CN111929737B - Method and device for remotely detecting layer interface position and electromagnetic information - Google Patents

Method and device for remotely detecting layer interface position and electromagnetic information Download PDF

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CN111929737B
CN111929737B CN202010983039.5A CN202010983039A CN111929737B CN 111929737 B CN111929737 B CN 111929737B CN 202010983039 A CN202010983039 A CN 202010983039A CN 111929737 B CN111929737 B CN 111929737B
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layer
medium
receiving coil
coil
transmitting coil
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CN111929737A (en
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唐章宏
许月晨
王芬
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Beijing Weizhi Jiachen Technology Development Co ltd
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01VGEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V3/00Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
    • G01V3/08Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation operating with magnetic or electric fields produced or modified by objects or geological structures or by detecting devices
    • G01V3/10Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation operating with magnetic or electric fields produced or modified by objects or geological structures or by detecting devices using induction coils
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/003Measuring arrangements characterised by the use of electric or magnetic techniques for measuring position, not involving coordinate determination
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01VGEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V3/00Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
    • G01V3/38Processing data, e.g. for analysis, for interpretation, for correction

Abstract

The embodiment of the application discloses a method and a device for remotely detecting the interface position and electromagnetic information of a layer, wherein the method comprises the steps of establishing a model of a transmitting coil wound by a vertical shaft in a symmetrical mode and a remote detection fractional turn receiving coil wound by a non-axial symmetry mode and coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil on the receiving coil according to the model; calculating a reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the receiving coil model and the transmitting coil model; calculating the total electric field generated by the transmitting coil at the receiving coil by adopting a field superposition principle; calculating the induced electromotive force of the receiving coil by adopting Gaussian integral according to the total electric field; based on the method, the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency are solved by emitting electromagnetic waves with different working frequencies, and then the position and the electromagnetic information of the interface of the dielectric layer are solved. The method and the device can quickly calculate the position and the electromagnetic information of the medium layer interface, and are favorable for remote and efficient detection.

Description

Method and device for remotely detecting layer interface position and electromagnetic information
Technical Field
The invention relates to the technical field of layer interface detection, in particular to a method and a device for remotely detecting layer interface position and electromagnetic information.
Background
With the rapid development of detection technology, remote edge detection and imaging systems have become hot issues, and especially for the fields of airplanes, radars, underwater submarines, well logging and the like, the development of imaging and remote detection of three-dimensional vector fields becomes very important research content. In the geological exploration process, when the long-distance detection logging can measure the tectonic geologic body in a well, the measuring range of the conventional logging technology is improved to dozens of meters from about one meter around the well.
However, in the process of implementing the present invention, the inventor finds that, in the existing remote detection technology, when detecting the interface position of the dielectric layer and the electromagnetic information, due to the existence of more than one medium, the calculated medium model is no longer an axisymmetric model, the calculation difficulty is high, a three-dimensional numerical solution mode must be adopted to solve the field domain during the simulation calculation, and particularly, for the large electric size and the small electric size with a relatively high contrast ratio, the number of divided grid nodes is too large, which correspondingly causes an excessively large calculation amount and a low calculation speed, and thus the requirement of remote and efficient detection is difficult to meet.
Disclosure of Invention
The embodiment of the application provides a method and a device for remotely detecting the position and the electromagnetic information of a layer interface, which can quickly calculate the position and the electromagnetic information of a medium layer interface and are beneficial to remote and efficient detection.
In a first aspect, an embodiment of the present application provides a method for remotely detecting a layer interface location and electromagnetic information, where the method includes:
establishing a model of an axisymmetrically wound transmitting coil and a model of a non-axisymmetrically wound far detection fractional turn receiving coil which is coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the models of the transmitting coil and the receiving coil;
calculating a reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil;
calculating a total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle;
calculating the induced electromotive force of the receiving coil by adopting Gaussian integral according to the total electric field at the receiving coil;
and according to the induced electromotive force, by transmitting electromagnetic waves with different working frequencies, solving the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency, and according to the amplitude and the phase angle of the induced electromotive force, solving the position and the electromagnetic information of the interface of the dielectric layer.
As a possible implementation, the model of the non-axisymmetrically wound far detecting fractional turn receive coil is represented as:
the discs on which the receiving coils are wound being divided intoN>An even number of sector areas passing through the center of a circle, wherein the serial numbers of the sector areas are arranged clockwise;
each turn of the receiving coil is divided intoN1 fractional sub-turn, each fractional sub-turn being wound in a sector, the fractional sub-turns of two adjacent sectors being wound in opposite directions, and the sectors being wound in opposite directionsNEmptying; each fractional sub-turn comprises a circumferential arc part and a radial straight line part, wherein the circumferential arc part is wound on the circumferential part of the sector area, and the radial straight line part is wound on the radial tangent plane part of the sector area passing through the center of a circle;
sector area 1 &N-1 fractional sub-turn ratios of the windings respectivelyn 1n N-1The ratio ofn iSatisfy the requirement of
Figure 377184DEST_PATH_IMAGE002
And is
Figure 147694DEST_PATH_IMAGE004
In the formulaiIs shown asiA sector-shaped area is formed by the circular arc-shaped area,n i representing a sector areaiThe number of the corresponding fractional turns is,Nthe number of the sector areas.
As a possible implementation manner, the eliminating, according to the receiving coil, the direct-coupled electromotive force generated by the transmitting coil to the receiving coil based on the model of the transmitting coil and the receiving coil includes:
the electric field generated by the transmitting coil which is coaxial and parallel to the receiving coil in the uniform medium is a concentric circle on the plane where the remote detection receiving coil is located, all radial straight line parts of the receiving coil passing through the center of the concentric circle are perpendicular to the direction of the electric field, all circumferential arc parts are parallel to the direction of the electric field, according to the winding direction of the receiving coil, the integral result of the electric field along the receiving coil is 0, correspondingly, the induced electromotive force received by the receiving coil is 0, and the direct coupling electromotive force generated by the transmitting coil to the receiving coil is eliminated.
As a possible implementation, in the calculating the reflected field of the transmitting coil at the receiving coil by using the mirror image method according to the model of the receiving coil and the transmitting coil, the determining a relationship between the mirror image source of the transmitting coil and the real source includes:
in a medium model comprising at least two layers of media, introducing a virtual mirror image transmitting coil which is in mirror symmetry with a transmitting coil in a first layer of media into a second layer of media, naming a real transmitting coil as a real source, naming the mirror image transmitting coil as a mirror image source, and replacing the second layer of media with the first layer of media, wherein the medium model is an axisymmetric model, and a relational expression between the mirror image source of the transmitting coil and the real source is as follows:
Figure 445952DEST_PATH_IMAGE005
in the formula (I), the compound is shown in the specification,I 2is the current of the mirror image source,I 1in order to be the current of the real source,
Figure 558702DEST_PATH_IMAGE006
is the reflection coefficient of the first layer medium and the second layer medium,
Figure 131766DEST_PATH_IMAGE006
is expressed as
Figure 225624DEST_PATH_IMAGE008
Wherein, in the step (A),
Figure 491520DEST_PATH_IMAGE010
is the wave impedance in the first layer of medium,
Figure 772460DEST_PATH_IMAGE012
is the wave impedance in the second layer of medium,
Figure 414794DEST_PATH_IMAGE014
Figure 159896DEST_PATH_IMAGE016
Figure 268798DEST_PATH_IMAGE017
and
Figure 568192DEST_PATH_IMAGE018
the magnetic permeability of the first layer medium and the second layer medium respectively,
Figure 483058DEST_PATH_IMAGE019
and
Figure 282999DEST_PATH_IMAGE020
complex dielectric constants of the first layer medium and the second layer medium respectively, and the expression is
Figure 156278DEST_PATH_IMAGE022
Figure 411810DEST_PATH_IMAGE024
Wherein
Figure 130367DEST_PATH_IMAGE026
And
Figure 850061DEST_PATH_IMAGE028
the real parts of the dielectric constants, σ, of the first and second layers of medium1And σ2The electrical conductivity of the first layer of medium and the second layer of medium respectively,
Figure 831924DEST_PATH_IMAGE030
is the angular frequency of the electromagnetic wave, j is the imaginary unit, j2=-1。
As a possible implementation manner, the solving of the amplitude and the phase angle of the induced electromotive force of the receiving coil at each operating frequency by emitting electromagnetic waves with different operating frequencies according to the induced electromotive force, and the solving of the position and the electromagnetic information of the dielectric layer interface according to the amplitude and the phase angle of the induced electromotive force includes:
setting the distance between the layer interface and the transmitting coil to d meters, wherein the electromagnetic information of the medium layer interface comprises the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
Transmitting electromagnetic waves of at least two different operating frequencies by a transmitting coil, and generating a receiving coilThe phase angle of the induced electromotive force is recorded as
Figure 637069DEST_PATH_IMAGE031
And
Figure 362579DEST_PATH_IMAGE032
the wavelength of the electromagnetic wave at the first operating frequency in the first layer of medium is
Figure 936780DEST_PATH_IMAGE033
The electromagnetic wave at the second working frequency has a wavelength in the first layer of medium
Figure 89544DEST_PATH_IMAGE034
Wherein, in the step (A),
Figure 116406DEST_PATH_IMAGE035
the first operating frequency is the wavelength in vacuum,
Figure 648537DEST_PATH_IMAGE036
Figure 811665DEST_PATH_IMAGE037
the relative permeability and the relative permittivity of the first layer of medium,
Figure 197647DEST_PATH_IMAGE038
a wavelength in vacuum for a second operating frequency;
the phase angle of the electromagnetic wave at the first operating frequency varying by 2 x d
Figure 915067DEST_PATH_IMAGE039
And the phase angle of the electromagnetic wave at the second operating frequency is changed to
Figure 779118DEST_PATH_IMAGE040
At the layer interface, the phase angle of the reflection coefficient at the first operating frequency is
Figure 62332DEST_PATH_IMAGE041
The phase angle of the reflection coefficient at the second operating frequency is
Figure 619215DEST_PATH_IMAGE042
The equations (1) to (3) are listed according to the variation rule of phase angle amplitude of the electromagnetic wave in the medium:
Figure 558352DEST_PATH_IMAGE043
in the equation (1),
Figure 226094DEST_PATH_IMAGE044
in the equation (2),
Figure 567076DEST_PATH_IMAGE045
in the equation (3),
in the formula (I), the compound is shown in the specification,
Figure 294861DEST_PATH_IMAGE046
presentation pair
Figure 518032DEST_PATH_IMAGE047
Taking a real part of the signal,
Figure 989465DEST_PATH_IMAGE048
presentation pair
Figure 182024DEST_PATH_IMAGE049
Taking a real part of the signal,real(V1) Is shown as pair V1Taking a real part of the signal,real(V2) Is shown as pair V2Taking the real part, V1Is an induced electromotive force of the receiving coil at a first operating frequency, V2The induced electromotive force of the receiving coil at the second operating frequency,
Figure 80710DEST_PATH_IMAGE050
Figure 791177DEST_PATH_IMAGE051
respectively at a first operating frequency andthe reflection coefficient of the lower layer interface of the second working frequency to the electromagnetic wave is respectively expressed as follows:
Figure 3983DEST_PATH_IMAGE053
Figure 116296DEST_PATH_IMAGE055
wherein
Figure 389145DEST_PATH_IMAGE057
Figure 321329DEST_PATH_IMAGE059
Figure 400144DEST_PATH_IMAGE061
Figure 570225DEST_PATH_IMAGE063
Figure 545134DEST_PATH_IMAGE065
Representing the complex permittivity of the first layer of dielectric at a first operating frequency,
Figure 495773DEST_PATH_IMAGE067
representing the complex permittivity of the first layer of dielectric at a second operating frequency,
Figure 65031DEST_PATH_IMAGE069
representing the complex permittivity of the second layer of dielectric at the first operating frequency,
Figure 151935DEST_PATH_IMAGE071
representing the complex permittivity of the second layer of dielectric at the second operating frequency,
Figure 297746DEST_PATH_IMAGE073
Figure 407784DEST_PATH_IMAGE075
is as followsReal part of dielectric constant, σ, of one layer of dielectric and a second layer of dielectric1、σ2Is the electrical conductivity of the first layer of medium and the second layer of medium,
Figure 828401DEST_PATH_IMAGE076
Figure 707496DEST_PATH_IMAGE077
respectively the angular frequency of the first operating frequency and the angular frequency of the second operating frequency,
Figure 555366DEST_PATH_IMAGE079
and
Figure 152700DEST_PATH_IMAGE081
permeability, k, of the first and second layer of medium, respectively1And k2Propagation constants of electromagnetic waves with first working frequency and electromagnetic waves with second working frequency in the first layer medium respectively are expressed as follows:
Figure 111429DEST_PATH_IMAGE083
and
Figure 907347DEST_PATH_IMAGE085
j is the imaginary unit, j2=-1;
Solving equations (1) to (3) of the nonlinear equation system by an iterative method to obtain the distance d between the interface of the medium layer and the transmitting coil and the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
In a second aspect, an embodiment of the present application provides an apparatus for remotely detecting a layer interface location and electromagnetic information, the apparatus comprising:
the first processing module is used for establishing a model of an axisymmetrically wound transmitting coil and a model of a non-axisymmetrically wound far detection fractional turn receiving coil which is coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the models of the transmitting coil and the receiving coil;
the second processing module is used for calculating the reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil;
the third processing module is used for calculating the total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle;
the fourth processing module is used for calculating the induced electromotive force of the receiving coil by adopting Gaussian integration according to the total electric field of the receiving coil;
and the fifth processing module is used for solving the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency by transmitting electromagnetic waves with different working frequencies according to the induced electromotive force, and solving the position and the electromagnetic information of the medium layer interface according to the amplitude and the phase angle of the induced electromotive force.
As a possible implementation, the model of the non-axisymmetrically wound far detecting fractional turn receive coil is represented as:
the discs on which the receiving coils are wound being divided intoN>An even number of sector areas passing through the center of a circle, wherein the serial numbers of the sector areas are arranged clockwise;
each turn of the receiving coil is divided intoN1 fractional sub-turn, each fractional sub-turn being wound in a sector, the fractional sub-turns of two adjacent sectors being wound in opposite directions, and the sectors being wound in opposite directionsNEmptying; each fractional sub-turn comprises a circumferential arc part and a radial straight line part, wherein the circumferential arc part is wound on the circumferential part of the sector area, and the radial straight line part is wound on the radial tangent plane part of the sector area passing through the center of a circle;
sector area 1 &N-1 fractional sub-turn ratios of the windings respectivelyn 1n N-1The ratio ofn iSatisfy the requirement of
Figure 660539DEST_PATH_IMAGE087
And is
Figure 479591DEST_PATH_IMAGE089
In the formulaiIs shown asiA sector-shaped area is formed by the circular arc-shaped area,n i representing a sector areaiThe number of the corresponding fractional turns is,Nthe number of the sector areas.
As a possible implementation, the eliminating, by the first processing module, the direct-coupled electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the model of the transmitting coil and the receiving coil includes:
the first processing submodule is used for enabling an electric field generated by a transmitting coil coaxial and parallel to a receiving coil in a uniform medium to be concentric in the plane where the remote detection receiving coil is located, all radial straight line parts of the receiving coil passing through the center of the concentric circle are perpendicular to the direction of the electric field, all circumferential arc parts are parallel to the direction of the electric field, according to the winding direction of the receiving coil, the integral result of the electric field along the receiving coil is 0, correspondingly, the induced electromotive force received by the receiving coil is 0, and the direct-coupled electromotive force generated by the transmitting coil to the receiving coil is eliminated.
As a possible implementation manner, in the second processing module, the calculating, according to the models of the receiving coil and the transmitting coil, the reflected field of the transmitting coil at the receiving coil by using a mirroring method includes determining a relationship between a mirror source of the transmitting coil and a real source, and the determining a relationship between a mirror source of the transmitting coil and a real source includes:
the second processing submodule is used for introducing a virtual mirror image transmitting coil which is in mirror symmetry with the transmitting coil in the first layer of medium into the second layer of medium in a medium model comprising at least two layers of media, naming the real transmitting coil as a real source, naming the mirror image transmitting coil as a mirror image source, and replacing the second layer of medium with the first layer of medium, so that the medium model is an axisymmetric model, wherein the relational expression between the mirror image source of the transmitting coil and the real source is as follows:
Figure 442343DEST_PATH_IMAGE090
in the formula (I), the compound is shown in the specification,I 2is the current of the mirror image source,I 1in order to be the current of the real source,
Figure 92767DEST_PATH_IMAGE091
is the reflection coefficient of the first layer medium and the second layer medium,
Figure 282440DEST_PATH_IMAGE091
is expressed as
Figure 651105DEST_PATH_IMAGE093
Figure 686057DEST_PATH_IMAGE095
Is the wave impedance in the first layer of medium,
Figure 394250DEST_PATH_IMAGE097
is the wave impedance in the second layer of medium, wherein,
Figure 754824DEST_PATH_IMAGE099
Figure 345205DEST_PATH_IMAGE101
Figure 387110DEST_PATH_IMAGE102
and
Figure 418652DEST_PATH_IMAGE103
the magnetic permeability of the first layer medium and the second layer medium respectively,
Figure 953057DEST_PATH_IMAGE104
and
Figure 233996DEST_PATH_IMAGE105
complex dielectric constants of the first layer medium and the second layer medium respectively, and the expression is
Figure 610751DEST_PATH_IMAGE107
Figure 90274DEST_PATH_IMAGE109
Wherein
Figure 792651DEST_PATH_IMAGE111
And
Figure 357624DEST_PATH_IMAGE113
the real parts of the dielectric constants, σ, of the first and second layers of medium1And σ2The electrical conductivity of the first layer of medium and the second layer of medium respectively,
Figure 741332DEST_PATH_IMAGE114
is the angular frequency of the electromagnetic wave, j is the imaginary unit, j2=-1。
As a possible implementation, the fifth processing module includes:
setting the distance between the layer interface and the transmitting coil to d meters, wherein the electromagnetic information of the medium layer interface comprises the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
Electromagnetic waves with at least two different working frequencies are transmitted by the transmitting coil, and the phase angle of induced electromotive force generated by the receiving coil is recorded as
Figure 340941DEST_PATH_IMAGE115
And
Figure 948640DEST_PATH_IMAGE116
the wavelength of the electromagnetic wave at the first operating frequency in the first layer of medium is
Figure 204172DEST_PATH_IMAGE117
The electromagnetic wave at the second working frequency has a wavelength in the first layer of medium
Figure 188308DEST_PATH_IMAGE118
Wherein, in the step (A),
Figure 642423DEST_PATH_IMAGE119
the first operating frequency is the wavelength in vacuum,
Figure 686603DEST_PATH_IMAGE120
Figure 957660DEST_PATH_IMAGE121
the relative permeability and the relative permittivity of the first layer of medium,
Figure 683170DEST_PATH_IMAGE122
a wavelength in vacuum for a second operating frequency;
the phase angle of the electromagnetic wave at the first operating frequency varying by 2 x d
Figure 991792DEST_PATH_IMAGE123
And the phase angle of the electromagnetic wave at the second operating frequency is changed to
Figure 941293DEST_PATH_IMAGE124
At the layer interface, the phase angle of the reflection coefficient at the first operating frequency is
Figure 233734DEST_PATH_IMAGE125
The phase angle of the reflection coefficient at the second operating frequency is
Figure 294094DEST_PATH_IMAGE126
The equations (1) to (3) are listed according to the variation rule of phase angle amplitude of the electromagnetic wave in the medium:
Figure 926064DEST_PATH_IMAGE127
in the equation (1),
Figure 46466DEST_PATH_IMAGE128
in the equation (2),
Figure 560624DEST_PATH_IMAGE129
in the equation (3),
in the formula (I), the compound is shown in the specification,
Figure 627938DEST_PATH_IMAGE130
presentation pair
Figure 176731DEST_PATH_IMAGE131
Taking a real part of the signal,
Figure 468035DEST_PATH_IMAGE132
presentation pair
Figure 398383DEST_PATH_IMAGE133
Taking a real part of the signal,real(V1) Is shown as pair V1Taking a real part of the signal,real(V2) Is shown as pair V2Taking the real part, V1Is an induced electromotive force of the receiving coil at a first operating frequency, V2The induced electromotive force of the receiving coil at the second operating frequency,
Figure 66124DEST_PATH_IMAGE134
Figure 672686DEST_PATH_IMAGE135
the reflection coefficients of the lower layer interface to the electromagnetic wave at the first working frequency and the second working frequency are respectively expressed as follows:
Figure 134892DEST_PATH_IMAGE137
Figure 623642DEST_PATH_IMAGE139
wherein
Figure 95074DEST_PATH_IMAGE141
Figure 290564DEST_PATH_IMAGE143
Figure 923670DEST_PATH_IMAGE145
Figure 899716DEST_PATH_IMAGE147
Figure 112523DEST_PATH_IMAGE149
Representing the complex permittivity of the first layer of dielectric at a first operating frequency,
Figure 959256DEST_PATH_IMAGE151
representing the complex permittivity of the first layer of dielectric at a second operating frequency,
Figure 28844DEST_PATH_IMAGE153
representing the complex permittivity of the second layer of dielectric at the first operating frequency,
Figure 961027DEST_PATH_IMAGE155
representing the complex permittivity of the second layer of dielectric at the second operating frequency,
Figure 36912DEST_PATH_IMAGE157
Figure 941414DEST_PATH_IMAGE159
is the real part of the dielectric constant, σ, of the first and second layers of medium1、σ2Is the electrical conductivity of the first layer of medium and the second layer of medium,
Figure 181903DEST_PATH_IMAGE160
Figure 601383DEST_PATH_IMAGE161
respectively the angular frequency of the first operating frequency and the angular frequency of the second operating frequency,
Figure 218309DEST_PATH_IMAGE163
and
Figure 39634DEST_PATH_IMAGE165
permeability, k, of the first and second layer of medium, respectively1And k2Propagation constants of electromagnetic waves with first working frequency and electromagnetic waves with second working frequency in the first layer medium respectively are expressed as follows:
Figure 654287DEST_PATH_IMAGE167
and
Figure 561063DEST_PATH_IMAGE169
j is the imaginary unit, j2=-1;
Solving equations (1) to (3) of the nonlinear equation system by an iterative method to obtain the distance d between the interface of the medium layer and the transmitting coil and the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
The embodiment of the application has the following beneficial effects:
according to the embodiment of the application, a model of a transmitting coil wound by a shaft symmetry is established, a model of a remote detection receiving coil wound by a non-shaft symmetry and coaxial and parallel with the transmitting coil is established, and based on the models of the transmitting coil and the receiving coil, direct coupling electromotive force generated by the transmitting coil to the receiving coil is eliminated according to the receiving coil; calculating a reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil; calculating a total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle; calculating the induced electromotive force of the receiving coil by adopting Gaussian integral according to the total electric field at the receiving coil; according to the induced electromotive force, by emitting electromagnetic waves with different working frequencies, the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency are solved, and according to the amplitude and the phase angle of the induced electromotive force, the position and the electromagnetic information of the medium layer interface are solved.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
FIG. 1 is a schematic flow chart diagram illustrating an embodiment of a method for remotely detecting layer interface position and electromagnetic information provided herein;
fig. 2 is a schematic model diagram of a non-axisymmetric remote detection receiver coil with N =4 in an embodiment of a method for remotely detecting a layer interface position and electromagnetic information provided in the present application;
FIG. 3 is a schematic diagram of a concentric electric field generated by a transmitting coil at a receiving coil in a homogeneous medium according to an embodiment of the method for remotely detecting layer interface position and electromagnetic information provided by the present application;
FIG. 4 is a schematic diagram of a conventional circular coil placed in an electric field;
FIG. 5 is a schematic diagram of a receiver coil placed in an electric field in an embodiment of a method for remotely detecting layer interface location and electromagnetic information provided herein;
FIG. 6a is a schematic diagram of an electric field at a receiver coil in the presence of a layer interface in an embodiment of a method for remotely detecting a position of a layer interface and electromagnetic information provided herein;
FIG. 6b is a diagram illustrating a directly coupled electric field background signal at a receiver coil in an embodiment of a method for remotely detecting layer interface position and electromagnetic information provided herein;
FIG. 6c is a diagram illustrating background signals of a reflected field at a receiver coil in an embodiment of a method for remotely detecting layer interface position and electromagnetic information provided herein;
FIG. 7 is a schematic view of a media model in an embodiment of a method for remotely detecting layer interface position and electromagnetic information provided herein;
FIG. 8 is a schematic view of a media model without consideration of a second layer of media in an embodiment of a method for remotely sensing layer interface location and electromagnetic information provided herein;
FIG. 9 is a schematic diagram of a model after a mirror image method is adopted when a second layer medium is considered in an embodiment of a method for remotely detecting layer interface position and electromagnetic information provided by the present application;
FIG. 10 is a schematic diagram of the variation of the induced electromotive force amplitude of the receiving coil and the distance between the layer interfaces in an embodiment of a method for remotely detecting the position and electromagnetic information of the layer interfaces provided in the present application;
FIG. 11 is a schematic diagram illustrating a phase angle of an induced electromotive force of a receiving coil and a distance change of a layer interface in an embodiment of a method for remotely detecting a position of the layer interface and electromagnetic information according to the present disclosure;
fig. 12 is a schematic structural diagram of an embodiment of a method for remotely detecting a layer interface location and electromagnetic information provided in the present application.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the technical solutions of the present invention will be described in detail by embodiments with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, "first", "second", "third", "fourth", "fifth", and the like are used only for distinguishing one from another, and do not indicate the degree of importance, the order, and the like thereof.
The division of the modules herein is merely a division of logical functions, and other divisions may be possible in actual implementation, for example, a plurality of modules may be combined or integrated in another system. Modules described as separate components may or may not be physically separate. Therefore, some or all of the modules can be selected according to actual needs to implement the scheme of the embodiment.
Referring to fig. 1-11, embodiments of the present application provide a method for remotely detecting layer interface position and electromagnetic information; as shown, the method mainly comprises:
establishing a model of an axisymmetrically wound transmitting coil and a model of a non-axisymmetrically wound far detection fractional turn receiving coil which is coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the models of the transmitting coil and the receiving coil;
calculating a reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil;
calculating a total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle;
calculating the induced electromotive force of the receiving coil by adopting Gaussian integral according to the total electric field at the receiving coil;
and according to the induced electromotive force, by transmitting electromagnetic waves with different working frequencies, solving the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency, and according to the amplitude and the phase angle of the induced electromotive force, solving the position and the electromagnetic information of the interface of the dielectric layer.
By adopting the method, the position and the electromagnetic information of the medium layer interface can be rapidly calculated, and the method is favorable for remote and efficient detection.
As a possible implementation, the model of the non-axisymmetrically wound far detecting fractional turn receive coil is represented as:
the discs on which the receiving coils are wound being divided intoN>An even number of sector areas passing through the center of a circle, wherein the serial numbers of the sector areas are arranged clockwise;Nis an even number;
each turn of the receiving coil is divided intoN1 fractional sub-turn, each fractional sub-turn being wound in a sector, the fractional sub-turns of two adjacent sectors being wound in opposite directions, and the sectors being wound in opposite directionsNEmptying; each fractional sub-turn comprises a circumferential arc part and a radial straight line part, wherein the circumferential arc part is wound on the circumferential part of the sector area, and the radial straight line part is wound on the radial tangent plane part of the sector area passing through the center of a circle;
sector area 1 &N-1 fractional sub-turn ratios of the windings respectivelyn 1n N-1The ratio ofn iSatisfy the requirement of
Figure 981680DEST_PATH_IMAGE171
And is
Figure 657512DEST_PATH_IMAGE173
In the formulaiIs shown asiA sector-shaped area is formed by the circular arc-shaped area,n i representing a sector areaiThe number of the corresponding fractional turns is,Nthe number of the sector areas.
As a possible implementation manner, the eliminating, according to the receiving coil, the direct-coupled electromotive force generated by the transmitting coil to the receiving coil based on the model of the transmitting coil and the receiving coil may include:
the electric field generated by the transmitting coil which is coaxial and parallel to the receiving coil in the uniform medium is a concentric circle on the plane where the remote detection receiving coil is located, all radial straight line parts of the receiving coil passing through the center of the concentric circle are perpendicular to the direction of the electric field, all circumferential arc parts are parallel to the direction of the electric field, according to the winding direction of the receiving coil, the integral result of the electric field along the receiving coil is 0, correspondingly, the induced electromotive force received by the receiving coil is 0, and the direct coupling electromotive force generated by the transmitting coil to the receiving coil is eliminated.
By adopting the method, the direct coupling electromotive force generated by the transmitting coil to the receiving coil can be completely eliminated, and the interference of the direct coupling signal to the reflected signal is avoided, so that the receiving coil can not effectively measure the reflected signal, and the electromagnetic information error of the layer interface is prevented from being larger.
In an electric field generated by a uniform field or a coaxial and parallel transmitting coil in a uniform medium, magnetic fluxes passing through N fan-shaped regions are equal, the induced electromotive force received by the receiving coil is 0 according to the winding direction of the receiving coil, and the direct-coupled electromotive force generated by the transmitting coil to the receiving coil is eliminated.
The integration result of the electric field along the receiving coil is explained as 0, as follows:
the induced electromotive force generated by the receiving coil is expressed as
Figure 443065DEST_PATH_IMAGE174
In the formulaEThe electric field strength at the receiver coil, as a vector,dlis the product of the receiving coilsIs divided into units of vectors whenEAnddlwhen the included angle of the directions is less than 90 degrees, the dot product result of the two is positive whenEAnddlwhen the included angle of the directions is larger than 90 degrees, the dot product result of the two is negative, and the induced electromotive force can be obtained by integrating one circle around the receiving coil.
FIG. 3 is a schematic diagram of a concentric electric field generated by a transmitting coil at a receiving coil in a homogeneous medium according to an embodiment of the method for remotely detecting layer interface position and electromagnetic information provided by the present application. Fig. 4 is a schematic view of a conventional circular coil placed in an electric field. As shown in the figure, the conventional circular receiving coil cannot eliminate the direct-coupled electromotive force because the direction of the concentric electric field is completely the same as the integral path of the circular coil, wherein the integral path is clockwise along the coil, and the electric field is positive along the coil integral result. Fig. 5 is a schematic diagram of a receiving coil placed in an electric field in an embodiment of a method for remotely detecting a layer interface position and electromagnetic information provided in the present application, where the electric field is integrated by 0 along the coil, where the linear portion of the receiving coil integrates: the electric field lines always being perpendicular to the linear part of the receiving coil, i.e.EAnddlthe included angle of the directions is 90 degrees, and the dot product integral result of the two directions is 0; integration of the arc part of the receiving coil: the coil circular arc part has clockwise and anticlockwise direction, and the electric field is positive along clockwise circular arc integral result, and is negative along anticlockwise circular arc integral result, because the number of turns when the coiling direction is for following the pointer and anticlockwise is the same, for example, 2 circles are coiled altogether clockwise to the coil, 2 circles are coiled altogether to the anticlockwise, and the integral result sum is 0.
As a possible implementation, in the calculating the reflected field of the transmitting coil at the receiving coil by using the mirror image method according to the model of the receiving coil and the transmitting coil, the determining a relationship between the mirror image source of the transmitting coil and the real source may include:
in a medium model comprising at least two layers of media, introducing a virtual mirror image transmitting coil which is in mirror symmetry with a transmitting coil in a first layer of media into a second layer of media, naming a real transmitting coil as a real source, naming the mirror image transmitting coil as a mirror image source, and replacing the second layer of media with the first layer of media, wherein the medium model is an axisymmetric model, and a relational expression between the mirror image source of the transmitting coil and the real source is as follows:
Figure 837137DEST_PATH_IMAGE175
in the formula (I), the compound is shown in the specification,I 2is the current of the mirror image source,I 1in order to be the current of the real source,
Figure 795866DEST_PATH_IMAGE176
is the reflection coefficient of the first layer medium and the second layer medium,
Figure 594713DEST_PATH_IMAGE176
is expressed as
Figure 285589DEST_PATH_IMAGE178
Wherein, in the step (A),
Figure 166957DEST_PATH_IMAGE180
is the wave impedance in the first layer of medium,
Figure 663798DEST_PATH_IMAGE182
is the wave impedance in the second layer of medium,
Figure 579801DEST_PATH_IMAGE184
Figure 503895DEST_PATH_IMAGE186
Figure 810242DEST_PATH_IMAGE187
and
Figure 845194DEST_PATH_IMAGE188
the magnetic permeability of the first layer medium and the second layer medium respectively,
Figure 615704DEST_PATH_IMAGE189
and
Figure 976278DEST_PATH_IMAGE190
complex dielectric constants of the first layer medium and the second layer medium respectively, and the expression is
Figure 769922DEST_PATH_IMAGE192
Figure 608565DEST_PATH_IMAGE194
Wherein
Figure 233581DEST_PATH_IMAGE196
And
Figure 762127DEST_PATH_IMAGE198
the real parts of the dielectric constants, σ, of the first and second layers of medium1And σ2The electrical conductivity of the first layer of medium and the second layer of medium respectively,
Figure 839805DEST_PATH_IMAGE199
is the angular frequency of the electromagnetic wave, j is the imaginary unit, j2=-1。
By adopting the method, the influence of the second layer medium on the medium model can be eliminated, so that the calculated model can adopt the fast algorithm of the axisymmetric model to realize fast and high-precision calculation of the reflection field, and the method is favorable for remote and efficient detection.
As a possible implementation, in the calculating the reflected field of the transmitting coil at the receiving coil by using the mirror image method, the calculation model used is as follows:
the relative dielectric constants of the first layer of medium and the second layer of medium are both 5, and the relative magnetic conductivities of the first layer of medium and the second layer of medium are both 1; the conductivity of the first layer of medium is 0.01S/m, and the conductivity of the second layer of medium is 0.5S/m; the coordinates of the circle center of the transmitting coil are (0, 0, 0), the coordinates of the circle center of the receiving coil are (0, 0, 0.05), the radiuses of the transmitting coil and the receiving coil are both 0.03m, the number of turns of the transmitting coil is 100, and the number of turns of the receiving coil is 50; the distance from the second layer interface to the z axis is gradually increased from 0.05m to 30 m; the transmitting coil current is 1A sine alternating current and the frequency is 100 kHz.
As a possible implementation, the calculating the total electric field generated by the transmitting coil at the receiving coil by using the field superposition principle includes: and calculating the total electric field generated by the real source and the mirror image source at the receiving coil by adopting a mirror image method by adopting a field superposition principle.
To be provided withNCoil model of =4, arc portion 0 toπThe calculation is performed by taking/2 as an example, as follows:
calculating induced electromotive force by Gaussian integration, and receiving induced electromotive force of coilVThe concrete expression is as follows:
Figure 419822DEST_PATH_IMAGE200
in the formula (I), the compound is shown in the specification,Eto receive the strength of the electric field at the coil,dlis an integration unit of the receiving coil,lfor the length of the receive coil, the above equation is converted to a function with respect to angle, resulting in:
Figure 899345DEST_PATH_IMAGE201
wherein
Figure 601721DEST_PATH_IMAGE202
For receiving coils at an angleθThe vector mode of the tangential component of the electric field strength,Rwhich is the radius of the coil,
by adopting the Gaussian transformation, the method has the advantages of simple operation,
Figure 166695DEST_PATH_IMAGE203
the transformed result is:
Figure 550403DEST_PATH_IMAGE204
Figure 884432DEST_PATH_IMAGE205
representing the field strength cut as an integrandVector modulo to the component;
Figure 757710DEST_PATH_IMAGE206
is an integral variable
Figure 809980DEST_PATH_IMAGE207
As a function of (a) or (b),
Figure 997379DEST_PATH_IMAGE208
namely the total electric field after superposition;
using gaussian integration yields:
Figure 185915DEST_PATH_IMAGE209
wherein
Figure 964515DEST_PATH_IMAGE210
Is a weight factor of the gaussian integral and,
Figure 784308DEST_PATH_IMAGE211
is a Gaussian point
Figure 509819DEST_PATH_IMAGE212
The vector mode of the tangential component of the electric field strength of (a), wherein the electric field at a gaussian point needs to be transformed to the electric field at the actual coordinates, i.e.
Figure 818440DEST_PATH_IMAGE213
Wherein
Figure 767942DEST_PATH_IMAGE214
Is a Gaussian point
Figure 60383DEST_PATH_IMAGE215
Corresponding to the coordinates of the sampling point at the actual receiving coil.
In the case of a layer interface in the vicinity of the coil, the layer interface reflects the electromagnetic wave generated by the transmitting coil, which electromagnetic wave is generated by a non-uniform and non-concentric circle with respect to the receiving coil, and therefore an induced electromotive force is generated in the coil. In the absence of a layer interface, the transmitting coil in the homogeneous medium generates a concentric electric field, as shown in fig. 3; when a layer interface exists, an electric field image at the receiving coil is as shown in fig. 6a, and fig. 6a is a schematic diagram of an electric field at the receiving coil when the layer interface exists in the embodiment of the method for remotely detecting the position of the layer interface and the electromagnetic information provided by the present application, that is, a schematic diagram of an electric field at the receiving coil obtained by using a field superposition principle; fig. 6b is a schematic diagram of a directly coupled electric field background signal at a receiving coil in an embodiment of a method for remotely detecting a layer interface location and electromagnetic information provided herein, fig. 6c is a schematic diagram of a reflected electric field background signal at a receiving coil in an embodiment of a method for remotely detecting a layer interface location and electromagnetic information provided herein, as shown in fig. 6a, 6b and 6c, fig. 6a is composed of fig. 6b and 6c, fig. 6b is a schematic diagram of a directly coupled electric field background signal at a receiving coil, independent of a layer interface, fig. 6c is a schematic diagram of a reflected electric field background signal at a receiving coil, dependent on a layer interface; wherein the direct coupling electric field is much larger than the reflection field, especially at larger layer distances, the direct coupling electric field is 1E4 times or even larger than the reflection field, and the reflection field is hardly detected if the direct coupling electric field is not eliminated. In order to accurately measure the layer interface information, a direct coupling field needs to be eliminated, which cannot be achieved by a traditional circular coil, and the receiving coil disclosed by the embodiment of the application can achieve the purpose of eliminating direct coupling electromotive force.
Specifically, the calculation of the reflected field of the transmitting coil at the receiving coil by using the mirror image method is described in detail as follows:
because the reflection field at the receiving coil is difficult to calculate due to the existence of the layer interface, the medium model is not an axisymmetric model any more, a three-dimensional numerical method is needed for solving, the calculation amount is huge, the calculation speed is low, the efficiency is low, and in order to calculate quickly, the mirror image method is adopted to solve the problem.
Referring to fig. 7-9, fig. 7 is a schematic diagram of a medium model in an embodiment of a method for remotely detecting a layer interface location and electromagnetic information provided in the present application, and fig. 8 is a schematic diagram of a method for remotely detecting a layer interface location and electromagnetic information provided in the present applicationFig. 9 is a model schematic diagram obtained after a mirror image method is adopted when the second layer medium is considered in the embodiment of the method for remotely detecting the interface position of the layer and the electromagnetic information provided by the present application. The idea of the mirror image method is to introduce a mirror image source in the second layer medium, the size of the mirror image source is equal to that of the transmitting coil, the mirror image source and the transmitting coil are symmetrical about the layer interface, and the relationship between the mirror image source and the transmitting coil is
Figure 120743DEST_PATH_IMAGE216
The second layer of medium can be transformed into the first layer of medium, and the medium model is changed from non-axisymmetric to axisymmetric, as shown in fig. 9. The schematic diagram of the field calculated after mirroring at the receiving coil is shown in fig. 6a, wherein the schematic diagram of the directly coupled electric field background signal of the transmitting coil at the receiving coil is shown in fig. 6b, the schematic diagram of the field background signal reflected by the mirror source at the receiving coil is shown in fig. 6c, and the schematic diagram of the resultant field is shown in fig. 6 a.
As a possible implementation manner, the solving of the amplitude and the phase angle of the induced electromotive force of the receiving coil at each operating frequency by emitting electromagnetic waves with different operating frequencies according to the induced electromotive force, and the solving of the position and the electromagnetic information of the dielectric layer interface according to the amplitude and the phase angle of the induced electromotive force includes:
setting the distance between the layer interface and the transmitting coil to d meters, wherein the electromagnetic information of the medium layer interface comprises the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
Electromagnetic waves with at least two different working frequencies are transmitted by the transmitting coil, and the phase angle of induced electromotive force generated by the receiving coil is recorded as
Figure 487133DEST_PATH_IMAGE217
And
Figure 873115DEST_PATH_IMAGE218
the wavelength of the electromagnetic wave at the first operating frequency in the first layer of medium is
Figure 121694DEST_PATH_IMAGE219
The electromagnetic wave at the second working frequency has a wavelength in the first layer of medium
Figure 251324DEST_PATH_IMAGE220
Wherein, in the step (A),
Figure 534538DEST_PATH_IMAGE221
the first operating frequency is the wavelength in vacuum,
Figure 29104DEST_PATH_IMAGE222
Figure 764979DEST_PATH_IMAGE223
the relative permeability and the relative permittivity of the first layer of medium,
Figure 695370DEST_PATH_IMAGE224
a wavelength in vacuum for a second operating frequency;
the phase angle of the electromagnetic wave at the first operating frequency varying by 2 x d
Figure 833090DEST_PATH_IMAGE225
And the phase angle of the electromagnetic wave at the second operating frequency is changed to
Figure 498558DEST_PATH_IMAGE226
At the layer interface, the phase angle of the reflection coefficient at the first operating frequency is
Figure 190571DEST_PATH_IMAGE227
The phase angle of the reflection coefficient at the second operating frequency is
Figure 130845DEST_PATH_IMAGE228
The equations (1) to (3) are listed according to the variation rule of phase angle amplitude of the electromagnetic wave in the medium:
Figure 326334DEST_PATH_IMAGE229
equation (1),
Figure 225020DEST_PATH_IMAGE230
In the equation (2),
Figure 201066DEST_PATH_IMAGE231
in the equation (3),
in the formula (I), the compound is shown in the specification,
Figure 945031DEST_PATH_IMAGE232
presentation pair
Figure 57344DEST_PATH_IMAGE233
Taking a real part of the signal,
Figure 64614DEST_PATH_IMAGE234
presentation pair
Figure 265307DEST_PATH_IMAGE235
Taking a real part of the signal,real(V1) Is shown as pair V1Taking a real part of the signal,real(V2) Is shown as pair V2Taking the real part, V1Is an induced electromotive force of the receiving coil at a first operating frequency, V2The induced electromotive force of the receiving coil at the second operating frequency,
Figure 78542DEST_PATH_IMAGE236
Figure 45361DEST_PATH_IMAGE237
the reflection coefficients of the lower layer interface to the electromagnetic wave at the first working frequency and the second working frequency are respectively expressed as follows:
Figure 489112DEST_PATH_IMAGE239
Figure 908592DEST_PATH_IMAGE241
wherein
Figure 525518DEST_PATH_IMAGE243
Figure 346843DEST_PATH_IMAGE245
Figure 758233DEST_PATH_IMAGE247
Figure DEST_PATH_IMAGE249
Figure DEST_PATH_IMAGE251
Representing the complex permittivity of the first layer of dielectric at a first operating frequency,
Figure DEST_PATH_IMAGE253
representing the complex permittivity of the first layer of dielectric at a second operating frequency,
Figure DEST_PATH_IMAGE255
representing the complex permittivity of the second layer of dielectric at the first operating frequency,
Figure DEST_PATH_IMAGE257
representing the complex permittivity of the second layer of dielectric at the second operating frequency,
Figure DEST_PATH_IMAGE259
Figure DEST_PATH_IMAGE261
is the real part of the dielectric constant, σ, of the first and second layers of medium1、σ2Is the electrical conductivity of the first layer of medium and the second layer of medium,
Figure 881654DEST_PATH_IMAGE262
Figure DEST_PATH_IMAGE263
respectively the angular frequency of the first operating frequency and the angular frequency of the second operating frequency,
Figure DEST_PATH_IMAGE265
and
Figure DEST_PATH_IMAGE267
permeability, k, of the first and second layer of medium, respectively1And k2Propagation constants of electromagnetic waves with first working frequency and electromagnetic waves with second working frequency in the first layer medium respectively are expressed as follows:
Figure DEST_PATH_IMAGE269
and
Figure DEST_PATH_IMAGE271
j is the imaginary unit, j2=-1;
Solving equations (1) to (3) of the nonlinear equation system by an iterative method to obtain the distance d between the interface of the medium layer and the transmitting coil and the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
The model used for the calculation is as follows: the relative dielectric constants of the first layer of medium and the second layer of medium are both 5, and the relative magnetic conductivities of the first layer of medium and the second layer of medium are both 1; the conductivity of the first layer of medium is 0.01S/m, and the conductivity of the second layer of medium is 0.5S/m; the coordinates of the circle center of the transmitting coil are (0, 0, 0), the coordinates of the circle center of the receiving coil are (0, 0, 0.05), the radiuses of the transmitting coil and the receiving coil are both 0.03m, the number of turns of the transmitting coil is 100, and the number of turns of the receiving coil is 50; the distance from the second layer interface to the z axis is 10 m; the transmitting coil current 1A is a sinusoidal alternating current with frequencies of 100kHz and 200 kHz. Calculating to obtain the induced electromotive force V under two working frequencies1=0.1716E-3+0.1848E-3iV and V2=0.3580E-3+0.1358E-3iV, the phase angle changes are
Figure 787424DEST_PATH_IMAGE272
=0.7485 and
Figure DEST_PATH_IMAGE273
and (5) =1.2083, and substituting equations (1), (2) and (3) to obtain a result.
Due to the adoption of the non-axisymmetrical receiving coil, the direct coupling electromotive force generated by the transmitting coil in the receiving coil is zero, and signals received by the receiving coil are all from reflected waves, so that the position of a layer interface and the dielectric conductivity can be calculated through the amplitude and the phase angle of the induced electromotive force. Fig. 10 is a schematic diagram of the amplitude of the induced electromotive force of the receiving coil and the distance change of the layer interface in an embodiment of a method for remotely detecting the position and the electromagnetic information of the layer interface provided in the present application, and as shown in the figure, the diagram is an image of the amplitude change of the induced electromotive force of the receiving coil when the distance from the layer interface to the z-axis is 0 to 30 m. Fig. 11 is a schematic diagram of a phase angle of an induced electromotive force of a receiving coil and a distance change of a layer interface in an embodiment of a method for remotely detecting a position of the layer interface and electromagnetic information provided in the present application, where in fig. 11, the distance from the layer interface to a z-axis is 0 to 30 m. It can be seen from fig. 10 that the amplitude of the induced electromotive force of the receiving coil gradually decreases as the layer interface distance increases, and at 30m, the amplitude of the single-turn receiving coil is about 1 e-6V, which can effectively identify the medium layer interface information; as can be seen from fig. 11, as the layer interface distance increases, the phase angle of the electromotive force induced in the receiver coil gradually decreases and then increases in the opposite direction, within 30m, the variation range is-pi/2, the medium interface information can be effectively identified through the phase angle variation, for electromagnetic fields with higher operating frequencies and higher dielectric resistivities, electromagnetic fields traveling over distances of 30m or more, reflected to the receiver coil, the phase difference exceeds 360 degrees, firstly, the attenuation condition of the electromagnetic field is judged according to the amplitude of the induced electromotive force generated by the receiving coil, the propagation distance of the electromagnetic wave is judged, an evaluation is made, if the propagation distance is greater than its wavelength in the medium, assuming that it is n times the wavelength in the medium, then n x 2 x pi is added to the phase of the induced electromotive force when solving for the changed phase.
Referring to fig. 12, an embodiment of the present application provides an apparatus for remotely detecting a layer interface position and electromagnetic information, as shown in the figure, the apparatus mainly includes:
the first processing module is used for establishing a model of an axisymmetrically wound transmitting coil and a model of a non-axisymmetrically wound far detection fractional turn receiving coil which is coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the models of the transmitting coil and the receiving coil;
the second processing module is used for calculating the reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil;
the third processing module is used for calculating the total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle;
the fourth processing module is used for calculating the induced electromotive force of the receiving coil by adopting Gaussian integration according to the total electric field of the receiving coil;
and the fifth processing module is used for solving the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency by transmitting electromagnetic waves with different working frequencies according to the induced electromotive force, and solving the position and the electromagnetic information of the medium layer interface according to the amplitude and the phase angle of the induced electromotive force.
As a possible implementation, the model of the non-axisymmetrically wound far detecting fractional turn receive coil is represented as:
the discs on which the receiving coils are wound being divided intoN>An even number of sector areas passing through the center of a circle, wherein the serial numbers of the sector areas are arranged clockwise;
each turn of the receiving coil is divided intoN1 fractional sub-turn, each fractional sub-turn being wound in a sector, the fractional sub-turns of two adjacent sectors being wound in opposite directions, and the sectors being wound in opposite directionsNEmptying; each fractional sub-turn comprises a circumferential arc part and a radial straight line part, wherein the circumferential arc part is wound on the circumferential part of the sector area, and the radial straight line part is wound on the radial tangent plane part of the sector area passing through the center of a circle;
sector area 1 &N-1 fractional sub-turn ratios of the windings respectivelyn 1n N-1The ratio ofn iSatisfy the requirement of
Figure DEST_PATH_IMAGE275
And is
Figure DEST_PATH_IMAGE277
In the formulaiIs shown asiA sector-shaped area is formed by the circular arc-shaped area,n i representing a sector areaiThe number of the corresponding fractional turns is,Nthe number of the sector areas.
As a possible implementation, the eliminating, by the receiving coil, the direct-coupled electromotive force generated by the transmitting coil to the receiving coil according to the model based on the transmitting coil and the receiving coil in the first processing module may include:
the first processing submodule is used for enabling an electric field generated by a transmitting coil coaxial and parallel to a receiving coil in a uniform medium to be concentric in the plane where the remote detection receiving coil is located, all radial straight line parts of the receiving coil passing through the center of the concentric circle are perpendicular to the direction of the electric field, all circumferential arc parts are parallel to the direction of the electric field, according to the winding direction of the receiving coil, the integral result of the electric field along the receiving coil is 0, correspondingly, the induced electromotive force received by the receiving coil is 0, and the direct-coupled electromotive force generated by the transmitting coil to the receiving coil is eliminated.
As a possible implementation, in the second processing module, the calculating, according to the model of the receiving coil and the transmitting coil, the reflected field of the transmitting coil at the receiving coil by using a mirroring method includes determining a relationship between a mirror source of the transmitting coil and a real source, and the determining a relationship between a mirror source of the transmitting coil and a real source may include:
the second processing submodule is used for introducing a virtual mirror image transmitting coil which is in mirror symmetry with the transmitting coil in the first layer of medium into the second layer of medium in a medium model comprising at least two layers of media, naming the real transmitting coil as a real source, naming the mirror image transmitting coil as a mirror image source, and replacing the second layer of medium with the first layer of medium, so that the medium model is an axisymmetric model, wherein the relational expression between the mirror image source of the transmitting coil and the real source is as follows:
Figure 400939DEST_PATH_IMAGE278
in the formula (I), the compound is shown in the specification,I 2is the current of the mirror image source,I 1in order to be the current of the real source,
Figure DEST_PATH_IMAGE279
is the reflection coefficient of the first layer medium and the second layer medium,
Figure 646545DEST_PATH_IMAGE279
is expressed as
Figure DEST_PATH_IMAGE281
Figure DEST_PATH_IMAGE283
Is the wave impedance in the first layer of medium,
Figure DEST_PATH_IMAGE285
is the wave impedance in the second layer of medium, wherein,
Figure DEST_PATH_IMAGE287
Figure DEST_PATH_IMAGE289
Figure 119246DEST_PATH_IMAGE290
and
Figure DEST_PATH_IMAGE291
the magnetic permeability of the first layer medium and the second layer medium respectively,
Figure 484499DEST_PATH_IMAGE292
and
Figure DEST_PATH_IMAGE293
complex dielectric constants of the first layer medium and the second layer medium respectively, and the expression is
Figure DEST_PATH_IMAGE295
Figure DEST_PATH_IMAGE297
Wherein
Figure DEST_PATH_IMAGE299
And
Figure DEST_PATH_IMAGE301
the real parts of the dielectric constants, σ, of the first and second layers of medium1And σ2The electrical conductivity of the first layer of medium and the second layer of medium respectively,
Figure 824957DEST_PATH_IMAGE302
is the angular frequency of the electromagnetic wave, j is the imaginary unit, j2=-1。
As a possible implementation manner, the solving of the amplitude and the phase angle of the induced electromotive force of the receiving coil at each operating frequency by emitting electromagnetic waves with different operating frequencies according to the induced electromotive force, and the solving of the position and the electromagnetic information of the dielectric layer interface according to the amplitude and the phase angle of the induced electromotive force includes:
setting the distance between the layer interface and the transmitting coil to d meters, wherein the electromagnetic information of the medium layer interface comprises the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
Electromagnetic waves with at least two different working frequencies are transmitted by the transmitting coil, and the phase angle of induced electromotive force generated by the receiving coil is recorded as
Figure DEST_PATH_IMAGE303
And
Figure 312570DEST_PATH_IMAGE304
the wavelength of the electromagnetic wave at the first operating frequency in the first layer of medium is
Figure DEST_PATH_IMAGE305
The electromagnetic wave at the second working frequency has a wavelength in the first layer of medium
Figure 131622DEST_PATH_IMAGE306
Wherein, in the step (A),
Figure DEST_PATH_IMAGE307
the first operating frequency is the wavelength in vacuum,
Figure 300566DEST_PATH_IMAGE308
Figure DEST_PATH_IMAGE309
the relative permeability and the relative permittivity of the first layer of medium,
Figure 888673DEST_PATH_IMAGE310
a wavelength in vacuum for a second operating frequency;
the phase angle of the electromagnetic wave at the first operating frequency varying by 2 x d
Figure DEST_PATH_IMAGE311
And the phase angle of the electromagnetic wave at the second operating frequency is changed to
Figure 281608DEST_PATH_IMAGE312
At the layer interface, the phase angle of the reflection coefficient at the first operating frequency is
Figure DEST_PATH_IMAGE313
The phase angle of the reflection coefficient at the second operating frequency is
Figure 325306DEST_PATH_IMAGE314
The equations (1) to (3) are listed according to the variation rule of phase angle amplitude of the electromagnetic wave in the medium:
Figure DEST_PATH_IMAGE315
in the equation (1),
Figure 94679DEST_PATH_IMAGE316
in the equation (2),
Figure DEST_PATH_IMAGE317
in the equation (3),
in the formula (I), the compound is shown in the specification,
Figure 537293DEST_PATH_IMAGE318
presentation pair
Figure DEST_PATH_IMAGE319
Taking a real part of the signal,
Figure 101130DEST_PATH_IMAGE320
presentation pair
Figure DEST_PATH_IMAGE321
Taking a real part of the signal,real(V1) Is shown as pair V1Taking a real part of the signal,real(V2) Is shown as pair V2Taking the real part, V1Is an induced electromotive force of the receiving coil at a first operating frequency, V2The induced electromotive force of the receiving coil at the second operating frequency,
Figure 629194DEST_PATH_IMAGE322
Figure DEST_PATH_IMAGE323
the reflection coefficients of the lower layer interface to the electromagnetic wave at the first working frequency and the second working frequency are respectively expressed as follows:
Figure DEST_PATH_IMAGE325
Figure DEST_PATH_IMAGE327
wherein
Figure DEST_PATH_IMAGE329
Figure DEST_PATH_IMAGE331
Figure DEST_PATH_IMAGE333
Figure DEST_PATH_IMAGE335
Figure DEST_PATH_IMAGE337
Representing the complex permittivity of the first layer of dielectric at a first operating frequency,
Figure DEST_PATH_IMAGE339
representing the complex permittivity of the first layer of dielectric at a second operating frequency,
Figure DEST_PATH_IMAGE341
representing the complex permittivity of the second layer of dielectric at the first operating frequency,
Figure DEST_PATH_IMAGE343
representing the complex permittivity of the second layer of dielectric at the second operating frequency,
Figure DEST_PATH_IMAGE345
Figure DEST_PATH_IMAGE347
is the real part of the dielectric constant, σ, of the first and second layers of medium1、σ2Is the electrical conductivity of the first layer of medium and the second layer of medium,
Figure 966372DEST_PATH_IMAGE348
Figure DEST_PATH_IMAGE349
respectively the angular frequency of the first operating frequency and the angular frequency of the second operating frequency,
Figure DEST_PATH_IMAGE351
and
Figure DEST_PATH_IMAGE353
permeability of first and second layer media respectively,k1And k2Propagation constants of electromagnetic waves with first working frequency and electromagnetic waves with second working frequency in the first layer medium respectively are expressed as follows:
Figure DEST_PATH_IMAGE355
and
Figure DEST_PATH_IMAGE357
j is the imaginary unit, j2=-1;
Solving equations (1) to (3) of the nonlinear equation system by an iterative method to obtain the distance d between the interface of the medium layer and the transmitting coil and the conductivity sigma of the first layer medium1And the electrical conductivity σ of the second layer medium2
The model used for the calculation is as follows: the relative dielectric constants of the first layer of medium and the second layer of medium are both 5, and the relative magnetic conductivities of the first layer of medium and the second layer of medium are both 1; the conductivity of the first layer of medium is 0.01S/m, and the conductivity of the second layer of medium is 0.5S/m; the coordinates of the circle center of the transmitting coil are (0, 0, 0), the coordinates of the circle center of the receiving coil are (0, 0, 0.05), the radiuses of the transmitting coil and the receiving coil are both 0.03m, the number of turns of the transmitting coil is 100, and the number of turns of the receiving coil is 50; the distance from the second layer interface to the z axis is 10 m; the transmitting coil current 1A is a sinusoidal alternating current with frequencies of 100kHz and 200 kHz. Calculating to obtain the induced electromotive force V under two working frequencies1=0.1716E-3+0.1848E-3iV and V2=0.3580E-3+0.1358E-3iV, the phase angle changes are
Figure 419086DEST_PATH_IMAGE358
=0.7485 and
Figure 684983DEST_PATH_IMAGE273
and (5) =1.2083, and substituting equations (1), (2) and (3) to obtain a result.
The foregoing is considered as illustrative of the preferred embodiments of the invention and the technical principles employed. It will be understood by those skilled in the art that the present application is not limited to the particular embodiments described herein, but is capable of various obvious changes, rearrangements and substitutions as will now become apparent to those skilled in the art without departing from the scope of the application. Therefore, although the present application has been described in more detail with reference to the above embodiments, the present application is not limited to the above embodiments, and may include other equivalent embodiments without departing from the spirit of the present application, and the scope of the present application is determined by the scope of the appended claims.

Claims (6)

1. A method for remotely detecting layer interface location and electromagnetic information, the method comprising:
establishing a model of an axisymmetrically wound transmitting coil and a model of a non-axisymmetrically wound far detection fractional turn receiving coil which is coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the models of the transmitting coil and the receiving coil;
calculating a reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil;
calculating a total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle;
calculating the induced electromotive force of the receiving coil by adopting Gaussian integral according to the total electric field at the receiving coil;
according to the induced electromotive force, by transmitting electromagnetic waves with different working frequencies, the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency are solved, and according to the amplitude and the phase angle of the induced electromotive force, the position and the electromagnetic information of the medium layer interface are solved;
wherein the model of the non-axisymmetrically wound far probe fractional turn receive coil is represented as:
the discs on which the receiving coils are wound being divided intoN>An even number of sector areas passing through the center of a circle, wherein the serial numbers of the sector areas are arranged clockwise;
each turn of the receiving coil is divided intoN1 fractional sub-turn, each fractional sub-turn being wound in a sector, the fractional sub-turns of two adjacent sectors being wound in opposite directions, and the sectors being wound in opposite directionsNEmptying; each fractional sub-turn comprises a circumferential arc part and a radial straight line part, wherein the circumferential arc part is wound on the circumferential part of the sector area, and the radial straight line part is wound on the radial tangent plane part of the sector area passing through the center of a circle;
sector area 1 &N-1 fractional sub-turn ratios of the windings respectivelyn 1n N-1The ratio ofn i Satisfy the requirement of
Figure DEST_PATH_IMAGE001
And is
Figure 490917DEST_PATH_IMAGE002
In the formulaiIs shown asiA sector-shaped area is formed by the circular arc-shaped area,n i representing a sector areaiThe number of the corresponding fractional turns is,Nthe number of the sector areas;
wherein, in the calculating the reflected field of the transmitting coil at the receiving coil by adopting the mirror image method according to the models of the receiving coil and the transmitting coil, the determining the relationship between the mirror image source of the transmitting coil and the real source comprises:
in a medium model comprising at least two layers of media, introducing a virtual mirror image transmitting coil which is in mirror symmetry with a transmitting coil in a first layer of media into a second layer of media, naming a real transmitting coil as a real source, naming the mirror image transmitting coil as a mirror image source, and replacing the second layer of media with the first layer of media, wherein the medium model is an axisymmetric model, and a relational expression between the mirror image source of the transmitting coil and the real source is as follows:
Figure DEST_PATH_IMAGE003
in the formula (I), the compound is shown in the specification,I 2is the current of the mirror image source,I 1in order to be the current of the real source,
Figure 218177DEST_PATH_IMAGE004
is the reflection coefficient of the first layer medium and the second layer medium,
Figure 466756DEST_PATH_IMAGE004
is expressed as
Figure DEST_PATH_IMAGE005
Figure 268490DEST_PATH_IMAGE006
Is the wave impedance in the first layer of medium,
Figure DEST_PATH_IMAGE007
is the wave impedance in the second layer of medium, wherein,
Figure 614021DEST_PATH_IMAGE008
Figure DEST_PATH_IMAGE009
Figure 843008DEST_PATH_IMAGE010
and
Figure DEST_PATH_IMAGE011
the magnetic permeability of the first layer medium and the second layer medium respectively,
Figure 578883DEST_PATH_IMAGE012
and
Figure DEST_PATH_IMAGE013
complex dielectric constants of the first layer medium and the second layer medium respectively, and the expression is
Figure 184308DEST_PATH_IMAGE014
Figure DEST_PATH_IMAGE015
Wherein
Figure 132147DEST_PATH_IMAGE016
And
Figure DEST_PATH_IMAGE017
the real parts of the dielectric constants of the first layer medium and the second layer medium respectively,
Figure 718987DEST_PATH_IMAGE018
and
Figure DEST_PATH_IMAGE019
the electrical conductivity of the first layer of medium and the second layer of medium respectively,
Figure 286365DEST_PATH_IMAGE020
is the angular frequency of the electromagnetic wave, j is the imaginary unit, j2=-1。
2. The method of claim 1, wherein the eliminating, from the receive coil, the direct-coupled electromotive force generated by the transmit coil to the receive coil based on the model of the transmit coil and the receive coil comprises:
the electric field generated by the transmitting coil which is coaxial and parallel to the receiving coil in the uniform medium is a concentric circle on the plane where the remote detection receiving coil is located, all radial straight line parts of the receiving coil passing through the center of the concentric circle are perpendicular to the direction of the electric field, all circumferential arc parts are parallel to the direction of the electric field, according to the winding direction of the receiving coil, the integral result of the electric field along the receiving coil is 0, correspondingly, the induced electromotive force received by the receiving coil is 0, and the direct coupling electromotive force generated by the transmitting coil to the receiving coil is eliminated.
3. The method of claim 1, wherein the solving for the magnitude and phase angle of the induced electromotive force of the receiving coil at each operating frequency by emitting electromagnetic waves of different operating frequencies based on the induced electromotive force, and the solving for the position and electromagnetic information of the dielectric layer interface based on the magnitude and phase angle of the induced electromotive force comprises:
setting the distance between the layer interface and the transmitting coil as d meters, wherein the electromagnetic information of the medium layer interface comprises the conductivity of the first layer medium
Figure DEST_PATH_IMAGE021
And the electrical conductivity of the second layer medium
Figure 492219DEST_PATH_IMAGE022
Electromagnetic waves with at least two different working frequencies are transmitted by the transmitting coil, and the phase angle of induced electromotive force generated by the receiving coil is recorded as
Figure DEST_PATH_IMAGE023
And
Figure 77921DEST_PATH_IMAGE024
the wavelength of the electromagnetic wave at the first operating frequency in the first layer of medium is
Figure DEST_PATH_IMAGE025
The electromagnetic wave at the second working frequency has a wavelength in the first layer of medium
Figure 320814DEST_PATH_IMAGE026
Wherein, in the step (A),
Figure DEST_PATH_IMAGE027
the first operating frequency is the wavelength in vacuum,
Figure 624757DEST_PATH_IMAGE028
Figure DEST_PATH_IMAGE029
the relative permeability and the relative permittivity of the first layer of medium,
Figure 712930DEST_PATH_IMAGE030
a wavelength in vacuum for a second operating frequency;
the phase angle of the electromagnetic wave at the first operating frequency varying by 2 x d
Figure DEST_PATH_IMAGE031
And the phase angle of the electromagnetic wave at the second operating frequency is changed to
Figure 949876DEST_PATH_IMAGE032
At the layer interface, the phase angle of the reflection coefficient at the first operating frequency is
Figure DEST_PATH_IMAGE033
The phase angle of the reflection coefficient at the second operating frequency is
Figure 106881DEST_PATH_IMAGE034
The equations (1) to (3) are listed according to the variation rule of phase angle amplitude of the electromagnetic wave in the medium:
Figure DEST_PATH_IMAGE035
in the equation (1),
Figure 304644DEST_PATH_IMAGE036
in the equation (2),
Figure DEST_PATH_IMAGE037
in the equation (3),
in the formula (I), the compound is shown in the specification,
Figure 445775DEST_PATH_IMAGE038
presentation pair
Figure DEST_PATH_IMAGE039
Taking a real part of the signal,
Figure 756802DEST_PATH_IMAGE040
presentation pair
Figure DEST_PATH_IMAGE041
Taking a real part of the signal,real(V1) Is shown as pair V1Taking a real part of the signal,real(V2) Is shown as pair V2Taking the real part, V1Is an induced electromotive force of the receiving coil at a first operating frequency, V2The induced electromotive force of the receiving coil at the second operating frequency,
Figure 590766DEST_PATH_IMAGE042
Figure DEST_PATH_IMAGE043
the reflection coefficients of the lower layer interface to the electromagnetic wave at the first working frequency and the second working frequency are respectively expressed as follows:
Figure 354454DEST_PATH_IMAGE044
Figure DEST_PATH_IMAGE045
wherein
Figure 299276DEST_PATH_IMAGE046
Figure DEST_PATH_IMAGE047
Figure 58284DEST_PATH_IMAGE048
Figure DEST_PATH_IMAGE049
Figure 469674DEST_PATH_IMAGE050
Indicating a first operating frequencyThe complex dielectric constant of the first layer of dielectric at a rate,
Figure DEST_PATH_IMAGE051
representing the complex permittivity of the first layer of dielectric at a second operating frequency,
Figure 717728DEST_PATH_IMAGE052
representing the complex permittivity of the second layer of dielectric at the first operating frequency,
Figure DEST_PATH_IMAGE053
representing the complex permittivity of the second layer of dielectric at the second operating frequency,
Figure 731821DEST_PATH_IMAGE054
Figure DEST_PATH_IMAGE055
is the real part of the dielectric constant of the first layer medium and the second layer medium,
Figure 17440DEST_PATH_IMAGE056
Figure DEST_PATH_IMAGE057
is the electrical conductivity of the first layer of medium and the second layer of medium,
Figure 193206DEST_PATH_IMAGE058
Figure DEST_PATH_IMAGE059
respectively the angular frequency of the first operating frequency and the angular frequency of the second operating frequency,
Figure 931486DEST_PATH_IMAGE060
and
Figure DEST_PATH_IMAGE061
of a first and second layer of medium respectivelyMagnetic permeability, k1And k2Propagation constants of electromagnetic waves with first working frequency and electromagnetic waves with second working frequency in the first layer medium respectively are expressed as follows:
Figure 624636DEST_PATH_IMAGE062
and
Figure DEST_PATH_IMAGE063
j is the imaginary unit, j2=-1;
Solving equations (1) to (3) of the nonlinear equation system by an iterative method to obtain the distance d between the interface of the medium layer and the transmitting coil and the conductivity of the first layer of medium
Figure 748450DEST_PATH_IMAGE064
And the electrical conductivity of the second layer medium
Figure 32800DEST_PATH_IMAGE057
4. An apparatus for remotely sensing layer interface position and electromagnetic information, the apparatus comprising:
the first processing module is used for establishing a model of an axisymmetrically wound transmitting coil and a model of a non-axisymmetrically wound far detection fractional turn receiving coil which is coaxial and parallel to the transmitting coil, and eliminating direct coupling electromotive force generated by the transmitting coil to the receiving coil according to the receiving coil based on the models of the transmitting coil and the receiving coil;
the second processing module is used for calculating the reflection field of the transmitting coil at the receiving coil by adopting a mirror image method according to the models of the receiving coil and the transmitting coil;
the third processing module is used for calculating the total electric field generated by the transmitting coil at the receiving coil according to the calculated reflection field by adopting a field superposition principle;
the fourth processing module is used for calculating the induced electromotive force of the receiving coil by adopting Gaussian integration according to the total electric field of the receiving coil;
the fifth processing module is used for solving the amplitude and the phase angle of the induced electromotive force of the receiving coil under each working frequency by transmitting electromagnetic waves with different working frequencies according to the induced electromotive force, and solving the position and the electromagnetic information of the interface of the medium layer according to the amplitude and the phase angle of the induced electromotive force;
wherein the model of the non-axisymmetrically wound far probe fractional turn receive coil is represented as:
the discs on which the receiving coils are wound being divided intoN>An even number of sector areas passing through the center of a circle, wherein the serial numbers of the sector areas are arranged clockwise;
each turn of the receiving coil is divided intoN1 fractional sub-turn, each fractional sub-turn being wound in a sector, the fractional sub-turns of two adjacent sectors being wound in opposite directions, and the sectors being wound in opposite directionsNEmptying; each fractional sub-turn comprises a circumferential arc part and a radial straight line part, wherein the circumferential arc part is wound on the circumferential part of the sector area, and the radial straight line part is wound on the radial tangent plane part of the sector area passing through the center of a circle;
sector area 1 &N-1 fractional sub-turn ratios of the windings respectivelyn 1n N-1The ratio ofn i Satisfy the requirement of
Figure DEST_PATH_IMAGE065
And is
Figure 258376DEST_PATH_IMAGE066
In the formulaiIs shown asiA sector-shaped area is formed by the circular arc-shaped area,n i representing a sector areaiThe number of the corresponding fractional turns is,Nthe number of the sector areas;
in the second processing module, the calculating, according to the models of the receiving coil and the transmitting coil, the reflected field of the transmitting coil at the receiving coil by using a mirror image method includes determining a relationship between a mirror image source of the transmitting coil and a real source, and the determining a relationship between the mirror image source of the transmitting coil and the real source includes:
the second processing submodule is used for introducing a virtual mirror image transmitting coil which is in mirror symmetry with the transmitting coil in the first layer of medium into the second layer of medium in a medium model comprising at least two layers of media, naming the real transmitting coil as a real source, naming the mirror image transmitting coil as a mirror image source, and replacing the second layer of medium with the first layer of medium, so that the medium model is an axisymmetric model, wherein the relational expression between the mirror image source of the transmitting coil and the real source is as follows:
Figure DEST_PATH_IMAGE067
in the formula (I), the compound is shown in the specification,I 2is the current of the mirror image source,I 1in order to be the current of the real source,
Figure 879851DEST_PATH_IMAGE068
is the reflection coefficient of the first layer medium and the second layer medium,
Figure 530275DEST_PATH_IMAGE068
is expressed as
Figure DEST_PATH_IMAGE069
Figure 530067DEST_PATH_IMAGE070
Is the wave impedance in the first layer of medium,
Figure DEST_PATH_IMAGE071
is the wave impedance in the second layer of medium, wherein,
Figure 23366DEST_PATH_IMAGE072
Figure DEST_PATH_IMAGE073
Figure 402525DEST_PATH_IMAGE074
and
Figure DEST_PATH_IMAGE075
the magnetic permeability of the first layer medium and the second layer medium respectively,
Figure 766511DEST_PATH_IMAGE076
and
Figure DEST_PATH_IMAGE077
complex dielectric constants of the first layer medium and the second layer medium respectively, and the expression is
Figure 940134DEST_PATH_IMAGE078
Figure DEST_PATH_IMAGE079
Wherein
Figure 858412DEST_PATH_IMAGE080
And
Figure DEST_PATH_IMAGE081
the real parts of the dielectric constants of the first layer medium and the second layer medium respectively,
Figure 572421DEST_PATH_IMAGE082
and
Figure DEST_PATH_IMAGE083
the electrical conductivity of the first layer of medium and the second layer of medium respectively,
Figure 525333DEST_PATH_IMAGE084
is the angular frequency of the electromagnetic wave, j is the imaginary unit, j2=-1。
5. The apparatus of claim 4, wherein the model based on the transmit coil and the receive coil in the first processing module for canceling direct-coupled electromotive force generated by the transmit coil to the receive coil according to the receive coil comprises:
the first processing submodule is used for enabling an electric field generated by a transmitting coil coaxial and parallel to a receiving coil in a uniform medium to be concentric in the plane where the remote detection receiving coil is located, all radial straight line parts of the receiving coil passing through the center of the concentric circle are perpendicular to the direction of the electric field, all circumferential arc parts are parallel to the direction of the electric field, according to the winding direction of the receiving coil, the integral result of the electric field along the receiving coil is 0, correspondingly, the induced electromotive force received by the receiving coil is 0, and the direct-coupled electromotive force generated by the transmitting coil to the receiving coil is eliminated.
6. The apparatus of claim 4, wherein the fifth processing module comprises:
setting the distance between the layer interface and the transmitting coil as d meters, wherein the electromagnetic information of the medium layer interface comprises the conductivity of the first layer medium
Figure DEST_PATH_IMAGE085
And the electrical conductivity of the second layer medium
Figure 132508DEST_PATH_IMAGE086
Electromagnetic waves with at least two different working frequencies are transmitted by the transmitting coil, and the phase angle of induced electromotive force generated by the receiving coil is recorded as
Figure 210185DEST_PATH_IMAGE088
And
Figure 977153DEST_PATH_IMAGE090
the wavelength of the electromagnetic wave at the first operating frequency in the first layer of medium is
Figure DEST_PATH_IMAGE091
The electromagnetic wave at the second working frequency has a wavelength in the first layer of medium
Figure 800883DEST_PATH_IMAGE092
Wherein, in the step (A),
Figure DEST_PATH_IMAGE093
the first operating frequency is the wavelength in vacuum,
Figure 831156DEST_PATH_IMAGE094
Figure DEST_PATH_IMAGE095
the relative permeability and the relative permittivity of the first layer of medium,
Figure 396130DEST_PATH_IMAGE096
a wavelength in vacuum for a second operating frequency;
the phase angle of the electromagnetic wave at the first operating frequency varying by 2 x d
Figure DEST_PATH_IMAGE097
And the phase angle of the electromagnetic wave at the second operating frequency is changed to
Figure 920783DEST_PATH_IMAGE098
At the layer interface, the phase angle of the reflection coefficient at the first operating frequency is
Figure DEST_PATH_IMAGE099
The phase angle of the reflection coefficient at the second operating frequency is
Figure 379446DEST_PATH_IMAGE100
The equations (1) to (3) are listed according to the variation rule of phase angle amplitude of the electromagnetic wave in the medium:
Figure DEST_PATH_IMAGE101
in the equation (1),
Figure 331353DEST_PATH_IMAGE102
in the equation (2),
Figure DEST_PATH_IMAGE103
in the equation (3),
in the formula (I), the compound is shown in the specification,
Figure 977098DEST_PATH_IMAGE104
presentation pair
Figure DEST_PATH_IMAGE105
Taking a real part of the signal,
Figure 695655DEST_PATH_IMAGE106
presentation pair
Figure DEST_PATH_IMAGE107
Taking a real part of the signal,real(V1) Is shown as pair V1Taking a real part of the signal,real(V2) Is shown as pair V2Taking the real part, V1Is an induced electromotive force of the receiving coil at a first operating frequency, V2The induced electromotive force of the receiving coil at the second operating frequency,
Figure 502767DEST_PATH_IMAGE108
Figure DEST_PATH_IMAGE109
the reflection coefficients of the lower layer interface to the electromagnetic wave at the first working frequency and the second working frequency are respectively expressed as follows:
Figure 406001DEST_PATH_IMAGE110
Figure DEST_PATH_IMAGE111
wherein
Figure 289775DEST_PATH_IMAGE112
Figure DEST_PATH_IMAGE113
Figure 812023DEST_PATH_IMAGE114
Figure DEST_PATH_IMAGE115
Figure 714120DEST_PATH_IMAGE116
Representing the complex permittivity of the first layer of dielectric at a first operating frequency,
Figure DEST_PATH_IMAGE117
representing the complex permittivity of the first layer of dielectric at a second operating frequency,
Figure 7829DEST_PATH_IMAGE118
representing the complex permittivity of the second layer of dielectric at the first operating frequency,
Figure DEST_PATH_IMAGE119
representing the complex permittivity of the second layer of dielectric at the second operating frequency,
Figure 893745DEST_PATH_IMAGE120
Figure DEST_PATH_IMAGE121
is the real part of the dielectric constant of the first layer medium and the second layer medium,
Figure 563892DEST_PATH_IMAGE122
Figure DEST_PATH_IMAGE123
is a first layer medium and a second layer mediumThe electrical conductivity of the layer medium,
Figure 727020DEST_PATH_IMAGE124
Figure DEST_PATH_IMAGE125
respectively the angular frequency of the first operating frequency and the angular frequency of the second operating frequency,
Figure 440899DEST_PATH_IMAGE126
and
Figure DEST_PATH_IMAGE127
permeability, k, of the first and second layer of medium, respectively1And k2Propagation constants of electromagnetic waves with first working frequency and electromagnetic waves with second working frequency in the first layer medium respectively are expressed as follows:
Figure 296335DEST_PATH_IMAGE128
and
Figure DEST_PATH_IMAGE129
j is the imaginary unit, j2=-1;
Solving equations (1) to (3) of the nonlinear equation system by an iterative method to obtain the distance d between the interface of the medium layer and the transmitting coil and the conductivity of the first layer of medium
Figure 285019DEST_PATH_IMAGE130
And the electrical conductivity of the second layer medium
Figure DEST_PATH_IMAGE131
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