP13511682A JP13511682A JPH0259416B2 JP H0259416 B2 JPH0259416 B2 JP H0259416B2 JP 13511682 A JP13511682 A JP 13511682A JP 13511682 A JP13511682 A JP 13511682A JP H0259416 B2 JPH0259416 B2 JP H0259416B2
- Authority
- JP
- Japan
- Prior art keywords
- resistance temperature
- capacitors
- lng
- voltage
- amplifier
- 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
- 239000003990 capacitor Substances 0.000 claims description 26
- 239000007788 liquid Substances 0.000 claims description 17
- 238000009529 body temperature measurement Methods 0.000 claims description 5
- 238000012545 processing Methods 0.000 description 8
- 238000012827 research and development Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000005070 sampling Methods 0.000 description 4
- 238000009835 boiling Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical group C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 206010037660 Pyrexia Diseases 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K3/00—Thermometers giving results other than momentary value of temperature
- G01K3/08—Thermometers giving results other than momentary value of temperature giving differences of values; giving differentiated values
- G01K3/14—Thermometers giving results other than momentary value of temperature giving differences of values; giving differentiated values in respect of space
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
- G01K1/02—Means for indicating or recording specially adapted for thermometers
- G01K1/026—Means for indicating or recording specially adapted for thermometers arrangements for monitoring a plurality of temperatures, e.g. by multiplexing
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
Description
〔発明の技術分野〕
本発明はタンクロールオーバの防止に有用な
LNG貯蔵タンクの温度差計測装置に関する。
〔発明の技術的背景〕
LNG貯蔵タンクに貯蔵された液体のLNGは沸
点が低く、かつ数種の沸点の異なる成分から成立
つているため貯蔵中に特異現象が発生し問題とな
る。
即ち、LNGをタンクに貯蔵しておくと、タン
クが外気に暖められ徐々に気化が進んでいく。こ
の気化ガスはそのまま放置するとタンクの耐圧を
越えるおそれがあるため、一定圧力以下になるよ
うに気化ガスを外へ抜きとつている。一方、
LNGの成分は下記の表1に示すものであり、主
成分はメタンで比重が小さくかつ沸点も低い。
[Technical field of the invention] The present invention is useful for preventing tank rollovers.
This article relates to a temperature difference measuring device for an LNG storage tank. [Technical Background of the Invention] Liquid LNG stored in an LNG storage tank has a low boiling point and is composed of several components with different boiling points, which causes problems when a peculiar phenomenon occurs during storage. In other words, when LNG is stored in a tank, the tank is warmed by the outside air and vaporization progresses gradually. If this vaporized gas is left as it is, there is a risk of exceeding the withstand pressure of the tank, so the vaporized gas is vented to the outside to keep the pressure below a certain level. on the other hand,
The components of LNG are shown in Table 1 below, and the main component is methane, which has a low specific gravity and a low boiling point.
【表】【table】
しかし、上記従来方法によると、LNGは液温
が−160℃の極低温領域にあり、0℃から掛け離
れているため、高い分解能が得難く、各部温度差
を精度良く捉えることができないことからタンク
ロールオーバが発生するおそれがあつた。
〔発明の目的〕
本発明は上記従来技術の問題点を解消し、
LNG貯蔵タンクの各部温度差を精度良く捉え、
タンクロールオーバを確実に防止することのでき
るLNG貯蔵タンクの温度差計測装置を提供する
ことを目的とする。
〔発明の概要〕
このため、本発明はLNG貯蔵タンク内部の高
さ方向には間隔を置いて複数個の液温計測用
RTDを配置する。一方、LNG液面にはフロート
を浮かべてそこに基準温度計測用RTDを配置す
る。前記各RTDを定電流源に直列接続し、各液
温計測用RTDの電圧を保持する複数のコンデン
サを設ける。これらコンデンサと対に基準温度計
測用RTDの電圧を保持する複数のコンデンサを
設ける。このようにして対にした2つのコンデン
サを逆接続することにより、保持電圧の差電圧を
順次1対ずつアンプに入力し、増幅後、A/D変
換器を介してデイジタル化して取り出すようにし
たものである。
〔発明の実施例〕
以下、本発明を図面に示す実施例を参照して説
明する。
第1図は本発明の一実施例に係わる温度差計測
装置の全体構成図を示したもので、1はLNGを
貯蔵するタンク、2はタンク1内に貯蔵されてい
るLNG液部、3はLNG液部2から気化したガス
の充満している気層部である。4A〜4Nはタン
ク1内部の底面から天井面にわたつて等間隔に取
り付けられているセンサで、LNG液温度を測る
ためのものである。5はLNG液面に浮かべられ
たフロートで、そこにはLNG液部2と気層部3
の境界面の温度を測るセンサ6A〜6Nがセンサ
4A〜4Nに対応する数だけ設けられている。7
はスキヤナ、アンプ、A/D変換器から成る処理
装置である。
第2図は処理装置7の内部とセンサ6A〜6N
の接続回路を示したもので、8は定電流源、9は
コンデンサ10A〜10N,11A〜11Nを有
するスキヤナ、12はアンプ、13はA/D変換
器である。
以上の構成で、LNG液部2と気層部3の境界
面温度は外部の温度に影響されず、LNGの成分
と気層部の圧力が決まれば一定温度となるLNG
の気化温度であり、一種の基準温度とみなすこと
ができる。この基準温度計測用のセンサ6A〜6
Nと、タンク1内に等間隔で取り付けられたセン
サ4A〜4Nとは定電流源8から電流の供給を受
ける電流ループを形成している。従つて、センサ
4A〜4N,6A〜6NのRTDはそれぞれの温
度に応じて低抗値が変化し、これらのセンサに電
流が流れると、それぞれの抵抗値に応じた電圧降
下の電圧が発生する。この電圧はケーブルでスキ
ヤナ9まで導かれ、コンデンサに電荷を貯える。
スキヤナのコンデンサはサンプリング指令が出る
と、センサ側から離れ、アンプ側につながるよう
になつている。スキヤナのコンデンサはセンサ電
圧と同電圧にチヤージされ、アンプとつながるた
め、サンプリング指令がでた瞬間はあたかもアン
プは直接センサに接続されたようになる。このよ
うな方式は一般にフライングキヤパシタ方式と呼
ばれている。
この場合、スキヤナ9のコンデンサは10Aと
11A,10Bと11B……10Nと11Nがそ
れぞれ対となつて順次1対ずつサンプリング指令
に応じてゼンサ側からアンプ側に切り換わる。こ
れにより、センサ6A〜6Nとセンサ4A〜4N
の各電圧はそれぞれ逆バイアスされて読み取ら
れ、各基準温度とLNG液温の温度差電圧がアン
プ12へ出力する。
例えば、センサ6Aと4Aの電圧について説明
すると、コンデンサ10Aがセンサ側につながる
とき、その上側は負、下側は正極性に充電され
る。一方、コンデンサ11Aは上側が正、下側が
負極性に充電される。次いで、サンプリング指令
に応じてコンデンサ10A,11Aがアンプ側に
つながると、コンデンサ10Aの下側とコンデン
サ11Aの上側が接続され、コンデンサ10Aの
上側とコンデンサ11Aの下側がアンプ12の入
力端に接続される。この結果、アンプ12にはセ
ンサ6Aの電圧EAとセンサ4Aの電圧EB=EA+
ΔEの温度差電圧ΔE=EB−EAが入力する。
この温度差電圧ΔEはセンサ6A〜6Nと、セ
ンサ4A〜4Nの温度が同温であれば0Vとなる
値であり、僅かな温度差であつてもアンプ12の
ゲインを上げれば、温度差のみを拡大して読み取
ることができる。これにより、従来に比べて高精
度の温度計測が可能となる。即ち、従来のように
LNG液内のセンサ出力電圧をそのままアンプに
入力し、A/D変換器して処理する場合、前述し
たようにLNG液温は−160℃であり、0℃からか
なり離れた温度であるため、分解能は当然低くな
る。これに対して本実施例のように温度差電圧
ΔEで処理すれば、分解能は極めて高くなり、精
度のよい温度計測が可能となる。また、定電流源
8の電流変動に対しても、例えば変動率をαとす
ると、絶対温度で処理する場合はEB×αとなり、
EB≫ΔEのため、変動が大きくなるが、温度差で
処理する場合はその影響を小さく抑えることがで
きる。同様にアンプ系のゲイン変動、A/D変換
器のバラツキに対しても絶対温度で処理するより
も、その影響を少なくすることができる。
このようにして各センサ6A〜6Nと4A〜4
Nの温度差電圧ΔEを取り出し、アンプ12で増
幅し、A/D変換器13でデイジタル化した後
は、更に各温度差電圧ΔEの差を取り出し、この
センサ間温度差に応じてタンク内撹拌を自動的に
行うことにより、タンクロールオーバを防止する
ことができる。あるいは、各温度差電圧ΔEを直
接表示し、これを監視することによつて、タンク
内の撹拌を行なうようにしてもよい。
このとき、温度差電圧ΔEと共にその絶対温度
も知りたい場合は、フロート5に更に余分に1個
のセンサを取り付け、このセンサ出力を各温度差
電圧ΔEに処理装置7内で加えることにより簡単
に得られることができる。あるいは、従来同様各
センサ4A〜4Nより直接アンプ12に取り出す
ようにしてもよい。
尚、上記実施例では基準温度と測定する液温を
センサ6A〜6Nと4A〜4Nからコンデンサ1
0A〜10Nと11A〜11Nに取り出し、一対
ずつ順番にサンプリングして各温度差電圧ΔEを
取り出すようにしたが、第3図に示すように基準
温度測定用のセンサは6A1個のみとし、センサ
6Aの発生電圧をコンデンサ10A〜10Nにチ
ヤージするようにしても上記実施例同様の作用効
果が得られる。
〔発明の効果〕
以上のように本発明によれば、LNG貯蔵タン
ク内の温度差を高分解能かつ高精度に計測するこ
とができる結果、従来LNG貯蔵タンクの監視員
の細心の注意力に委ねられていたLNG貯蔵タン
クの監視が正確なデータに基づいて行なうことが
可能となり、監視員の負荷を軽減してLNG貯蔵
タンクを安全に管理することができるようにな
る。
However, according to the above conventional method, the liquid temperature of LNG is in the cryogenic region of -160℃, which is far from 0℃, so it is difficult to obtain high resolution and it is not possible to accurately capture the temperature difference in each part. There was a risk that a rollover would occur. [Object of the invention] The present invention solves the problems of the above-mentioned prior art,
Accurately captures temperature differences in each part of the LNG storage tank,
The purpose of the present invention is to provide a temperature difference measuring device for an LNG storage tank that can reliably prevent tank rollover. [Summary of the Invention] Therefore, the present invention provides a plurality of liquid temperature measuring devices spaced apart in the height direction inside the LNG storage tank.
Place the RTD. On the other hand, a float is placed on the LNG liquid surface and an RTD for reference temperature measurement is placed there. Each of the RTDs is connected in series to a constant current source, and a plurality of capacitors are provided to hold the voltage of each RTD for measuring liquid temperature. Paired with these capacitors are a plurality of capacitors that hold the voltage of the reference temperature measurement RTD. By connecting the two capacitors paired in this way in reverse, the difference voltage between the holding voltages is input to the amplifier one pair at a time, and after amplification, it is digitized and taken out via an A/D converter. It is something. [Embodiments of the Invention] The present invention will be described below with reference to embodiments shown in the drawings. FIG. 1 shows an overall configuration diagram of a temperature difference measuring device according to an embodiment of the present invention, in which 1 is a tank for storing LNG, 2 is an LNG liquid part stored in tank 1, and 3 is a tank for storing LNG. This is a gas layer filled with gas vaporized from the LNG liquid part 2. Sensors 4A to 4N are installed at equal intervals from the bottom to the ceiling inside the tank 1, and are used to measure the temperature of the LNG liquid. 5 is a float floating on the LNG liquid surface, and there are LNG liquid part 2 and gas layer 3.
The number of sensors 6A to 6N that measure the temperature at the boundary surfaces of the two sensors 4A to 4N are provided in a number corresponding to the number of sensors 4A to 4N. 7
is a processing device consisting of a scanner, an amplifier, and an A/D converter. Figure 2 shows the inside of the processing device 7 and the sensors 6A to 6N.
In this figure, 8 is a constant current source, 9 is a scanner having capacitors 10A to 10N and 11A to 11N, 12 is an amplifier, and 13 is an A/D converter. With the above configuration, the temperature at the interface between the LNG liquid part 2 and the gas layer part 3 is not affected by the external temperature, and the LNG temperature remains constant once the LNG components and the pressure in the gas layer are determined.
It can be considered as a kind of reference temperature. Sensors 6A to 6 for measuring this reference temperature
N and the sensors 4A to 4N installed at equal intervals in the tank 1 form a current loop that receives current from the constant current source 8. Therefore, the low resistance values of the RTDs of sensors 4A to 4N and 6A to 6N change depending on their respective temperatures, and when current flows through these sensors, a voltage drop corresponding to their respective resistance values is generated. . This voltage is led to the scanner 9 via a cable, and the charge is stored in a capacitor.
When a sampling command is issued, the scanner capacitor is separated from the sensor side and connected to the amplifier side. The scanner capacitor is charged to the same voltage as the sensor voltage and connected to the amplifier, so the moment a sampling command is issued, it is as if the amplifier were directly connected to the sensor. Such a method is generally called a flying capacitor method. In this case, the capacitors of the scanner 9 are 10A and 11A, 10B and 11B, . . . 10N and 11N, which form pairs, and are sequentially switched from the sensor side to the amplifier side one pair at a time in response to a sampling command. As a result, sensors 6A to 6N and sensors 4A to 4N
Each voltage is reverse biased and read, and a temperature difference voltage between each reference temperature and the LNG liquid temperature is output to the amplifier 12. For example, regarding the voltages of the sensors 6A and 4A, when the capacitor 10A is connected to the sensor side, the upper side thereof is charged to a negative polarity, and the lower side thereof is charged to a positive polarity. On the other hand, the capacitor 11A is charged with positive polarity on the upper side and negative polarity on the lower side. Next, when the capacitors 10A and 11A are connected to the amplifier side in accordance with the sampling command, the lower side of the capacitor 10A and the upper side of the capacitor 11A are connected, and the upper side of the capacitor 10A and the lower side of the capacitor 11A are connected to the input terminal of the amplifier 12. Ru. As a result, the amplifier 12 has the voltage E A of the sensor 6A and the voltage E B of the sensor 4A = E A +
The temperature difference voltage ΔE = E B − E A is input. This temperature difference voltage ΔE is a value that is 0V if the temperatures of sensors 6A to 6N and sensors 4A to 4N are the same.Even if there is a slight temperature difference, if you increase the gain of the amplifier 12, the temperature difference will be reduced. can be enlarged and read. This makes it possible to measure temperature with higher precision than in the past. That is, as before
If the sensor output voltage in the LNG liquid is directly input to the amplifier and processed by the A/D converter, the LNG liquid temperature is -160°C, which is quite far from 0°C, as mentioned above. Naturally, the resolution will be lower. On the other hand, if processing is performed using the temperature difference voltage ΔE as in this embodiment, the resolution will be extremely high, allowing highly accurate temperature measurement. Also, regarding the current fluctuation of the constant current source 8, for example, if the fluctuation rate is α, when processing at absolute temperature, E B × α,
Since E B ≫ΔE, the fluctuation becomes large, but when processing with a temperature difference, the influence can be suppressed to a small level. Similarly, the influence of gain fluctuations in the amplifier system and variations in the A/D converter can be reduced compared to processing using absolute temperature. In this way, each sensor 6A-6N and 4A-4
After taking out the temperature difference voltage ΔE of N, amplifying it with the amplifier 12, and digitizing it with the A/D converter 13, the difference between each temperature difference voltage ΔE is taken out, and the tank is stirred according to the temperature difference between the sensors. By automatically performing this, tank rollover can be prevented. Alternatively, the inside of the tank may be stirred by directly displaying and monitoring each temperature difference voltage ΔE. At this time, if you want to know the absolute temperature as well as the temperature difference voltage ΔE, you can easily do this by attaching one additional sensor to the float 5 and adding this sensor output to each temperature difference voltage ΔE in the processing device 7. can be obtained. Alternatively, the signals may be taken out directly from each sensor 4A to 4N to the amplifier 12 as in the conventional case. In the above embodiment, the reference temperature and the liquid temperature to be measured are connected to the capacitor 1 from the sensors 6A to 6N and 4A to 4N.
0A to 10N and 11A to 11N, and sampled pair by pair in order to extract each temperature difference voltage ΔE. However, as shown in Fig. 3, only one 6A sensor was used for reference temperature measurement, and sensor 6A Even if the generated voltage is charged to the capacitors 10A to 10N, the same effects as in the above embodiment can be obtained. [Effects of the Invention] As described above, according to the present invention, it is possible to measure the temperature difference inside an LNG storage tank with high resolution and high precision, and as a result, it is possible to measure the temperature difference inside an LNG storage tank with high resolution and precision, which previously was dependent on the careful attention of the LNG storage tank monitor. Monitoring of LNG storage tanks, which had previously been monitored, can now be performed based on accurate data, reducing the burden on monitors and enabling safe management of LNG storage tanks.
第1図は本発明の一実施例を示すLNG貯蔵タ
ンクの温度差計測装置の構成図、第2図は第1図
の電気回路図、第3図は本発明の他の実施例を示
す温度差計測装置の電気回路図である。
1……タンク、2……LNG液部、3……気層
部、4A〜4N,6A〜6N……センサ、5……
フロート、7……処理装置、8……定電流源、9
……スキヤナ、10A〜10N,11A〜11N
……コンデンサ、12……アンプ、13……A/
D変換器。
Fig. 1 is a configuration diagram of a temperature difference measuring device for an LNG storage tank showing one embodiment of the present invention, Fig. 2 is an electric circuit diagram of Fig. 1, and Fig. 3 is a temperature diagram showing another embodiment of the present invention. FIG. 3 is an electrical circuit diagram of the difference measuring device. 1...tank, 2...LNG liquid part, 3...gas layer part, 4A~4N, 6A~6N...sensor, 5...
Float, 7... Processing device, 8... Constant current source, 9
...Sukiyana, 10A~10N, 11A~11N
...Capacitor, 12...Amplifier, 13...A/
D converter.
Claims (1)
定間隔で取り付けられた複数の抵抗測温体と、タ
ンク内液面に浮かぶフロートに取り付けられた基
準抵抗測温体と、前記複数の抵抗測温体と基準抵
抗測温体を定電流源に直列に接続して成る回路
と、前記複数の抵抗測温体に発生する電圧を保持
する複数のコンデンサおよびこの複数のコンデン
サに対応して設けられ、前記基準抵抗測温体に発
生する電圧を保持する複数の基準コンデンサを有
し、前記複数のコンデンサおよび前記複数の基準
コンデンサをそれぞれ対として順次走査し、それ
らの差電圧を順次取り出すスキヤナと、このスキ
ヤナから出力される前記各差電圧を増幅する増幅
器と、この増幅器の出力をデイジタル化するA/
D変換器とを備えて成ることを特徴とするLNG
貯蔵タンクの温度差計測装置。 2 特許請求の範囲第1項記載において、前記基
準抵抗測温体は前記複数の抵抗測温体に対応する
数だけ存在し、前記複数のコンデンサへの保持電
圧を発生することを特徴とするLNG貯蔵タンク
の温度差計測装置。[Claims] 1. A plurality of resistance temperature sensors installed at predetermined intervals from the bottom to the ceiling inside the LNG storage tank, a reference resistance temperature measurement object installed on a float floating on the liquid level in the tank, and the Compatible with a circuit consisting of multiple resistance temperature detectors and a reference resistance temperature detector connected in series with a constant current source, multiple capacitors that hold the voltage generated in the multiple resistance temperature detectors, and these multiple capacitors. and a plurality of reference capacitors for holding the voltage generated in the reference resistance temperature sensing element, the plurality of capacitors and the plurality of reference capacitors are each sequentially scanned as a pair, and the difference voltage between them is sequentially scanned. A scanner to take out the data, an amplifier to amplify the difference voltages outputted from the scanner, and an A/D converter to digitize the output of the amplifier.
LNG characterized by comprising a D converter.
Storage tank temperature difference measuring device. 2. The LNG according to claim 1, wherein the reference resistance temperature sensing elements are present in a number corresponding to the plurality of resistance temperature sensing elements, and generate a holding voltage to the plurality of capacitors. Storage tank temperature difference measuring device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13511682A JPS5926025A (en) | 1982-08-04 | 1982-08-04 | Temperature difference measuring device of lng storage tank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13511682A JPS5926025A (en) | 1982-08-04 | 1982-08-04 | Temperature difference measuring device of lng storage tank |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5926025A JPS5926025A (en) | 1984-02-10 |
| JPH0259416B2 true JPH0259416B2 (en) | 1990-12-12 |
Family
ID=15144196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13511682A Granted JPS5926025A (en) | 1982-08-04 | 1982-08-04 | Temperature difference measuring device of lng storage tank |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5926025A (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2729221A1 (en) * | 1995-01-05 | 1996-07-12 | Savourey Gustave | Multi-sensor probe for measuring temp. gradients, esp. in biological materials |
| US6293699B1 (en) * | 1998-10-26 | 2001-09-25 | Merck & Co., Inc. | Method of continuously monitoring controlled temperature units |
| AU2003241519A1 (en) * | 2002-05-21 | 2003-12-12 | Acrolon Technologies, Inc. | System and method for temperature sensing and monitoring |
| US7470060B1 (en) * | 2006-06-23 | 2008-12-30 | Innovative Measurement Methods, Inc. | Detection apparatus for measuring fluid in a vessel |
| CN103644454B (en) * | 2013-11-29 | 2016-08-24 | 中国海洋石油总公司 | LNG tank liquid anti-rolling location fills and EGR |
-
1982
- 1982-08-04 JP JP13511682A patent/JPS5926025A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5926025A (en) | 1984-02-10 |
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