CA1100212A - Tilt detection-system - Google Patents

Tilt detection-system

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Publication number
CA1100212A
CA1100212A CA299,116A CA299116A CA1100212A CA 1100212 A CA1100212 A CA 1100212A CA 299116 A CA299116 A CA 299116A CA 1100212 A CA1100212 A CA 1100212A
Authority
CA
Canada
Prior art keywords
voltage
magnitude
voltages
impedances
derived
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
Application number
CA299,116A
Other languages
French (fr)
Inventor
Edward L. Ratcliffe
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LEAK "X" DETECTION DEVICES Ltd
Original Assignee
LEAK "X" DETECTION DEVICES Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by LEAK "X" DETECTION DEVICES Ltd filed Critical LEAK "X" DETECTION DEVICES Ltd
Priority to CA299,116A priority Critical patent/CA1100212A/en
Application granted granted Critical
Publication of CA1100212A publication Critical patent/CA1100212A/en
Expired legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D5/00Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable
    • G01D5/12Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means
    • G01D5/14Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means influencing the magnitude of a current or voltage
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C9/00Measuring inclination, e.g. by clinometers, by levels
    • G01C9/02Details
    • G01C9/06Electric or photoelectric indication or reading means

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)

Abstract

ABSTRACT OF THE DISCLOSURE
A system for sensing the deviation of a surface, structure or the like from a reference axis is disclosed. A tilt sensitive transducer is used and this has two impedances the values of which vary differentially according to the angle and direction of tilt of the surface or member to which the transducer is mounted. Two equal but antiphase A.C. voltages are applied, respectively, to the two impedances and the current derived in each impedance is used to generate a D.C. voltage. The two D.C. volt-ages are compared to derive a difference D.C. voltage the magnitude and sign of which are dependent on the angle and direction, respectively, of tilt.

Description

"` 11002~2 The invention relates to systems for sensing deviation of a surface, structure or the like from a reference plane which may be, for example, a horizontal plane.
In such systems it has been known to use a tilt sensitive transducer which has two resistance values which vary according to the angle and direc-tion of tilt. When the transducer is connected in an A.C. bridge circuit - an output signal varying in amplitude and phase according to the angle and direction of tilt can be obtained. See, for example, U.S. patent 3,114,204 which issued April 27, 1960 to Foody et al. In that patent there is no teaching of how the phase of the output signal is actually determined so as to determine the direction of tilt. Moreover, it is noted that the Foody circuit disclosed does not provide a reference voltage in terms of magnitude and phase and this presents a problem in processing the output signal.
According to the present invention, there is provided a system for sensing deviation of a surface, structure or the like from a reference axis comprising a tilt sensitive transducer including a first and a second imped-ance the values of which vary differentially according to the angle and direc-tion of tilt, means for applying an A.C. voltage across the first impedance, means for applying an antiphase A.C. voltage across the second impedance, rectifier means for deriving a positive D.C. voltage having a magnitude depending on the magnitude of the first impedance and deriving a negative D.C. voltage having a magnitude depending on the magnitude of the second impedance, means for adding the positive D~C~ voltage and the negative D~C.
voltage to derive a D.C. voltage the magnitude of which is dependent on the angle of tilt and the sign of which is dependent on the direction of tilt.
Figure 1 is a block diagram of a deflection sensing system of the invention;
Figure 2 is a circuit diagram of a portion of the system shown in Figure l;
Figure 3 is a circuit diagram of an alarm circuit shown in Figure l;

and ~k `-`` 110~212 Figure 4 is a circuit diagram of an alternate A.C. source which can be incorporated in the system of the invention.
The system of claim 1 can be seen to comprise an A.C. source 10 arranged to supply to identical circuit halves each associated with a par-ticular deflection sensing transducer or sensor 11, 11'. Because of the identity between the two circuit halves, essentially only one half will be described in detail, it being understood that the components of the other circuit half (which are given a prime notation in Figure 1) and the operation of the other circuit half are identical to those of the first circuit half.
The sensors 11 and 11' are, for example, each in the form of an arcuate sealed glass tube partially filled with an electrolytic fluid, the remainder of the tube being filled with a gas bubble. A symmetrically spaced arrangement of three electrodes is provided on the inner surface of the tube in contact with the electrolytic fluid so that the resistances between two predetermined pairs of electrodes is dependent on the location of the gas bubble. With the sensor placed on a horizontal plane the bubble will be located centrally and the two resistance values will be identical. Movement of the sensor about a horizontal axis will cause the bubble to move, thus increasing one resis~ance value and decreasing the other. Such a sensor is described in U.S. patent 3,497,950 which issued on March 3, 1970 to Squire et al. Similar sensors but with a slightly different electrode configur-ation are available from Spectron Glass.
The invention is not limited to the use of electrolytic sensors as any other type of deflection sensor which includes two resistances which vary in magnitude and sense according to the extent and direction of tilt may be used. For example, the sensor described in above mentioned U.S.
patent 3,114,209 to Foody et al, would be suitable. This sensor also com-prises an arcuate tube partially filled with a fluid and having a gas bub-ble. In this case, however, the fluid is one such as ethyl alcohol or kero-sene which has good thermal conductivity and is electrically non-conductive ``` 110(~212 and, instead of electrodes, two temperature sensitive resistance elements are used, movement of the bubble causing differential cooling of the resist-ance elements and thus differential resistance values.
The two sensors 11 and 11' are mounted in a suitable protective housing so as to rest on the same plane with the sensors disposed on two mutually perpendicular axes so as to sense deflection along these two axes.
The A.C. source 10 is arranged to provide to each circuit half, and, in particular to the sensor 11 or 11', two anti-phase equal amplitude A~C~
voltages with respect to one common bus. The sensor 11 is connected to one input of a comparator 12, the signal supplied by the sensor 11 being depen-dent in amplitude and phase on the degree and direction of tile of the sensor 11 .
The two antiphase voltages are also supplied to a remote electronic leveling circuit (REL) 13 which is a variable means for deriving a voltage in phase with that produced by the sensor 11 and equal in magnitude to the sensor voltage at a selected inclination of the sensor 11. This is . _ to compensate for situations where it is physically difficult or impossible to position the sensor 11 in a perfectly level plane or where the reference axis is intentionally non-horizontal or where, after an initial deflection, the sensor has to be reset to the new reference axis.
The output of REL 13 is supplied to the other input of the differ-ential amplifier 12 which derives an output signal which varies in magnitude and phase depending on the deviation of the sensor from the reference axis.
As stated above this reference is not necessarily lying in a horizontal plane but, in practice, it will be ver~ close to being horizontal.
The output of amplifier 12 is fed to a programmable alarm 14 arranged to derive an alarm signal when the magnitude of the voltage output of ampli-fier 12 exceeds a programmable predetermined value corresponding to a pre-determined magnitude of deviation from the reference level.
The output of amplifier 12 is also fed to a phase discrimination and ``` llO~Z12 amplitude detection circuit tPDAD) 15 also supplied by the A.C. source 10.
The PDAD circuit 15 converts the output signal from amplifier 12 into a D.C.
voltage the magnitude of which is proportional to the angle of inclination or deviation from the reference and the sense ~ositive or negative) of which is dependent on the direction of inclination of the sensor.
- The output voltage of PDAD 15 is fed to a potentiometer 16 for cali-brating the sensor 11 to a voltmeter display 17. The calibrated voltage may be supplied to a recording or transmitting device and, for this purpose, a buffer circuit 18 is used to provide an isolated auxiliary output 19.
Referring now to Figure 2 which shows the detailed circuitry for - only one sensor, namely sensor 11, the A.C. source 10 comprises a transformer Tl the secondary winding S of which is centre tapped. Identical resistors Rl and R2 are connected to each half Sl and S2 of the winding S and two pairs of zener diodes Dl, D2 and D3, D4, the diodes of each pair being connected in opposition, are serially connected across resistors Rl and R2. The center tap CT is grounded and connected to the junction of diodes D2 and D3. The voltage derived at the point identified as 21 is essentially a square wave equal in magnitude but opposite in phase to the square wave derived at the point 22.
The sensor 11 is represented in Figure 2 as two variable resistors SRl and SR2 which are the two resistance values which vary according to the inclination of the sensor 11. Each antiphase square wave is, in effect, applied across the respective resistor SRl or SR2 to derive a voltage depend-ing upon the values of the resistors SRl or SR2. The antiphase voltages derived across resistors SRl and SR2 are applied through resistor R6 to one input of a differential amplifier DAl formed as an integrated circuit.
The REL circuit 13 of Figure 1 is formed as three resistors R3, R4 and R5 serially connected across the points 21 and 22. R4 is a variable re-sistor which can be set at any desired value to determine the reference pos-ition of the sensor 11. The voltage derived across the combination of R3 and , .

oa~z part of R4 and the antiphase voltage derived across R5 and the remainder of R3 are applied to the second input of DAl. The difference between the voltages derived by the resistors SRl, SR2 and the voltages derived by the potential divider R3, R4 and R5 are amplified in DAl, the gain of which is controlled by resistor R7.
: The PDAD 15 of Figure 1 is a symmetrical circuit connected across the points 21 and 22. It comprises series connected resistors R8, R9, R10 and Rll, the junction of R9 and R10 being connected to the output of DAl. Two resistors R12 and R13 in series are connected between the junction of resis-tors R8 and R9 and the junction of resistors R10 and Rll via two oppositely connected diodes D5 and D6. Two smoothing capacitors Cl and C2 are connected across resistors R12 and R13, the junction of capacitors Cl and C2 being grounded. The output of the PDAD is taken at the junction of resistors R12 and R13.
A voltage, the magnitude of which is dependent on the voltage across SRl, the voltage across R3 and part of R4, the gain of DAl and the values of resistors R8 and R9, is obtained at the junction of R8 and R9. This voltage is rectified into negative pulses by diode D5, these pulses being smoothed by capacitor Cl into a negative D.C. voltage appearing across R12.
2Q Simiarly, a voltage, the magnitude of which is dependent on the volt-age across SR2. The voltage across R5 and part of R4, the gain of DAl and the values of resistors R10 and Rll, is obtained at the junction of R10 and Rll.
This voltage is, of course, in phase opposition to the voltage obtained at the junction of R8 and R9 and is rectified by diode D6 and smoothed by capac-itor C2 to provide a D.C. positive voltage across resistor R13.
The resulting voltage at the junction of R12 and R13 is the sum of the negative voltage on R12 and the positive voltage on R13.
The potentiometer 16 is represented in Figure 2 as a grounded resis-tance R14 and wiper W providing an input to the grounded display 17.
The buffer circuit 18 of Figure 1 is represented b~ a resistor R15 llOQ212 - serially connected to the input of an inverting applifier IAl, which may be formed as an I.C. The gain of IAl is controlled by resistor R16.
The alarm 14 shown in Figure 1 will now be described in greater detail with reference to Figure 3~
A zener diode Z is connected through a resistor R17 to a positive potential. A rheostat R 18 is connected across the zener diode Z and the output side of the rheostat is connected to the positive input of a differ-ential amplifier DA2. The output side of the rheostat is also connected through an inverter IA2 to the negative input of a differential amplifier DA3.
The negative input of D2 and the positive input of DA3 are both connected to an input terminal Vin which is connected to the junction of resistors R12 and R13 of Figure 2. Thus, if Vin is greater than the positive reference voltage established by rheostat R18, the output A of DA2 goes high and output B of DA3 goes low and if Vin is more negative than the negative reference voltage established at the output of inverter IA2, the output A
goes low and output B goes high~
Output A is connected through a resistor to the base of an NPN trans-istor Tl the emitter of which is connected to a negative potential and the collector of which is connected through a resistor to a positive potential.
2Q Output B is connected through a resistor to the base of an NPN transistor T2 to the emitter of which is also connec~ed to the negative potential and the collector of which is also connected to the positive potential through a resistor. When either output A or B is high transistor Tl or T2 is biased into conduction so that the collector potential becomes virtually identical to the emitter potential. Thus the collector potential becomes low and this is used as an alarm signal.
The double transistor arrangement Tl, T2 operates as an OR gate which could take other forms, for example, a double diode arrangement in which inputs A and B are connected respectivel~ through two diodes the cathodes of which are connected together.

` -`' 1~0~212 It should be understood that the protective housing containing the sensors 11, 11' is, in use, secured to the surface or structure being tested or monitored by means of clamps, fasteners, cement, adhesives, magnetic bonds, soil anchors or any appropriate means.
The circuitry of Figure 2 which derives an output voltage indicative of the tilt angle and direction of sensor 11 is, of course, duplicated for sensor 11'. The main portion of this combined circuitry up to and including R14 and excluding SRl and SR2 which are incorporated in the sensor is incor-porated in an interface module connected to the sensors 11 and 11' by leads.
The interface module may be located adjacent or attached to the sensor hous-ing or may be located some distance therefrom at a maximum distance determined by the losses and noise generated in the leads. A knob for varying resistance R4 to set the reference level, a knob for movlng wiper W to provide proper calibration and means for varying the gain of DAl and/or IAl may be provided on the interface module.
The remainder of the circuitry to the right of R14 is incorporated in a monitor assembly at which the data from the interface module is displayed at any desired location remote from the sensors 11, 11'. The monitor can easily be ad;apted for use with more than one interface module and sensor assembly.
As described, the two signals corresponding to the tilt angle and direction with respect to the two orthogonal axes are processed separately and independently but, of course the auxiliary outputs could be applied to further circuitry in order, for example, to obtain a representation of or value for the vector sum of these two signals.
Where a mains supply is not available, the transformer Tl may be replaced by a 24 volt battery feeding a function generator G shown in Figure 4. The function generator is supplied by lines 25 and 26 connected across the 24 volt battery and representing connections to ~12 volts and -12 volts, respectively. A zero volt terminal in the battery is grounded and connected to a line 27 which corresponds to the centre tap CT of Figure 2. The connec-tion of the function generator G is shown by two lines 28 and 29 but it should be understood that various resistors and capacitors would be connected between function generator G and lines 25 and 26 in a manner well known in the art.
The output of function generator G is taken on line 30 and passed through a resistor R30 to a negative input of an inverting amplifier IA3 which is biased by the ~12 and -12 voltages by lines 31 and 32. A calibrat-ing variable resistor R31 is connected in the feedback loop of amplifier IA3.
The output of amplifier IA3 taken on line 32 is a sine wave relative to the zero voltage on line 27.
The output of amplifier IA3 is also passed through a resistor R32 and supplied to a negative input of an inverting amplifier IA4 having in its feedback loop a fixed resistance R33 equal in value to resistance R32 whereby it operates as an inverter providing an output voltage on line 33 equal in amplitude but opposite in phase to the voltage on line 33.
As stated, line 27 is equivalent to the centre tap CT and so line 27 replaces line CT in Figure 2. Also, lines 32 and 33 are connected to resistors Rl and R2, respectively instead of windings Sl and S2.
Typical applications include the monitoring of cased lateral distor-tion, surveillance of dams, the study of slope stability and embankment settlement patterns, tower installation orientation, the monitoring of structural member deflection, monitoring pipeline hillside sideslip, in addition to offshore and laboratory applications.
The system according to the invention is not limited to applica-tions in which the sensors are mounted in a fixed location. For example, the sensors and interface module may be combined in a rugged housing mounted rigidly on two runners to form a sled which can be pulled along a pipe the gradient of which is being analysed. In this case, as only one axis is of interest, only one sensor 11 or 11' is necessary and the auxiliary output ~` -" llOOZlZ

is advantageously fed to a chart recorder so that a continuous record of the pipe geometry can be obtained. This record would show gradient in per-cent or degrees and would aslo pinpoint problem areas such as serious joint separation, settling and undulation.

Claims (7)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A system for sensing deviation of a surface, structure or the like from a reference axis comprising a tilt sensitive transducer including a first and a second impedance the values of which vary differentially accord-ing to the angle and direction of tilt, means for applying an A.C. voltage across the first impedance, means for applying an antiphase A.C. voltage across the second impedance, rectifier means for deriving a positive D.C.
voltage having a magnitude depending on the magnitude of the first impedance and deriving a negative D.C. voltage having a magnitude depending on the magnitude of the second impedance, means for adding the positive D.C. volt-age and the negative D.C. voltage to derive a D.C. voltage the magnitude of which is dependent on the angle of tilt and the sign of which is dependent on the direction of tilt.
2. A system according to claim 1 in which the means for applying the A.C. voltage and the antiphase A.C. voltage is a transformer having a center tapped secondary winding.
3. A system according to claim 1 including a third and a fourth imped-ance connected respectively, to the means for applying the A.C. voltage and the means for applying the antiphase A.C. voltage, the third and the fourth impedances being selectively variable, and means for comparing, respectively, the voltages derived across the third, and fourth impedances with the volt-ages derived across the first and second impedances to derive two difference voltages which are supplied to the rectifier means whereby the positive D.C.
signal derived has a magnitude dependent on the magnitude of the difference of the first and third voltages and the negative D.C. signal derived has a magnitude dependent on the magnitude of the difference of the second and fourth voltages.
4. A system according to claim 3 in which the means for comparing is a differential amplifier, two inputs of which are connected respectively to a junction of the first and second impedances and a junction of the third and fourth impedances.
5. A system according to claim 1 in which the means for applying the A.C. voltage and the antiphase A.C. voltage is a function generator supplied by equal magnitude positive and negative voltages from a battery, the function generator having an output connected to an amplifying means to derive at an output thereof the A.C. voltage, the output of the amplifying means being connected to an inverter to derive at an output thereof the antiphase A.C.
voltage.
6. A system according to claim 2 or claim 5 including a third and a fourth impedance connected respectively, to the means for applying the A.C. voltage and the means for applying the antiphase A.C. voltage, the third and the fourth impedances being selectively variable, and means for comparing, respectively, the voltages derived across the third, and fourth impedances with the voltages derived across the first and second impedances to derive two difference voltages which are supplied to the rectifier means whereby the positive D.C. signal derived has a magnitude dependent on the magnitude of the difference of the first and third voltages and the negative D.C. signal derived has a magnitude dependent on the magni-tude of the difference of the second and fourth voltages.
7. A system according to claim 1, 2 or 5 including means comparing the voltage derived by the adding means with predetermined positive and negative voltages and means instigating an alarm when the voltage derived exceeds in magnitude the predetermined positive or negative voltages.
CA299,116A 1978-03-16 1978-03-16 Tilt detection-system Expired CA1100212A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA299,116A CA1100212A (en) 1978-03-16 1978-03-16 Tilt detection-system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA299,116A CA1100212A (en) 1978-03-16 1978-03-16 Tilt detection-system

Publications (1)

Publication Number Publication Date
CA1100212A true CA1100212A (en) 1981-04-28

Family

ID=4111015

Family Applications (1)

Application Number Title Priority Date Filing Date
CA299,116A Expired CA1100212A (en) 1978-03-16 1978-03-16 Tilt detection-system

Country Status (1)

Country Link
CA (1) CA1100212A (en)

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