GB2068124A - Conditioning unit for use with linear variable differential transformers - Google Patents
Conditioning unit for use with linear variable differential transformers Download PDFInfo
- Publication number
- GB2068124A GB2068124A GB8002712A GB8002712A GB2068124A GB 2068124 A GB2068124 A GB 2068124A GB 8002712 A GB8002712 A GB 8002712A GB 8002712 A GB8002712 A GB 8002712A GB 2068124 A GB2068124 A GB 2068124A
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- GB
- United Kingdom
- Prior art keywords
- output
- signal
- transducer
- motion
- motions
- 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.)
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING 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
- G01D5/00—Mechanical 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
- G01D5/12—Mechanical 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
- G01D5/14—Mechanical 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
- G01D5/20—Mechanical 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 by varying inductance, e.g. by a movable armature
- G01D5/22—Mechanical 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 by varying inductance, e.g. by a movable armature differentially influencing two coils
- G01D5/2208—Mechanical 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 by varying inductance, e.g. by a movable armature differentially influencing two coils by influencing the self-induction of the coils
- G01D5/2216—Mechanical 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 by varying inductance, e.g. by a movable armature differentially influencing two coils by influencing the self-induction of the coils by a movable ferromagnetic element, e.g. a core
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING 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
- G01D5/00—Mechanical 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
- G01D5/12—Mechanical 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
- G01D5/14—Mechanical 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
- G01D5/20—Mechanical 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 by varying inductance, e.g. by a movable armature
- G01D5/22—Mechanical 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 by varying inductance, e.g. by a movable armature differentially influencing two coils
- G01D5/2291—Linear or rotary variable differential transformers (LVDTs/RVDTs) having a single primary coil and two secondary coils
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
- G01P3/42—Devices characterised by the use of electric or magnetic means
- G01P3/56—Devices characterised by the use of electric or magnetic means for comparing two speeds
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Control Of Position Or Direction (AREA)
Abstract
The invention comprises an excitation and conditioning system for one or two linear variable differential transformers (L.V.D.Ts.) of standard design to give a D.C. analogue voltage output representing:- (a) Position of motion relative to any datum point. (b) Velocity of motion. Automatic internal surveillance of the integrity of the output signals ensures that any electrical failure of the L.V.D.T. or the conditioning unit is immediately indicated. When using two L.V.D.Ts. driven from separate motions, a further output gives the difference in position of the two motions and can be used to synchronise the motions when required. An oscillator produces two sinusoidal outputs in quadrature to excite the L.V.D.Ts. and demodulates their outputs signals by means of sample and hold circuitry. By sampling the position signal twice in each cycle excitation ripple is eliminated. By sampling a third time in the next cycle a rate of change of position signal is obtained, i.e., velocity.
Description
SPECIFICATION
Conditioning unit for use with linear variable differential transformers
This invention relates to the excitation and the conditioning of the signals from one or more linear variable differential transformers (L.V.D.T.'s) of standard design so as to give outputs which provide a distance measuring system, a velocity measuring system, and automatic surveillance of the integrity of the output signals. Existing conditioning equipment only provides a distance measuring system which is not self-monitoring. Satisfactory velocity measurement had not so far been obtainable from an L.V.D.T. and a different type of transducer with its own conditioning system is required therefore, which considerably increases the cost and complexity of the system.
The invention is applicable to any mechanical device, which is moved by means of a hydraulic or pneumatic actuator, where feedback signals of position and/or velocity are required for control purposes. Typical applications would be for hydraulic presses, machine tools, variable stroke pumps, injection moulders, remote handling equipment, aircraft or ship steering and stabilising systems and similar servo system devices. The invention is particularly useful where two actuators produce the mechanical motion and the movements of the actuators need to be synchronised. The necessary signal to control the synchronisation is an integral feature of the invention.
The surveillance system produces a failure signal should the output signals cease to be a true indication of the position or velocity of the mechanical device being controlled. This signal can be used to stop the movement of the mechanical device, or cause it to revert to a fail safe position, until the fault producing the false output is rectified.
The invention comprises an electronic circuit composed of readily available standard components mounted on a single printed circuit board approximately 200mm x 150mm in size. The circuit embodies a type of oscillator which gives two amplitude controlled sinusoidal outputs in quadrature at a fixed frequency in the range of 400Hz to 5000Hz dependant on individual applications. This oscillator is used to excite the L.V.D.T. The oscillator also drives two parallel sets of four gating pulse generators which provide four gating signals at intervals of 90 electrical degrees during each cycle.
These gating pulses are used to drive sample and hold circuits and are denoted by A, B, C & D in the order in which they occur chronologically.
The two signal coils of the L.V.D.T. feed into separate differential amplifiers. Two parallel sets of amplifiers are used denoted by Channel 1 and Channel 2.
Where a single L.V.D.T. is used the signal coils are linked to both channels. When two L.V.D.T.'s are employed, each feeds a single channel. Channel 1 and Channel 2 are identical duplicated circuits; thus only Channel 1 needs description.
The single ended outputs of the signal coil amplifiers are first fed to a summing amplifier which also acts as a rectifier. The output of this amplifier is therefore a D.C. voltage the level of which remains constant within approximately 0.5 volts throughout the total travel of the L.V.D.T. This voltage is fed to two comparators with reference voltages set to give a band gap which contains the normal variation to be expected. The output from each comparator is normally 'HIGH'. Thus failure of either L.V.D.T. signal coil or the oscillator exciting the L.V.D.T. will cause one of the comparators to change state. The resulting 'LOW' will produce the failure signal. This is the first part of the surveillance system.
The same single ended outputs of the signal coil amplifiers are also fed to a differential amplifier. The output from this amplifier will be in accordance with standard practice:- A sinusoidal signal at oscillator frequency, with a maximum amplitude when the
L.V.D.T. is at the beginning of its stroke which decreases to zero as the L.V.D.T. moves to midstroke, and then increases again with a phase inversion of 180O during the motion from midstroke to end of stroke. Typical output signals are shown dotted in
Fig. 1 for zero; f; ; q and full stroke. This signal needs to be demodulated and filtered to remove ripple at oscillator frequency before a useful 'Position
Output' can be obtained.One part of this invention provides an improved demodulation system which can be used to give a 'Position Output' devoid of oscillator ripple with a resolution betterthan one part in ten thousand, ie. .01 mm with a stroke of 1 00mm. This is ten times better than that obtainable with existing systems unless very slow movement is used. In this invention the absence of filters to remove ripple at fundamental frequency much improves the frequency response of the system. The maximum linear velocity for a given resolution will depend on the oscillator frequency employed.
Obtainable values from this equipment for an LV.D.T. with a stroke of 100mm are 50mm/sec for a resolution of 0.1 mm or 500mm/sec for a resolution of 0.1 mm. Some filtration may be employed on the final output signal to remove random noise produced by the electronic components but this will not impair the useful frequency response of this system.
To continue the description of Channel 1. The output signal from the differential amplifier requiring demodulation is first moved by a voltage shift network so that it is always a positive voltage. For exampie +6V + SVmax would be suitable but other voltage ranges could be used. The phase is also adjusted where necessary to coincide with that of the oscillator. Gating Pulse 'A' is used to open and close a suitable electronic switch such as one of the cos/mos type. When closed the switch connects a low leakage capacitor to the signal for a short period of each cycle as the signal approaches its first peak.
The voltage across the capacitor at the instant that the switch opens remains virtually constant until
Pulse 'A' closes the switch again during the next succeeding cycle and any variation in signal voltage due to the next succeeding cycle and any variation in signal voltage due to movement of the L.V.D.T. during this period will, therefore, be detected by the change in voltage level presentwhen the switch opens if compared with the level held during the
previous cycle. To prevent loss of charge on the
capacitor during the time the switch is open the
capacitor is followed by a non-inverting buffer amp
lifier with a high input impedance. A suitable type
which is readily available is an insulated gate F.E.T.
amplifier such as a CA3140E. The voltage level of the
output from the buffer amplifier is, therefore, a true
measure of the position of the L.V.D.T. Reference to
Fig. 1 shows that this voltage is subject to variation whilst the switch is closed, ie. throughout the duration of gating Pulse 'A' especially when the L.V.D.T.
is near the beginning or end of its stroke. This variation or ripple is removed by sampling the output from the 1 st buffer by means of gating Pulse 'B' after gating Pulse 'A' has closed the gate. The 2nd sample & hold circuit is identical with the first and has a buffered output. The output of the 2nd buffer is, therefore, devoid of ripple at oscillator frequency and is used as the 'Position Output' signal from
Channel 1. A similar 'Position Output' signal is obtained from Channel 2. The use of this additional signal is described later.
The 'Velocity Output' is obtained from the 'Position Output' in the following manner. The output level from the 1st buffer is sampled a second time in each cycle by gating Pulse 'D' which controls a 3rd sample and hold circuit, identical in details with the previous two circuits. At the end of a cycle the output levels from the 2nd and 3rd buffers will be identical.
During the 2nd quadrant of the next cycle the output from the 2nd buffer will be updated to take into account any change in L.V.D.T. position during one oscillator cycle. At this instant in time the output
level of the 3rd buffer is that of the previous cycle.
During the 4th quadrant of the new cycle the output of the 3rd buffer is updated again to the new level of the 2nd buffer. The output of the 2nd buffer feeds the non-inverting input of a differential amplifier. The output of the 3rd buffer feeds the inverting input of the same amplifier. Thus the output from this amplifier is proportional to the difference in 'Position
Level' between succeeding cycles during quadrant 2 to quadrant 4 and zero at other times. Gating Pulse 'C' which occurs during the 3rd quadrant is used to drive a fourth sample and hold circuit which samples the output from the differential amplifier during the period that the inputs are fed from the succeeding cycles. The output of the 4th buffer is, therefore, a true measure of the change in position which has occurred during one cycle, ie. the velocity of the motion.This then is the 'Velocity Output' and its
polarity is dependant on the direction of motion
making eminently suitable for feedback control pur
poses. The process is shown diagrammatically in
Fig. 2. A similar 'Velocity Output' is obtained from
Channel 2.
When Channel 1 and Channel 2 are fed from the
same L.V.D.T. the two 'Velocity Output' voltages
should be virtually identical. When two separate
L.V.D.T.'s are used there may be a small permissible
difference determined by the requirements of the
mechanical device being controlled. The two 'Veloc
ity Output' voltages are, therefore, compared by a
further differential amplifier. The output of this amp
lifier feeds into two comparators with reference vol
tages set to give a band gap equivalent to the max
imum permissible error. The output from each com
parator is normally 'HIGH'. Errors greater than per
missible in either 'Velocity Output' voltage will cause
one comparator to change state. The resulting 'LOW'
will produce the 'FAILURE' signal.This is the second
part of the surveillance system and automatically
checks the integrity of gating pulses C & D and their
respective sample and hold circuits in each channel.
The two 'Velocity Output' signals can be fed out
separately, with filter networks to eliminate high fre
quency noise where necessary, and used for control
purposes. Alternativelyrthe two signals can be aver
aged by summing them together in a summing amp
lifierwith the closed loot gain adjusted to give the
desired range of output vDltage. This single output,
filtered where necessary, can be used for velocity
feedback purposes in any suitable control system,
eg. a servo system.
Reverting to the 'Position Output' signals from
Channel 1 and Channel 2:-The two signals are com
pared in the same manner as the 'Velocity Output'
signals with comparators set to a band gap equival
ent to the maximum permissible error in position
between the two channels. A 'LOW' from either
comparator will produce the 'FAILURE' signal. This
is the third part of the surveillance system and
automatically checks the integrity of gating pulses A
& B and their respective sample and hold circuits.
The differential amplifier used in the third part of
the surveillance system, directly compares the 'Posi
tion Output' signals from the two channels. This,
however, is a true measure of the error in position of
the mechanical devices driving the two L.V.D.T.'s.
The error signal can, therefore, be suitably proces
sed to provide a correction for the two motions to
bring them into synchronisation and reduce the
errorto an acceptable low value. For example, in a
press where the platen is moved by two hydraulic
actuators, the error signal could be used to drive a
suitable interface such as an electrohydraulic valve
to increase the fluid flow to one actuator and reduce itto the other to correct any difference in motion
between the two actuators. Alternatively, the error
signal could be used to spill off some fluid from the
actuator which is moving too fast.
The two 'Position Output' signals, filtered where
necessary, can be fed out separately and used for
control purposes; alternatively, they can be summed
and meaned to give a single signal. A D.C. voltage
offset can be introduced at this stage to make the
zero signal output coincide with the mechanical zero
reference point. The combined output signal, filtered
where necessary, can be used as a feedback signal in
a positional servo system or in some other way.
The 'Position Output' signal could be compared
with a 'Reference Position' signal generated by a
potentiometer or digitally by thumbwheel switches,
a computer or a microprocessor. When 'Position'
and 'Reference' become coincident a signal is
obtained for control purposes:- For example to stop
the slide of a machine tool or the platen of a press at
a precise and repeatable position, which can be
selected at will by changing the 'Reference' signal.
Either of the following methods could be amp loyed:- The digital 'Reference' signal could be converted to an analogue voltage and compared directly with the analogue 'Position Output' signal. Alternatively, the analogue 'Position Output' signal could be converted to a digital signal and compared with the digital 'Reference' signal by means of a suitable counter.
A block diagram of one version of this invention using two L.V.D.T.'s is given in Fig. 3.
There will be many applications for this invention where all the available output signals are not required. The invention, therefore, consists of any features of novelty described herewith, taken singly or in any combination.
Claims (6)
1. An electronic conditioning system for the sinusoidal signals from an inductive type of trans ducerwhich is self monitoring and which by means of a plurality of sample and hold circuits triggered from an oscillator with dual outputs in quadrature, which also provides the excitation for the said transducer produces a demodulated output which is devoid of excitation frequency ripple together with a second output which gives the rate of change of the first output.
2. An electronic conditioning system for an inductive type of position transducer which is self monitoring and which by means of a plurality of sample and hold circuits triggered from an oscillator with dual outputs in quadrature, which also provides the excitation for the said position transducer, produces a demodulated output signal of position of motion which is devoid of excitation frequency ripple together with a second output which istheveloc- ity of motion without the need to use an additional velocity transducer.
3. A system which as claimed in claim 1 or 2 produces a failure signal in the event of an electrical failure occurring in the transducer or the conditioning unit, by continuous monitoring of the oscillator signals, the transducer output signals and the sample and hold circuits.
4. A system which as claimed in claims 2 and 3 produces a failure signal in the event of an electrical failure occurring in position transducer or the conditioning unit, which can be used to stop the motion or otherwise ensure the safety of the equipment producing the motion.
5. Asystem which as claimed in claims 2, 3 and 4 but employing two position transducers driven from separate motions produces a further output signal which is proportional to the difference in position of the two motions which can then be used to synchronise the two motions.
6. An electronic system which is substantially as described with reference to the block diagram Fig. 3.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8002712A GB2068124B (en) | 1980-01-26 | 1980-01-26 | Conditioning unit for use with linear variable differential transformers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8002712A GB2068124B (en) | 1980-01-26 | 1980-01-26 | Conditioning unit for use with linear variable differential transformers |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2068124A true GB2068124A (en) | 1981-08-05 |
GB2068124B GB2068124B (en) | 1983-12-14 |
Family
ID=10510924
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8002712A Expired GB2068124B (en) | 1980-01-26 | 1980-01-26 | Conditioning unit for use with linear variable differential transformers |
Country Status (1)
Country | Link |
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GB (1) | GB2068124B (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2512555A1 (en) * | 1981-09-04 | 1983-03-11 | Sentec Sa | USE OF AN ELECTRONIC SENSOR FOR MEASURING THE INSTANT SPEED AND / OR INSTANTANEOUS SPEED VARIATION OF A MOBILE WITH POSITION MEASUREMENT |
FR2538535A1 (en) * | 1982-12-27 | 1984-06-29 | Varian Associates | HIGH RESOLUTION POSITION DETECTION DEVICE, IN PARTICULAR FOR THE MAGNETRON TUNING ROD |
GB2178855A (en) * | 1984-11-16 | 1987-02-18 | Gersan Anstalt | Weighing a number of objects in succession |
US4696358A (en) * | 1984-11-16 | 1987-09-29 | Doerman Eryk S | Weighing a number of objects in succession |
FR2633126A1 (en) * | 1988-06-17 | 1989-12-22 | Aerospatiale | METHOD AND SYSTEM FOR OPERATING SIGNALS FROM INDUCTIVE LINEAR INDUCER SENSORS |
US4916391A (en) * | 1984-11-15 | 1990-04-10 | Doerman Eryk S | LVDT displacement sensor with signal noise reduction for use in weighing apparatus |
FR2671878A1 (en) * | 1991-01-23 | 1992-07-24 | Sextant Avionique | Synchronous detector with analogue gate |
EP1132718A1 (en) * | 2000-03-10 | 2001-09-12 | General Electric Company | Method and apparatus for detecting faults in a transducer |
WO2002090892A2 (en) * | 2001-05-07 | 2002-11-14 | Marposs Società per Azioni | Conditioning device for an analog transducer |
WO2003095946A1 (en) * | 2002-05-07 | 2003-11-20 | Volvo Lastvagnar Ab | Method and device for diagnosis of detector |
EP1780514A1 (en) * | 2005-10-26 | 2007-05-02 | Bosch Rexroth Aktiengesellschaft | Measuring device and drive controller |
CN104019833A (en) * | 2014-06-13 | 2014-09-03 | 四川亚美动力技术有限公司 | Engine oil pin position sensor detecting circuit |
-
1980
- 1980-01-26 GB GB8002712A patent/GB2068124B/en not_active Expired
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2512555A1 (en) * | 1981-09-04 | 1983-03-11 | Sentec Sa | USE OF AN ELECTRONIC SENSOR FOR MEASURING THE INSTANT SPEED AND / OR INSTANTANEOUS SPEED VARIATION OF A MOBILE WITH POSITION MEASUREMENT |
FR2538535A1 (en) * | 1982-12-27 | 1984-06-29 | Varian Associates | HIGH RESOLUTION POSITION DETECTION DEVICE, IN PARTICULAR FOR THE MAGNETRON TUNING ROD |
US4916391A (en) * | 1984-11-15 | 1990-04-10 | Doerman Eryk S | LVDT displacement sensor with signal noise reduction for use in weighing apparatus |
GB2178855A (en) * | 1984-11-16 | 1987-02-18 | Gersan Anstalt | Weighing a number of objects in succession |
US4696358A (en) * | 1984-11-16 | 1987-09-29 | Doerman Eryk S | Weighing a number of objects in succession |
GB2178855B (en) * | 1984-11-16 | 1989-04-19 | Gersan Anstalt | Sensing displacement using a linear variable differential transformer |
AU605670B2 (en) * | 1984-11-16 | 1991-01-17 | Anstalt Gersan | Sensing displacement using a linear variable differential transformer |
US4937523A (en) * | 1988-06-17 | 1990-06-26 | Aerospatiale Societe Nationale Industrielle | Method and system for exploiting the signals of linear inductive sensors, which system is adaptable for different sensor structures |
EP0348259A1 (en) * | 1988-06-17 | 1989-12-27 | AEROSPATIALE Société Nationale Industrielle | System for the exploration of signals provided by linear inductive displacement sensors |
FR2633126A1 (en) * | 1988-06-17 | 1989-12-22 | Aerospatiale | METHOD AND SYSTEM FOR OPERATING SIGNALS FROM INDUCTIVE LINEAR INDUCER SENSORS |
FR2671878A1 (en) * | 1991-01-23 | 1992-07-24 | Sextant Avionique | Synchronous detector with analogue gate |
EP1132718A1 (en) * | 2000-03-10 | 2001-09-12 | General Electric Company | Method and apparatus for detecting faults in a transducer |
US7138794B1 (en) | 2000-03-10 | 2006-11-21 | General Electric Company | Detection of faults in linear and rotary voltage transducers |
WO2002090892A2 (en) * | 2001-05-07 | 2002-11-14 | Marposs Società per Azioni | Conditioning device for an analog transducer |
WO2002090892A3 (en) * | 2001-05-07 | 2007-10-25 | Marposs Spa | Conditioning device for an analog transducer |
WO2003095946A1 (en) * | 2002-05-07 | 2003-11-20 | Volvo Lastvagnar Ab | Method and device for diagnosis of detector |
EP1780514A1 (en) * | 2005-10-26 | 2007-05-02 | Bosch Rexroth Aktiengesellschaft | Measuring device and drive controller |
CN104019833A (en) * | 2014-06-13 | 2014-09-03 | 四川亚美动力技术有限公司 | Engine oil pin position sensor detecting circuit |
CN104019833B (en) * | 2014-06-13 | 2016-06-08 | 四川亚美动力技术有限公司 | Engine oil needle position sensor detection circuit |
Also Published As
Publication number | Publication date |
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GB2068124B (en) | 1983-12-14 |
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Legal Events
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PCNP | Patent ceased through non-payment of renewal fee |