CA1167104A - Magnetic field differential probe - Google Patents

Magnetic field differential probe

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Publication number
CA1167104A
CA1167104A CA000361280A CA361280A CA1167104A CA 1167104 A CA1167104 A CA 1167104A CA 000361280 A CA000361280 A CA 000361280A CA 361280 A CA361280 A CA 361280A CA 1167104 A CA1167104 A CA 1167104A
Authority
CA
Canada
Prior art keywords
magnetic field
magnetic
differential probe
field differential
wires
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
CA000361280A
Other languages
French (fr)
Inventor
Friedrich M.O. Forster
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of CA1167104A publication Critical patent/CA1167104A/en
Expired legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R33/00Arrangements or instruments for measuring magnetic variables
    • G01R33/02Measuring direction or magnitude of magnetic fields or magnetic flux
    • G01R33/022Measuring gradient

Abstract

ABSTRACT

A magnetic field differential probe has field sensors located at spaced intervals along a tensilely stressed diamagnetic wire free of mechanical support between the sensors.

Description

'7~

The present invention relates generally ts a magnetic field differential probe and, more particularly, ~o such a differential probe the par~s of which can be quickly and accurately adjusted into parallelisrn for use.

BACKGROUND OF THE INVENTION

Differential probes are primarily used f~r detecting ferromagnetic bodies hidden in the earth or in water, such as bombs, mines, ships, ship parts or the like. Such bodies are located by evaluating the disturbance caused by such bodies of the otherwise homogeneous magnetic field of the earth, i.e., the earth field gradient. In many cases, harmonic-wave magnetic field sensors are used for this purpose in which the transducer consists of a soft-magnetic core element of high magnetic permeability. The core is magnetized to full saturation by a magnetic alternating field of a given frequency. An external magnetic field occuxring in the direction of the core element results in a dissymmetry of the magnetization charac~eristic of the core element thereby producing in ~he winding surrounding the core element an electric voltage of an amplitude proportional to the field strength of the external magnetic field and of a frequency consisting in an even-numbered harmonic wave of the frequency of the exciting alternating field. Although it is true that harmonic wave magnetic field probes are useful for this purpose, other magnetic ield sensors may on prinicple also r~
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be used in a differential probe, and, in particular, in so-called search instruments.

Frequently, the above-mentioned differential probes must resolve magnetic field differences in the ranye of 1 x 10 9 Tesla (1 nano Tesla), while under the influence of a field strength of 50jO00 nano Tesla. In the case of a search device, this may for instance be the influence of the magnetic earth field. However, this means that exacting demands must be placed on the parallelism of the magnetic axes of the magnetic field sensors used in relation to each other and also in relation to an imagined straight line for the entire probe; otherwise, a difference in the magnetic fields could be falsely indicated in the case of a rotation of the differential probe about its longitudinal axis, for example. The angular deviation from parallelism would have to be kept below 4 seconds of arc, i.e., 2 x 10-5 radians.

In search applications, the sensitivity of the differential probe increases as the base distance between the magnetic field sensors increases. The upper limit of the base distance is determined by the temperature and aging effects provoking a maladjustment of the parallelism of the magnetic axes of the sensors. Presently, this upper limit is approximately 0.5 meters.

A magnetic field differential probe of the general type referenced above is set forth in United States Patent
3,982,179. The differential probe of this patent has each magnetic core element fastened onto two stretched wires extending at a specified distance and parallel to each other.
One end of the wires is provided with means for maintaining the parallelism which enables the exact adjustment of the parallelism of the magnetic core elements in two planes vertical to each other. The two wixes are ~enerally part of a continuous wire formed by a return means into a U-shaped loop and maintained under mechanical tension by a spring.

As compared to differential probes formerly used, the probe of this patent offers a considerable advantage.
While the former differential probes had their magnetic field sensors installed in the upper and lower ends, respectively, of a probe tube so that any distortion of the probe tube provoked a notable maladjustment of the parallelism of the magnetic axes, this error source is eliminated.

However, there still remain other possible detrimental effects upon the parallelism which are important. Different degrees of extension ~f the material of the return means and the material between the points where the free ends of the U-shaped wire loop are clamped, lead to non-parallelism.
The same applies even more to a possible rotation of the return means about the longitudinal axis of the differential probe. Such a rotation for a given angle causes the two ends of the wires in the return means to be dislocated in opposite senses, and this, in turn ! resul~s in a deviation from ~4--parallelism which is greater the larger the diameter of the return means becomes. The only way to avoid this latter error is to provide a correspondin~ly sturdy ancl weighty design of the return means, but this necessarily renders handling more difficult and increases cost. The means or maintaining the parallellsm, which necessarily must be constructed to cover a relatively wide range of adjustment, constitute an additional risk of changes from parallelism due to temperature influences and shocks. Still further, the two means for maintaining parallelism require finely adjustable slides with carefully finished guide faces, which renders them rather expensive. If the deviation from parallelism produced by the gravity forces resulting from the slack of the two wires when the differential probe is in the horizontal position, is to be kept within narrow limits, the tension must be very highO But the high tension, in turn, means that the tension forces in the two wires must be well balanced by the use of a freely turning return roller, for example. However, in this case the shock-proof suspension of the roller can be achieved only at great cost. The desire to reduce the slack Q~ the wires leads to the use of materials for the latter which combine the properties of light weight, low extension and strength. However, as such materials are rather brittle, they require a wide radius of cur~ature, and this, in turn, leads to undesirably large diameters for the return meansO

OBJECTS AND SUMMARY OF THE INVENTION
. .

It is therefore an objecl of the presen~ invention to provide a differential probe in which probe core parallelism achieved during production is already such that the necessity of readjustment is eithe~ completely avoided or reduced to a minimum, and in which the parallelism is resistant to shocks and temperature influences even when base distances are relatively yreat.

In the practice of the present invention, the probe magnetic core elements determining the magnetic axes of the maynetic field sensors are mounted on one continuous wire arrangement which is stretched between two end points and completely unsupported between the magnetic core elements.
With the wire arrangement tensioned, the deviation from parallelism of the magnetic core elements de~ends only on two factors, namely, the slack in the wire arrangement caused by gravity, and the deviation in parallelism between the magnetic core elements and the axis of the wire arrangement at the point where-$he magnetic core elements are mounted.
By optimal selection of the wire material, the deviation from parallelism caused by the slack can be maintained within very narrow limits, at least if only the magnetic core elements themselves are supported on the wire arrangement. With the -probe maintained substantially vertically, which is the normal position for seaTch devices, the deviation caused by the slack is of min`or importance. As will be shown hereafter, '7~

the suspension of the magnetic core elements on the wire arrangement can be carried out so t~at in many cases the need for subsequent adjustments is completely eliminated~
In any case, however, the range necessary for adjusting the parallelism is extremely reduced so that means for maintaining the parallelism can be us~ed which are not sultable for larger ranges, such as the so-called magne!tic method which permits the non-contact complete compensation of the remaininy minor deviations from parallelism.

According to the magnetic method, a balancing body extending vertically in relation to the probe magnetic core element and consisting of a strip or pin of a highly permeable soft-magnetic materlal, is brought near to the magnetic core element so that the magnetic axis of the latter tilts towards the balancing element. This method is described in United States Patent 3,487,459. However, in practice, it has not been possible to replace the mechanical method of balancing ~he parallelism with the magnetic method of balancing the parallelism. As it is absolutely necessary in differential probes that the properties of the individual sensors exactly conorm, it proved to be disadvantageous that apart from a rising non-linearity of the sensor in response to the degree of tilting of the magnetic axis, the sensitivity of a sensor should vary directly in response to the approach of the strip or pin used as balancing element. In addition, there existed the risk in the case of relatively large balancing elements, which also had to be finely adjusted, of disturbances due ~7--7~

to residual maynetism induced by the relatively strong magnetic fields.

Because of the very small deviations from parallelism to be balanced in the case of the clifferential probe of the invention, very small balancing elements or correspondingly large distances from the maynetic ore element will suffice to restore the parallelism. Accorclingly, the above-mentioned undesirable secondary effects are safely excluded so that in the case of the differential probe of the invention the mechanical method of balancing the parallelism may, if necessary, be completely replaced by the magnetic method of balancing the parallelism. Another advantage can be seen in the elimination of any special spring arrangement for tensioning the supporting wires.

Still further, as compared to the differential probes heretofore known, the differential probe of the invention is of simpler design, reduces considerably the production cost, achieves an extraordinary stability of core parallelism and eliminates the need ~or maintenance. In addition, the invention permits the construction of a differential probe with a base distance of 2 meters without sacrificing any of the desirable features of operation.

DESCRIPTION OF THE DRAWI~G
__ __ Figure 1 shows an elevational, partially sectional view of a differential prohe in acc:ordance with the invention.

Figuxe 2 is an enlaxged sectional view of an end portion of the differentlal probe.

Figure 3 is a sectional view taken long the line 3-3 of Figure 2.

Figure 4 is an elevational, partially fragmentary view of a magnetic core element.

Figure 5 is a sectional view taken along the line 5-5 of Figure 4.

Figure 6 is an elevational view of a balancing element.

Figures 7 ~nd 8 show other magnetic core elements.

DESCRIPTION OF A PREFERRED EMBODIMENT
.

The differential probe 1 shown in Figure 1 includes two harmonic wave,magnetic fiPld sensors 2 and 3 connected in a general manner known for producing a signal to an _g_ ~:~6'~

evaluation means (not shown), which signal corresponds to the magnetic field difference existing between the two sensors 2 and 3, the base distance being identified as B.
The two sensors 2 and 3, which are of exactly identical design, each include as an essential component magnetic core elements 4 which determine the magnetic axes of the two sensors. The magnetic core elements 4 are mounted in a manner to be described on a wire arrangement 5 so that their orientation conforms very exactly to that of the wlre arrangement 5. Coil sets 6 serve both to build up magnetic alternating fields magnetizing the magnetic core elements 4 to saturation, and to receive a signal voltage corresponding to the magnetic field strength. The coil sets 6 are mounted by means of supporting rings 7 on the inside of a probe tube 8 which, in turn, may be mounted in a suitable carrier tube (not shown).

Instead of the sensor arrangement shown here, each of the two sensors 2 and 3 may alternatively include a pair of coil sets 6 and magnetic core elements 4. In this case, the two coil sets an~- core elements belonging to one sensor are arrang d adjacent each other in the longitudinal direction of the differential probe, and the two core elements are fastened to the wire 5 in series.

The probe tube 8 is closed on both ends by caps 9 provided with means 10 for stretching the wire arrangement 5.
The means 10 are illustrated in more detail in Figure 2, and are seen to have a threaded tube 15, a tightening nut 16, a washer 17 and a check-nut I8. Openings 11 in the shell of the cap 9 provide acces~ to the check-nut 18 when the cap 9 is applied. Secured into the bore of the threaded tube 15 is the wire arrangement 5 consisting of three individual wires 19 arranged in parallel contacting rela~ion. The threaded tube 15 may be provided on two sides with flat portions 20 which can be best seen in the sectional view of Figure 3, the flat portions serving to retain the threaded tube 15 against rotation when the nut 16 is tightened for the purpose of stretching the wire arrangement 5. To this end, the flat portions can be either simply retained by means of a wrench or else retained against rotation in ~he bore of the cap 9.

The material of the wire arrangemen~ 5 must have certain exacting physical characteristics. First, its specific gravity should be low so that on the one hand the slack caused by the gravity forces are kept within narrow limits and, on the other hand, the forces and uibrations occasioned by shocks will be as small AS possible and be quickly dissipated.
The tensile strength should be high so as to permit efficient stretching of the wire arrangement 5, while still maintaining a sufficiently large safety margin to the breaking stress.
Of course, only a diamagnetic material can be used. Good results have been obtained with a tungsten wire and with a boron fiber, the latter being produced by precipitating elemental boron upon a tungsten wixe of 10 micrometers ~7 ll~

thickness. The difficulty in processing relatively brittle boron fibers is largely made up for by the fact that their specific gravity is approximately ten tlmes lower than tungsten, although the tensile strength is oE the same maynitude.

The combination of wires lt3 to form the wire arrangement 5 offers several advantages. Provided a given length of the securing area and a given cross-section of the wire arrangement 5, the active securing surface, which determines the adhesive force, is higher when the desired cross-section is built up by several wires. Also, the flexibility of a plurality of wires exceeds that of an individual wire the cross-section of which equals the sum of the cross-sections of the combined wires.

Figure 4 shows such a magnetic core element 4 at a scale approximately ten times larger than that of Figure 2.
A housing tube 25, preferably made of a cera~ic material, includes seven capillary tubes 26 in symmetrical arrangement, four of them filled with a high-t~uality, wire-shaped magnetic core material 27. The other three capillary tubes accommodate the wires 19 of the wire arrangement 5. The locations of these three and also of the aforementioned four capillary tubes 26 are preerably provided in symmetrical arrangement in relation to the center of the housing tube 25 so that torsional forces will mutually cancel themselves and the magnetic center of gravity will be located in the center of the wire arrangement 5. The high mutual parallelism of the .

capillary tubes are most advantageous when both the magnetic core material 27 and the wires 19 fit the capillary tubes 26 as closely as possible. In addition, the wires 19 will rest well against the wall of the capil]ary tubes 26 if the distance between them at the securing point 21 is kept a little larger or smaller ~han the distance between the capillary tubes 26.
The parallel arrangement of several wires 19 not only results in an eli~ination of unwanted torsion, but also in a reduction of the slack. To prevent mechanical tensions between the capillary tube 25 and the wires 19, the latter are secured (cemented) to the capillary tube 25 only on one side. To this end, a groove 28 surrounding the tube 25 may be provided which enables the adhesive to be applied from the outside.

In assembling the described differential probe 1, one may proceed substantially as follows: The three wires 19 of the wire arrangement 5 are mounted in the prepared magnetic core elements 4 and in two threaded tubes 15 so that their ends extend a little beyond the threaded tubes 15 when the latter are spaced at the correct distance. The free ends of the wire arrangement,5 are clamped in a simple tensioning device. While maintaining the wire arrangement 5 under a slight tension, the threaded tubes 15 are filled with cast resin. In order to bring the wires 19 at the securing point into the desired position and the correct distance, the magnetic core elements 4 are provisionally pushed near the points 21.
When the resin has cured, the magnetic core elements 4 are moved back to their correct location where they are fixed in position by means of an adhesive applied in the groove 28.
The assembly consisting of the wire arrangement 5, the magnetic core element 4 and the threaded tubes 15 with their check-nuts 18, is mounted in the probe tube 8. When the caPs 9 have been fitted over the ends, the wire arrangement 5 is stretched by means of one of the two tightening nuts 16 until the intended tension is reached. Thereafter, the check nuts 18 can be tightened to secure the threaded pipes 15.

The parallelism of the magnetic core elements 4 can be easily checked by rotating the vertically suspended probe tube 8 about its axis and observing the indication obtained. In many cases, the existing parallelism will be already sufficient. Otherwise, the parallelism can be corrected simply by rotating the two magnetic core elements 4 about their axes relative to each other until the slight inclinations of their magnetic axes resulting from the inclinations of the individual wires of the magnetic core material 27 coincide. This is done by rotating one o the two threaded tubes 15 about its axis until the variation of the indication caused by an axial rotation of the differential probe 1 is reduced to a minimum. To this end, the bore of one of the two caps 9 is of a design such that it enables the threaded tube 15 to be rotated.

In pxactice, the magnetic method of balancing maladjustments of the parallelism can be carried out in different ways. For instance, the required small balancing 7 ~

strips may be directly fixed by means of an adhesive to the face of a supporting ring 7. The magnitude of the non-parallelism to be balanced, i.e., the maxim~m difference in indications during an axial rotation of the differential probe 1, determines the radial dis~ance between the balancing strip and the tube center, while the resulting direction of the adjustment determines the angular position of the balancing strip. Another possibility of carrying out the magnetic method for balancing misadjus~ments in parallelism consists in that the balancing strips 12 are .embedded in small plastic pills 13 (Figure 6) which are fi~ed by means of an adhesive to the outside of the probe tube 8. In this case, the axial distance is varied instead of the radial distance in order to balance out the different amounts of non-parallelism.

Figure 7 shows a magnetic core element 31 consisting essentially of a tube 32 of a soft-magnetic, highly-permeable material. The wire arrangement consists in this case preferably of a single wire 33. The tube 32 is provided with a full-length.sl-ot 34 so that it does not constitute a short-circuited turn for the exciting alternating field.
No slot 34 is necessary if the magnetic excitation of the core element 32 is achieved by a circular alternating field generated by a current flowing through the wire 33.

Figure 7 shows another magnetic core element 35, also of cylindrical shape. In this case, the element takes the form of an extremely thin coat 36 of a soft magnetic highly-permeable material applied upon the wire 33. The coating may be applied by vaporization, for example. The geometry of the magnetic core element 36 achieved by this process is closely adpated to that of the stretched wire 33, so that no balancing of ~he parallelism will be necessary even if the highest demands are placed on the arrangement.

Claims (17)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A magnetic field differential probe having a housing and two magnetic field sensors each with a magnetic core element having its magnetic axis extending parallel to a predetermined straight line which magnetic core elements are spaced along said straight line at a predetermined base distance, said sensors being connected to evaluation means for generating an electric signal corresponding to the difference between the magnetic fields existing at the respective locations of the magnetic field sensors, comprising:
a plurality of diamagnetic wires mounted on said probe housing in tension and arranged in a straight line parallel to said predetermined line; and the magnetic core elements are each affixed to said plurality of wires and mutually spaced from one another at said prescribed base distance.
2. A magnetic field differential probe as in claim 1, in which the wire arrangement includes a plurality of wires laterally spaced and parallel to each other.
3. A magnetic field differential probe as in claim 1, in which each magnetic core element includes an elongated body of a diamagnetic material having a plurality of openings extending in parallel to the longitudinal axis of the body, at least one of said openings including wire-shaped magnetic cores, and at least one of said openings including one of the wires of the wire arrangement.
4. A magnetic field differential probe as in claim 3, in which the openings including the magnetic cores and the openings including the wires are arranged symmetrically about the central axis of the elongated body.
5. A magnetic field differential probe as in claim 3, in which both the wires and the magnetic cores closely fit in the openings of the elongated body.
6. A magnetic field differential probe as in either of claims 3 or 4, in which the relative lateral spacing between the wires differs from the lateral spacing between the respective openings of the elongated body accommodating the wires at least at one point.
7. A magnetic field differential probe as in claim 3, in which the elongated body is of cylindrical shape and equipped on one end with a groove extending to the wires passing therethrough and a quantity of adhesive within said groove affixing the body to the wires.
8. A magnetic field differential probe as in claim 1, in which the magnetic core elements are rotatable relative to each other about their longitudinal axes.
9. A magnetic field differential probe as in claim 1, in which an oblong balancing body of a highly-permeable, magnetically soft material, is affixed to the housing and arranged in substantially vertical orientation relative to the magnetic core element axis.
10. A magnetic field differential probe as in claim 1, in which the wire arrangement is fixed at least at one end in a threaded sleeve mounted on the housing and which is adjustable in the axial direction.
11. A magnetic field differential probe as in claim 10, in which the sleeve is secured against rotation.
12. A magnetic field differential probe as in claim 1, in which the magnetic core elements each consists of a small tube of a highly permeable, magnetically soft material.
13. A magnetic field differential probe as in claim 12, in which the tube includes a longitudinally extending slot.
14. A magnetic field differential probe as in claim 1, in which the magnetic core elements consist of a coating of a highly permeable, magnetically soft material formed onto a single wire.
15. A magnetic field differential probe as in claim 12, in which an exciting alternating current flows through the wire arrangement to provide magnetic saturation of the magnetic core element.
16. A magnetic field differential probe as in claim 1, in which the mechanical tension of the wire arrangement is solely the result of its elastic extension.
17. A magnetic field differential probe as in claim 1, in which the base distance is larger than 1 meter.
CA000361280A 1979-10-24 1980-09-30 Magnetic field differential probe Expired CA1167104A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP2942847.5 1979-10-24
DE2942847A DE2942847C2 (en) 1979-10-24 1979-10-24 Magnetic field difference probe

Publications (1)

Publication Number Publication Date
CA1167104A true CA1167104A (en) 1984-05-08

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CA000361280A Expired CA1167104A (en) 1979-10-24 1980-09-30 Magnetic field differential probe

Country Status (5)

Country Link
US (1) US4384253A (en)
EP (1) EP0028302B1 (en)
AT (1) ATE2462T1 (en)
CA (1) CA1167104A (en)
DE (1) DE2942847C2 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3134811C1 (en) * 1981-09-03 1999-02-18 Stn Atlas Elektronik Gmbh Arrangement for determining the spatial variation of magnetic field gradients
US4590425A (en) * 1982-06-23 1986-05-20 Schonstedt Instrument Company Magnetic detector apparatus with excitation conductors connected in series via sensor housing
US4539522A (en) * 1982-06-23 1985-09-03 Schonstedt Instrument Company Magnetic detector apparatus with liquid-supported, conductive, sensor-support tube
FR2558599B1 (en) * 1984-01-24 1986-08-01 Thomson Csf METHOD AND DEVICE FOR AUTOMATIC COMPENSATION OF MECHANICAL ERRORS OF A MAGNETIC GRADIENTMETER
CA1219633A (en) * 1984-11-13 1987-03-24 Her Majesty The Queen, In Right Of Canada, As Represented By The Minister Of National Defence Magnetic transducer
US5115197A (en) * 1990-03-26 1992-05-19 Giusseppe Brandolino Fluxgate sensor having adjustable core extending beyond a coil winding and a gradiometer incorporating a pair of sensors
DE19725200A1 (en) * 1997-06-14 1998-08-13 Vallon Gmbh Total magnetic field measuring device with triple sensor
DE102004059199A1 (en) 2004-07-02 2006-02-09 OKM Ortungstechnik Krauß & Müller GmbH Arrangement for operating a geophysical locating device
EP2012143B1 (en) * 2007-07-05 2014-11-12 Vallon GmbH Compensation method for differential voltage deviations with varying alignment of a sensor rod of magnetometers in the earth's magnetic field and magnetometer
ES2395844T3 (en) 2009-10-23 2013-02-15 Klaus Ebinger Differential magnetometer probe

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710376A (en) * 1955-06-07 Magnetic armature mirror for galvanometers x
US3281683A (en) * 1966-10-25 One piece, round, galvanometer fila- ment suspension having flattened and reduced diameter portions, and meth- od of making same
DE1153451B (en) * 1956-07-05 1963-08-29 Varian Associates Magnetometer for measuring a magnetic field strength with a probe body made of ferromagnetic material
GB1140950A (en) * 1966-08-02 1969-01-22 Barringer Research Ltd Instrument supporting system
US3439264A (en) * 1967-08-14 1969-04-15 Erick O Schonstedt Core assembly of prefabricated parts for a magnetic field sensor
US3487459A (en) * 1968-03-28 1969-12-30 Erick O Schonstedt Induced magnetic compensation for misalignment of magnetic gradiometer sensors
US3488579A (en) * 1969-04-01 1970-01-06 Erick O Schonstedt Magnetic gradiometer apparatus with misalignment compensation
BE760017A (en) * 1970-12-08 1971-05-17 Org Europeene De Rech MULTIFILAR TORSION CABLE SUSPENSION DEVICE.
US3736502A (en) * 1971-01-28 1973-05-29 Schonstedt Instrument Co Series string flux gate magnetic sensor apparatus with additive response
US3757209A (en) * 1972-02-11 1973-09-04 E Schonstedt Compensation for misalignment of magnetic sensors
GB1445063A (en) * 1974-02-22 1976-08-04 Foerster F Magnetic gradient detector
US3961245A (en) * 1974-11-20 1976-06-01 Schonstedt Instrument Company Magnetic locator having improved sensors
US4110689A (en) * 1975-01-17 1978-08-29 Schonstedt Instrument Company Magnetic detecting apparatus with novel means for positioning sensor assembly in a housing

Also Published As

Publication number Publication date
EP0028302A1 (en) 1981-05-13
ATE2462T1 (en) 1983-03-15
DE2942847A1 (en) 1981-05-07
US4384253A (en) 1983-05-17
EP0028302B1 (en) 1983-02-09
DE2942847C2 (en) 1983-03-24

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