专利摘要:
A capacitance transducer has a central chamber with a conductive diaphragm disposed therein to separate the chamber into at least two portions, at least one portion having an electrical conductor disposed thereon to form in combination with the diaphragm at least one variable sensor capacitor, and wherein at least one portion of the chamber is coupled by a passageway to communicate with an isolator having an isolator chamber and an isolator diaphragm which in combination with the conductive diaphragm enclose a substantially incompressible fluid such that when pressure is applied to an exposed side of the isolation diaphragm, the conductive diaphragm is urged to deflect and thus change the sensor capacitance. Configuration of the isolators, spaced from the sensor capacitors, and other factors disclosed herein, eliminate unwanted mechanical and thermal stresses thereby improving the capacitive sensors' response to pressure.
公开号:SU1421266A3
申请号:SU823453803
申请日:1982-06-04
公开日:1988-08-30
发明作者:Леонард Фрик Роджер
申请人:Роузмаунт Инк (Фирма);
IPC主号:
专利说明:

6t / JO S3 SI
The invention relates to a design of insulating devices and nodes for installing diaphragms of capacitive pressure sensors.
The aim of the invention is to improve the accuracy.
FIG. 1 shows the pressure sensor, section; in fig. 2 - the case of the sensitive element of the pressure sensor: ШШ, section; in fig. 3 is a graph of the results of sensor tests, on which the magnitude of the error (in tenths of a percent) is shown depending on the pressure drop for five different calibrations, with an overpressure of 0–200 psi. inch, or 0-140, 62 kg / cm; in fig. 4 — Plot of output deviation versus line pressure and temperature; in fig. 5 is a diagram of a sensitive element in the absence of static pressure; in fig. 6 is a diagram of the deformation of the sensitive element in the presence of static pressure in the line.
The sensor comprises a support frame 1 serving as a support for the housing 2 of the sensing element and two separation nodes 3 and 4. The separation nodes 3 and 4 can be embedded in the housing or located at a distance from it. Arrows 5 and 6 designate the pressure at the sensor inlets, Diaphragm 7 and 8 of the separation nodes are flexible (in the left) with corrugations 9. Chambers 10 and 11 are formed by membranes 7 and 8 of the separation node 3 and 4 and are connected by pipelines 12 and 13, made For example, from rust-resistant steel.
The case 2 of the sensing element is made of stainless steel, for example, austenitic steel of grade 304. Case 2 is formed of two identical parts 14 and 15, which are distorted by the sensitive membrane 16, the edges of which are clamped. The membrane 16 may be deformed under the influence of a pressure differential, and during assembly, it is preliminarily subjected to a certain radial tension. In the part of the housing 14, a central conical cavity 17 with bores 18 and 19 is formed, and in the part of the housing 15 a similar central conical cavity 20 with bores 21 and 22 is formed. In parts of the housing 14 and 15 there are pipelines 23 and 24 communicated with pipelines 12 and 13 respectively. The internal cavities of the pipelines 23 and 24 are continuations of the cavities of pipelines 12 and 13 and are connected to the chamber 25 formed in part 14 by the diaphragm 16 and the insulating insert 26, and to the chamber 27 formed in part 15 by the membrane 16 and insulating insert 28, respectively . Through the opening 18 into the chamber 17 introduced the electrical conductor 29, and through the opening 21 into the chamber 20 - the same electrical conductor 30. The conductors 29 and 30 can be made in the form of metal tubes, ensuring the filling of sensitive chambers with an incompressible fluid.
Electrically conductive body sections. 2 are insulated from metallic pipes 12 and 13 and from conductors 29 and 30. Insulating non-porous material of inserts 26 and 28, for example glass, ceramics, fills cavities 17 and 20, spreads 18 and 21, and is fixed to the surfaces of body parts 14 and 15, forming an angle of 9 with respect to the plane of the membrane. The central parts of the insulating inserts 26 and 28, the central zones of the parts of the body 14 and 15, as well as the inner ends of the conductors 29 and 30 are machined and form a concave working surface for the sensitive membrane 16 when it is deflected by the increased pressure differential. - on the isolating diaphragm. Pipelines 23 and 24 can be made in the form of a single cylinder or a variety of small shishndry to create support for the membrane 16 under the condition of increased pressure on it.
Corresponding electrically conductive material 31 and 3.2 are deposited on the inner surface of the insulating inserts 26 and 28, forming electrodes facing the chunkswitch membrane 16 and connected to conductors 29 and 30. The sensitive membrane 16 is made of electrically conductive material and fixed between the parts bodies 14 and 15 and layers 31 and 32 with a continuous weld seam 33, so that it forms a capacitor with eMivO-st C, and C with each of these layers, respectively. The lead is connected to housing 2, which is 14
It has the same potential as membrane 16. Membrane 16 can also be made of non-conductive material and have a conductive section that will be a common plate for a sensitive capacitor, and the conductor should then be connected to this section. Bolts 34 are provided to absorb the forces generated by the pressure on the body 2.
On either side of the membrane 16 into the chamber formed by part of the housing 14 and the diaphragm 16, and insulating chamber 10, as well as into the chamber formed by part of the housing 15 and membrane 16, and into the insulating chamber 11 through the conductors 29 and 30 pour incompressible fluid, for example silicone oil. When these cavities are filled, the ends of the conductors 29 and 30 are cut off and the corresponding electrical wires are connected to them.
The location of the separation membranes 7 and 8 at a distance from the sensitive membrane 16 is conventionally shown, since the location of these membranes is not so important provided that they are arranged so that they are not exposed to unwanted mechanical loads other than the pressure of incompressible fluid on the body of the sensitive element 2. The element 2 is preferably fixed to the support frame 1 fixedly, it need not be fixed rigidly, for example by welding. As shown in FIG. 1, it is held by elastic bands 35, made of electrically non-conductive material, hands isolating the body 2 of the sensing element from the frame 1 and supporting the body 2.
The embodiment of the sensor is shown in FIG. 2. Identical elements are indicated in FIG. 2 with the same numbers as in FIG. 1, but with the addition of the letter a. Here, the sensor body 2a is somewhat wider than in the device shown in FIG. 1, and bores 19a and 22a are somewhat deeper, than bores 19 and 22, and partially filled with material 26a and 28a, forming insulating inserts. Angle b is the angle between the membrane in its average height and distance.
five
0
266
A chested surface forming a cavity in the corresponding part of the body, filled with material 26a and 28a. This angle determines the effective depth of the material 26a, 28a (26, 28 in the first embodiment), which serves as the electrodes of the capacitor 31a and 32a (31 and 32). Although in both embodiments of the device, the angle 0 is approximately 45 °, it was found that the increased stability and, consequently, increased stability. accuracy provide angles in the range of 25. -70. The angle can also be measured with respect to the central axis of the body of the sensing element, which is perpendicular to the plane of the membrane 16a (16), in its middle position.
The sensor works as follows.
When chambers 10 and 11, pipes 12 and 13 (including the holes of the pipe 5 of wires 23 and 24) and the chambers between electrodes 30 and 32 and the membrane 16 are filled with incompressible fluid, the difference between the pressures indicated by arrows 5 and 6 causes the membrane 16. proportional to the differential pressure at these pressures, as a result of which the capacitance formed by these layers and the membrane changes.
One of the advantages of the sensor is the reduction of the effect of static pressure on the pressure range of the sensor.
If the thickness of the insulating material is small, or if the interface of the insulating material — the metal is essentially parallel to the supporting axis of the membrane (perpendicular to the membrane plane), such interfaces (connections) 36 and 37 (Zba and 37a) are subject to shear forces weakening or disrupting communication. If a force is applied to the broken connection, it causes the insulating material to move in the direction away from the membrane. The displacement of the insulating material creates undesirable changes in capacitance that are not the magnitude of the pressure being measured, which leads to an increase in the error caused by static pressure in the line. If the sensor is made according to the invention, then connections 36 and 37 (Zba and 37a) test0
0
five
0
five
15
51421266
Mostly compressive loads are much less susceptible to failure.
When insulators are removed from the side of the sensitive element casing, the space of the capacitor plate on both sides of the membrane 16 increases with increasing static pressure in lines 5 and 6 due to a small external displacement of the portions of the sensing element with respect to the sensitive membrane. This increase in static pressure in the line also causes parts 14 and 15 to twist about their respective neutral axes (in Figs. 2, 3 and 6, these axes are indicated by X-X), while both parts of the body tend to contract near the membrane, as shown by arrows 38 in FIG. 2 and 6 (in Figs. 5 and 6, the insulating material is not marked, configurations are shown on them, as shown in Figs. 1 and 2). Such an imbalance can best be explained by FIG. 5, parts 14 and 15 are shown in the unloaded state, and FIG. 6, which shows the skew state caused by the increase in static pressure in the line. As the static pressure in the line increases, the capacitor space d (Fig. 5) between the membrane 16 and the capacitor plates 31 and 32 increases to size d
ABOUT
CH + CL
Xf
X /
f.
where O is the output signal of the capacitive cell of the differential pressure capacity of the larger of the Cond
CH CL X. On
sator C or C2; the capacitance of the smaller capacitor C, or the deviation of the membrane under the pressure differential capacitor space with zero static growth; the tension of the diaphragm.
20
25
thirty
Simplified formula looks good
About - H.sG,
If the sensor is made to agree with the increase in the static pressure in the line, the condensate space X o increases with the measure XQ, the output value is almost equal, essentially constant, it is possible to detect the deviation of the diaphragms X p depending on the pressure drop applied to it The result value of the output signal O does not depend on the value of static differential F in line.
They were tested by valid workers.
(Fig. 6), however, this increase is not the V 35 load of the sensor, made according to
The invention according to FIG. 1 and 2 but from the cylindrical interface of the metal-insulating mate the interface is first
represents an increase in pressure drop. In accordance with the invention, the increase in capacitance caused by such a bias is largely offset by a decrease in the radial tension of the membrane caused by compression close to it. The radial preload applied to the membrane at the time of manufacture of the sensor, as well as the appropriate selection. sizes and materials provide a decrease in membrane elasticity with increasing static pressure. The preferred material for the membrane is high-strength steel with high elasticity. This compensation takes place at all values of the statistics and does not affect the test results. Otherwise, the device under test was made according to the invention, i.e. Separators: 3 and 4 were separated from the pressure sensing line body 2, however, it is most pronounced at the pressure element, there was a compensation above 500 psig. inch of body curvature 2 sensitive (-vSS kg / cm) of its element and pre-nat The following equation removes static pressure compensation:
membrane 16. The thickness of the membrane 16 was 1.8 mt1l (1 mil
CH + CL
Xf
X /
f.
where O is the output signal of the capacitive cell of the pressure differential; larger capacity of condensn

CL X. On
sator C or C2; the capacitance of the smaller of the capacitors C, or the membrane deflection under the action of pressure drop; condenser space at zero static pressure; the tension of the diaphragm.

Simplified formula looks like this:
About - H.sG,
If the sensor is made according to the invention, by increasing the static pressure in the line, the condenser space X o increases to the size XQ, the product is almost equal, i.e., essentially constant, it is possible to fix the deviation value of the membrane X p depending on the applied pressure drop, as a result, the magnitude of the output signal O will not depend on the magnitude of the static FS in the line.
Were conducted under the influence of actual workers on
sensor loads performed by
The invention according to FIG. 1 and 2, but with a cylindrical interface metal-insulating material, the interface is first
made perpendicular to the membrane 16 (9 is 90), then almost parallel (b is zero). Moreover, the test sensor did not have a pre, folded, starchy bond, but had a known cut link. Improved communication helps to avoid the destruction of the connection, but since it was established that such destruction does not occur, therefore, the type of connection
no effect on test results. Otherwise, the device under test was made according to the invention, i.e. separation units: 3 and 4 were separated from the case 2 of the sensing element, there was compensation for the curvature of the case 2 of the sensitive element and the pre-tension element, there was a compensation for the curvature of the case 2 of the sensitive element and the preload tension of the membrane 16. The thickness of the membrane 16 was la 1.8 mt1l (1 mil 71A212668
25.4 µm), diameter — approximately 1.12 inches (-28.5 mm) was also performed; a preliminary test of 105,000 psi to demonstrate improved tension was not carried out. an inch (7380 kg / cm), although pre-tension values of 50,000 to 200,000 psi can be used. inch (3515-14062 kg / cm), in FIG. 4. The self-propelled membrane was extracted from the material. The action is an error that has Nispan C, the material of the insulating inserts 27 and 28 (27a and 28a) or Owens glass 0120 (Owens) the case of the sensitive element was made of Nispan C material and had 1,250
compensated for the temperature effects in relation to the stability of the output signal of the proposed sensor, the results of which are given
FIG. 4 is a separate countdown. Several such samples were completed, of which FIG. 4 shown
, 0 place before any electrical signal compensation. Electrical signal compensation is usually used to reduce further errors, however, most preferably an inch in diameter (/ - 31.75 mm). A con- tact with a device with a small non-compensatory space X was an equal error. Each curve on the Ho-wO, 0075 inch (0.19 mm) in the center. Insulators 3 and 4 were made of 304SST grade stainless steel, had about 3 inches (76.2 mm) in the bottom — 20–7. The curves show that the proposed configuration provides excellent stability and very low thermal hysteresis, since the capacitance deviation for 25 three samples at 100 F was less than 18%. Thermal hysteresis is related to 1e to the difference in the results of readings at a given temperature, depending on whether
meter and were connected to chambers 25 and 27 by means of pipelines 12 and 13 of stainless steel tube with an outer diameter of 1/16 inch (1.46 mm).
The test results are shown in FIG. 3
As can be seen from the graph, all deviations of the test points under the influence of the static pressure in the linley ZO of this reading from the higher or not exceeded 0.2% in the range of the differential temperature.
 A test was also carried out to demonstrate the improved FIG. 4. Its erroneous effect is an error, having
compensated for the temperature effects in relation to the stability of the output signal of the proposed sensor, the results of which are given
FIG. 4 is a separate countdown. Several such samples were completed, of which FIG. 4 shown
place before any electrical signal compensation. Electrical signal compensation is usually used to reduce further errors, however, it is most preferable to have a device with a small uncompensated error. Each curve for seven. The curves show that the proposed configuration provides excellent stability and very low thermal hysteresis, since the deviation of the capacitance value for three readings at 100 F was less than 18%. Thermal hysteresis is related to 1e to the difference in the results of readings at a given temperature, depending on whether
and pressures from 0 to 240 inches of water (0-609 cm), in the static pressure range from 0 to 2,000 psi. inch (0-140 kg / cm). Curves in FIG. 3 have a very small mechanical hysteresis. Such a mechanical hysteresis is not unusual and depends not only on the instantaneous value of the load caused by the pressure drop and the static pressure in the line, but also on the preliminary value of such a load. An advantage of the invention is that the zero stability margin of the sensor, which varies with temperature and static pressure, is improved due to the fact that the insulator casing does not have direct contact with the casing of the sensing element. Only tubes forming pipelines 12 and 13 are in direct contact with the body of the sensing element, but these tubes can absorb the loads on the insulators and their changes due to the temperature change without transferring these forces to the body 2 of the sensing element.
Many samples made of various materials and having different sizes were successfully tested, while in the experiments we used membranes made of Havar steel from Hamilton Indrastriz (Hamilton Industries) or Elgiloy Co. alloy. The material of insulating inserts 26 and 28 was made of alkaline lead glass, namely Corning 1990 glass, and the body of the sensitive element was made of austenitic stainless steel.
In addition, the advantage of this invention is that since the membranes 7 and 8 of the separation nodes 3 and 4, respectively, do not form part of the body of the sensing element, their size may be larger than the size of this body. Such an increase in size can be very important in reducing the effect of temperature and other factors on the operation of the sensor.
Since the body 2 of the sensing element is isolated from the support frame
1, the sensor circuit is simplified when electrical insulation is required, which occurs quite often in industrial pressure measurements.
invention formula
权利要求:
Claims (2)
[1]
1. A capacitive pressure sensor, comprising a sensor case, having a central chamber divided by an electrically conductive membrane into two cavities, in each of which an insulating insert is made with a feed channel in the center and a buried working surface equipped with an electrode facing membranes, and two separating nodes; with separating membranes, the cavities of the nodes and the sensing element being filled with a liquid, characterized in that
1421266 About
 It is equipped with a support with a hole inside which the core of the sensitive element is fixed, and the sub g membrane cavity of each separation unit is connected to the corresponding inlet channel of the insulation insert with the help of a pipeline inserted into the sensor, each 10 insulation insert Compressed in the shape of a truncated cone with an angle of 25-27 between the generator of the cone and the plane of the membrane.
[2]
2. The sensor according to claim 1, characterized in that c. There, two separation units are spaced apart from the body of the sensing element and attached to the frame, while the body of the sensitive element is fixed inside the frame by means of non-conductive supports.
G1
Fi.2.
tf%
fo
50
too
a / f.J
110 ifo
about tfSI6 fWOPlIf
a MoPSJf ieooKie d leaafsif
rOO 150 Fi.
Zoo
250
Ifi
38
fff
类似技术:
公开号 | 公开日 | 专利标题
SU1421266A3|1988-08-30|Capacitance pressure transducer
US4364276A|1982-12-21|Differential pressure measuring transducer assembly
US4424713A|1984-01-10|Silicon diaphragm capacitive pressure transducer
US3618390A|1971-11-09|Differential pressure transducer
EP0041886B1|1984-10-17|Capacitive pressure transducer
US4507973A|1985-04-02|Housing for capacitive pressure sensor
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US5134887A|1992-08-04|Pressure sensors
US5165281A|1992-11-24|High pressure capacitive transducer
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US4531415A|1985-07-30|Differential pressure transducer
GB1581903A|1980-12-31|Capacitor transducer
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CA1057969A|1979-07-10|Differential pressure sensor
US4072057A|1978-02-07|Differential pressure cell with diaphragm tension and overpressure protection
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US3035240A|1962-05-15|Beam-diaphragm pressure load cell improvements
US4741214A|1988-05-03|Capacitive transducer with static compensation
KR900001465B1|1990-03-12|Capacitive pressure transducer with isolated sensing diapharm
US5349491A|1994-09-20|Pre-stressed pressure transducer and method of forming same
JP2546013B2|1996-10-23|Capacitive differential pressure detector
同族专利:
公开号 | 公开日
GB2099587A|1982-12-08|
IT8149423D0|1981-10-05|
YU41525B|1987-08-31|
YU238981A|1983-12-31|
JPS57501494A|1982-08-19|
GB2099587B|1984-11-07|
HK89885A|1985-11-22|
AU7720381A|1982-04-28|
MX154961A|1988-01-14|
ZA816837B|1982-09-29|
CA1164240A|1984-03-27|
FI72809C|1987-07-10|
EP0061488B1|1986-12-17|
IT1193784B|1988-08-24|
FI821976A0|1982-06-03|
AU551166B2|1986-04-17|
IL64028A|1987-12-20|
HU190799B|1986-11-28|
US4370890A|1983-02-01|
EP0061488A1|1982-10-06|
IN154802B|1984-12-15|
EP0061488A4|1983-10-04|
FI72809B|1987-03-31|
JPH046889B2|1992-02-07|
BR8108830A|1982-08-24|
WO1982001250A1|1982-04-15|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题

FR1582509A|1968-05-17|1969-10-03|
US3618390A|1969-10-27|1971-11-09|Rosemount Eng Co Ltd|Differential pressure transducer|
DE2230264A1|1972-06-21|1974-01-31|Union Rheinische Braunkohlen|PROCESS FOR THE PRODUCTION OF AROMATIC OR HYDROAROMATIC HYDROPEROXIDES|
US3793885A|1972-09-05|1974-02-26|Rosemount Inc|Diaphrgam construction for differential pressure transducer|
JPS5617720B2|1972-12-25|1981-04-23|
US3869920A|1973-04-13|1975-03-11|Yokogawa Electric Works Ltd|Symmetrically arranged, deflection type differential pressure transmitters for controlling industrial systems and processes|
US3808480A|1973-04-16|1974-04-30|Bunker Ramo|Capacitive pressure transducer|
SU506223A1|1973-06-18|1982-09-30|Государственный научно-исследовательский институт теплоэнергетического приборостроения|Membrane unit|
SU506224A1|1973-06-18|1982-09-30|Государственный научно-исследовательский институт теплоэнергетического приборостроения|Pressure differential transducer|
US3926055A|1973-10-01|1975-12-16|Itt|Mechanical span and zero adjustment apparatus for pressure transducers|
JPS5232368Y2|1973-10-30|1977-07-23|
US3999435A|1975-04-24|1976-12-28|Fischer & Porter Co.|Differential pressure transmitter|
US4111056A|1975-06-30|1978-09-05|Michael Mastromatteo|Control devices|
JPS5232368U|1975-08-29|1977-03-07|
JPS562890B2|1975-09-09|1981-01-22|
US3994166A|1975-11-10|1976-11-30|Warren Automatic Tool Co.|Apparatus for eliminating differential pressure surges|
US4072058A|1976-05-03|1978-02-07|Honeywell Inc.|Differential pressure transmitter with pressure sensor protection|
CA1077294A|1976-05-03|1980-05-13|Honeywell Inc.|Pressure transmitter with simplified pressure sensing head|
JPS5829862B2|1977-05-14|1983-06-25|Fuji Electric Co Ltd|
JPS5831855B2|1977-06-22|1983-07-08|Fuji Electric Co Ltd|
DE2824489C2|1978-06-03|1982-06-16|Reifen-Ihle GmbH, 8870 Günzburg|Pipe connector for crossing pipes|
DE2827274C2|1978-06-21|1988-08-04|Fuji Electric Co., Ltd., Kawasaki, Kanagawa, Jp|
US4218925A|1979-06-27|1980-08-26|Honeywell Inc.|Differential pressure transmitter with pressure sensor protection|
US4285244A|1980-02-13|1981-08-25|Honeywell Inc.|Non-symmetrical overload protection device for differential pressure transmitter|DE3213320A1|1982-04-06|1983-10-13|Siemens AG, 1000 Berlin und 8000 München|PRESSURE OR PRESSURE DIFFERENTIAL TRANSMITTER|
US4425799A|1982-06-03|1984-01-17|Kavlico Corporation|Liquid capacitance pressure transducer technique|
US4539998A|1983-04-29|1985-09-10|American Hospital Supply Corporation|Pressure transducer assembly|
USRE33518E|1983-04-29|1991-01-15|Baxter International, Inc.|Pressure transducer assembly|
US4502003A|1983-07-29|1985-02-26|Rosemount Inc.|Two wire circuit having an adjustable span|
US4612812A|1985-08-15|1986-09-23|Rosemount Inc.|Stress reducing stop for unstretched pressure sensing diaphragm|
JPH043244Y2|1985-11-29|1992-02-03|
IL82194A|1986-04-23|1992-03-29|Rosemount Inc|Measurement circuit|
US5083091A|1986-04-23|1992-01-21|Rosemount, Inc.|Charged balanced feedback measurement circuit|
US4791352A|1986-07-17|1988-12-13|Rosemount Inc.|Transmitter with vernier measurement|
US4745810A|1986-09-15|1988-05-24|Rosemount Inc.|Flangeless transmitter coupling to a flange adapter union|
US4798089A|1987-03-12|1989-01-17|Rosemount Inc.|Isolator apparatus|
US4760859A|1987-05-18|1988-08-02|Rosemount Inc.|Modular pressure instrument|
US4833922A|1987-06-01|1989-05-30|Rosemount Inc.|Modular transmitter|
US4818994A|1987-10-22|1989-04-04|Rosemount Inc.|Transmitter with internal serial bus|
US5062302A|1988-04-29|1991-11-05|Schlumberger Industries, Inc.|Laminated semiconductor sensor with overpressure protection|
JP2639159B2|1989-04-14|1997-08-06|富士電機株式会社|Capacitive differential pressure detector|
US4949581A|1989-06-15|1990-08-21|Rosemount Inc.|Extended measurement capability transmitter having shared overpressure protection means|
US5022270A|1989-06-15|1991-06-11|Rosemount Inc.|Extended measurement capability transmitter having shared overpressure protection means|
US4970898A|1989-09-20|1990-11-20|Rosemount Inc.|Pressure transmitter with flame isolating plug|
US5134887A|1989-09-22|1992-08-04|Bell Robert L|Pressure sensors|
DE3933512C2|1989-10-06|1993-02-18|Endress U. Hauser Gmbh U. Co, 7864 Maulburg, De|
US5163326A|1991-03-08|1992-11-17|Rosemount Inc.|Line pressure compensator for a pressure transducer|
US5230248A|1991-07-12|1993-07-27|Rosemount Inc.|Corrosion resistant isolator|
US5184514A|1991-07-12|1993-02-09|Rosemount Inc.|Corrosion resistant isolator|
US5237285A|1991-10-18|1993-08-17|Rosemount Inc.|Method and apparatus for capacitance temperature compensation and manufacturability in a dual plate capacitive pressure transmitter|
US5271277A|1991-12-23|1993-12-21|The Boc Group, Inc.|Capacitance pressure transducer|
US5329818A|1992-05-28|1994-07-19|Rosemount Inc.|Correction of a pressure indication in a pressure transducer due to variations of an environmental condition|
US5596147A|1995-11-17|1997-01-21|Wilda; Douglas W.|Coplanar pressure sensor mounting for remote sensor|
US5757608A|1996-01-25|1998-05-26|Alliedsignal Inc.|Compensated pressure transducer|
US5741975A|1996-07-31|1998-04-21|Motorola, Inc.|Media isolated differential pressure sensor and fluid injection method|
US6047244A|1997-12-05|2000-04-04|Rosemount Inc.|Multiple range transition method and apparatus for process control sensors|
US6038961A|1998-03-02|2000-03-21|Rosemount Inc.|Flush mount remote seal|
US6295875B1|1999-05-14|2001-10-02|Rosemount Inc.|Process pressure measurement devices with improved error compensation|
US6328647B1|2000-04-06|2001-12-11|Jon E. Traudt|Pressure differential detecting system, and method of use|
DE10050300A1|2000-10-10|2002-04-11|Endress Hauser Gmbh Co|pressure measuring cell|
US6516672B2|2001-05-21|2003-02-11|Rosemount Inc.|Sigma-delta analog to digital converter for capacitive pressure sensor and process transmitter|
FR2830612B1|2001-10-10|2004-01-23|Bosch Gmbh Robert|RACE SENSOR, PNEUMATIC SERVOMOTOR INCLUDING THE SAME, AND BRAKING SYSTEM COMPRISING SUCH A SERVOMOTOR|
DE10152681A1|2001-10-19|2003-04-30|Endress & Hauser Gmbh & Co Kg|Diaphragm seal with separating membrane and process for its manufacture|
JP4163880B2|2002-03-05|2008-10-08|長野計器株式会社|Differential pressure detector, flow meter and liquid level meter equipped with the differential pressure detector|
US6839546B2|2002-04-22|2005-01-04|Rosemount Inc.|Process transmitter with wireless communication link|
US6843133B2|2002-06-18|2005-01-18|Rosemount, Inc.|Capacitive pressure transmitter|
DE10229703A1|2002-07-02|2004-01-15|Endress + Hauser Gmbh + Co. Kg|Capacitive pressure sensor|
DE102004006383A1|2004-02-09|2005-08-25|Endress + Hauser Gmbh + Co. Kg|Differential pressure sensor with overload diaphragm|
US9184364B2|2005-03-02|2015-11-10|Rosemount Inc.|Pipeline thermoelectric generator assembly|
JP5058785B2|2004-03-02|2012-10-24|ローズマウントインコーポレイテッド|Process equipment with improved power generation|
DE102004017580A1|2004-04-07|2005-12-01|Endress + Hauser Gmbh + Co. Kg|Differential pressure sensor with dynamic overload protection|
US8145180B2|2004-05-21|2012-03-27|Rosemount Inc.|Power generation for process devices|
US8538560B2|2004-04-29|2013-09-17|Rosemount Inc.|Wireless power and communication unit for process field devices|
US7262693B2|2004-06-28|2007-08-28|Rosemount Inc.|Process field device with radio frequency communication|
US8160535B2|2004-06-28|2012-04-17|Rosemount Inc.|RF adapter for field device|
US7213464B1|2004-10-25|2007-05-08|Traudt Jon E|System for visually monitoring pressure in an enclosed space|
US7680460B2|2005-01-03|2010-03-16|Rosemount Inc.|Wireless process field device diagnostics|
US7334484B2|2005-05-27|2008-02-26|Rosemount Inc.|Line pressure measurement using differential pressure sensor|
CA2602758C|2005-06-27|2016-03-15|Rosemount Inc.|Field device with dynamically adjustable power consumption radio frequency communication|
US7379792B2|2005-09-29|2008-05-27|Rosemount Inc.|Pressure transmitter with acoustic pressure sensor|
US7415886B2|2005-12-20|2008-08-26|Rosemount Inc.|Pressure sensor with deflectable diaphragm|
US7308830B2|2006-01-26|2007-12-18|Rosemount Inc.|Pressure sensor fault detection|
US7913566B2|2006-05-23|2011-03-29|Rosemount Inc.|Industrial process device utilizing magnetic induction|
US8188359B2|2006-09-28|2012-05-29|Rosemount Inc.|Thermoelectric generator assembly for field process devices|
ITMI20070191A1|2007-02-05|2008-08-06|Abb Service Srl|PRESSURE TRANSMITTER FOR DETECTION OF A VARIABLE RELATED TO A PROCESS FLUID.|
US8898036B2|2007-08-06|2014-11-25|Rosemount Inc.|Process variable transmitter with acceleration sensor|
US7624642B2|2007-09-20|2009-12-01|Rosemount Inc.|Differential pressure sensor isolation in a process fluid pressure transmitter|
US7484416B1|2007-10-15|2009-02-03|Rosemount Inc.|Process control transmitter with vibration sensor|
US7578194B1|2008-02-11|2009-08-25|Sensata Technologies, Inc.|Differential fluid pressure measurement apparatus|
US8191424B2|2008-02-14|2012-06-05|Kulite Semiconductor Products, Inc.|Low differential pressure transducer|
US7743662B2|2008-02-14|2010-06-29|Kulite Semiconductor Products, Inc.|Low differential pressure transducer|
US8250924B2|2008-04-22|2012-08-28|Rosemount Inc.|Industrial process device utilizing piezoelectric transducer|
US8847571B2|2008-06-17|2014-09-30|Rosemount Inc.|RF adapter for field device with variable voltage drop|
US9674976B2|2009-06-16|2017-06-06|Rosemount Inc.|Wireless process communication adapter with improved encapsulation|
US8929948B2|2008-06-17|2015-01-06|Rosemount Inc.|Wireless communication adapter for field devices|
US8694060B2|2008-06-17|2014-04-08|Rosemount Inc.|Form factor and electromagnetic interference protection for process device wireless adapters|
US8626087B2|2009-06-16|2014-01-07|Rosemount Inc.|Wire harness for field devices used in a hazardous locations|
CN102084307B|2008-06-17|2014-10-29|罗斯蒙特公司|RF adapter for field device with low voltage intrinsic safety clamping|
EP2294765B1|2008-06-17|2017-01-18|Rosemount Inc.|Rf adapter for field device with loop current bypass|
US7977924B2|2008-11-03|2011-07-12|Rosemount Inc.|Industrial process power scavenging device and method of deriving process device power from an industrial process|
US7870791B2|2008-12-03|2011-01-18|Rosemount Inc.|Method and apparatus for pressure measurement using quartz crystal|
US7954383B2|2008-12-03|2011-06-07|Rosemount Inc.|Method and apparatus for pressure measurement using fill tube|
US8327713B2|2008-12-03|2012-12-11|Rosemount Inc.|Method and apparatus for pressure measurement using magnetic property|
US8371175B2|2009-10-01|2013-02-12|Rosemount Inc.|Pressure transmitter with pressure sensor mount|
US8429978B2|2010-03-30|2013-04-30|Rosemount Inc.|Resonant frequency based pressure sensor|
US8234927B2|2010-06-08|2012-08-07|Rosemount Inc.|Differential pressure sensor with line pressure measurement|
US8132464B2|2010-07-12|2012-03-13|Rosemount Inc.|Differential pressure transmitter with complimentary dual absolute pressure sensors|
US10761524B2|2010-08-12|2020-09-01|Rosemount Inc.|Wireless adapter with process diagnostics|
US8384915B2|2010-10-01|2013-02-26|Rosemount Inc.|Test block for use in a welding process|
US9310794B2|2011-10-27|2016-04-12|Rosemount Inc.|Power supply for industrial process field device|
DE102012103585A1|2012-04-24|2013-10-24|Endress + Hauser Gmbh + Co. Kg|pressure transducers|
US8752433B2|2012-06-19|2014-06-17|Rosemount Inc.|Differential pressure transmitter with pressure sensor|
US9048901B2|2013-03-15|2015-06-02|Rosemount Inc.|Wireless interface within transmitter|
RU2545085C1|2013-11-12|2015-03-27|Закрытое акционерное общество Промышленная группа "Метран"|Design of biplanar capacitance sensor of pressure difference|
US9316553B2|2014-03-26|2016-04-19|Rosemount Inc.|Span line pressure effect compensation for diaphragm pressure sensor|
US9857259B2|2014-09-30|2018-01-02|Rosemount Inc.|Differential pressure sensor with high pressure capabilities|
DE102015117222A1|2014-10-10|2016-04-14|Steering Solutions Ip Holding Corporation|Dual-channel pressure sensor with a single connection opening|
DE102014119407A1|2014-12-22|2016-06-23|Endress + Hauser Gmbh + Co. Kg|Differential pressure sensor and differential pressure transducer with such a differential pressure sensor|
US10126193B2|2016-01-19|2018-11-13|Rosemount Aerospace Inc.|Compact or miniature high temperature differential pressure sensor capsule|
CN107976279A|2017-12-15|2018-05-01|北京创昱科技有限公司|A kind of vacuum measuring device|
US11041773B2|2019-03-28|2021-06-22|Rosemount Inc.|Sensor body cell of a pressure sensor|
CN110553763B|2019-09-10|2021-03-19|广州敏华仪器仪表有限公司|Coplanar suspension type full-isolation sensor|
法律状态:
优先权:
申请号 | 申请日 | 专利标题
US06/194,758|US4370890A|1980-10-06|1980-10-06|Capacitive pressure transducer with isolated sensing diaphragm|
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