CN217467206U - Three-component measurement system for magnetic source ground-air transient electromagnetism - Google Patents
Three-component measurement system for magnetic source ground-air transient electromagnetism Download PDFInfo
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Abstract
The utility model belongs to the technical field of magnetic source ground-to-air transient electromagnetism measurement, especially, relate to a magnetic source ground-to-air transient electromagnetism three-component measurement system, magnetic source ground-to-air transient electromagnetism three-component measurement system includes magnetic source transmitting system, three-component aerial receiving system and synchronization system, magnetic source transmitting system is used for in the primary magnetic field of ground transmission, arouse the underground object body to produce secondary induction magnetic field, three-component aerial receiving system is used for measuring the three-component response that magnetic source transmitting system arouses the secondary induction magnetic field that the underground object body produced, synchronization system is used for carrying out the time service and location to three-component aerial receiving system. The utility model discloses realize the quick collection of three-component transient electromagnetic data to utilize the director to rectify raw data, obtain the three-component data of normalization.
Description
Technical Field
The utility model belongs to the technical field of magnetic source ground-to-air transient electromagnetism measurement, especially, relate to a three component measurement system of magnetic source ground-to-air transient electromagnetism.
Background
In a gully in a mountainous area with complex terrain, the vegetation is dense, the conventional ground geophysical method is limited by complex terrain conditions, the construction is difficult, the data acquisition period is long, and the actual requirements of quickly and reliably detecting an underground structure at present cannot be met, so that the development of an air-ground transient electromagnetic detection method and technical research is very necessary. The ground-air transient electromagnetic method is a semi-aviation transient electromagnetic device form which transmits and receives in the air on the ground, is a rapid exploration method developed in recent years, has the characteristics of large exploration depth and high data quality, and is mainly applied to the fields of coal fields, engineering exploration and the like at present. Researches show that the ground-air transient electromagnetic method has great application potential in the fields of mineral products, oil gas and geological disasters. However, the starting time of China in the field of aeronautical geodetic physics is late, the equipment is backward, the system is limited by the equipment level of a flight platform, and the geodetic transient electromagnetic detection system in China is still imperfect.
The ground-air transient electromagnetic detection system based on the unmanned aerial vehicle utilizes a transmitting system to transmit on the ground, and carries a receiver and a sensor on the rotor unmanned aerial vehicle to implement measurement. The existing air-core coil transient electromagnetic sensor for aerial collection can only measure a vertical component, but a single component has defects in detection of a complex target body, cannot reflect the boundary of the target body clearly, and cannot meet the actual requirement.
The conventional ground-to-air transient electromagnetic method is that the electromagnetic wave is transmitted on the ground through a grounding electric source, and only a vertical component transient response is received by an air receiving system. In areas with poor grounding conditions such as desert and gobi, the problem of grounding resistance of an electrical transmission grounding source is difficult to deal with, and large current is difficult to supply by transmission current. In addition, saline-alkali earth surface shells exist in some areas, the phenomenon that power supply current runs along the earth surface can occur, and the expected purpose cannot be achieved. On the other hand, the single-component transient response in the receiving system is not reflected clearly to the boundary of the target geologic body. In actual measurement in the field, the three-component coil can rotate in the air, wherein the vertical (Z) component probe has no influence on data acquisition by the rotation of the probe. However, when measuring the horizontal (X, Y) component, the rotation of the coil itself in the air can make the measurement data influence greatly. Therefore, it is necessary to perform rotation angle correction on the horizontal component (X, Y) horizontal component.
The utility model provides a three measuring system of magnetism source ground-air transient electromagnetism and measuring method utilizes ungrounded magnetism return wire source to pass through return wire transmission frame at ground transmission, carries on the transient electromagnetism three-component response that receiver and three-component sensor based on the director arouses at aerial measurement ground transmission system through rotor unmanned aerial vehicle, acquires the information of richer target geologic body.
SUMMERY OF THE UTILITY MODEL
The utility model provides a three measuring system of magnetic source ground-air transient electromagnetism, aim at realize three-component transient electromagnetism data and gather fast to utilize the director to rectify raw data, obtain the three-component data of normalization.
In order to achieve the above object, the utility model adopts the following technical scheme:
a magnetic source ground-air transient electromagnetic three-component measurement system comprises a magnetic source transmitting system, a three-component air receiving system and a synchronization system;
the magnetic source emission system comprises an emitter, a rectifier, a generator and an emission frame, wherein one end of the rectifier is connected with the generator, the other end of the rectifier is connected with the emitter, and the emitter is connected with two joints of the emission frame through a binding post; the magnetic source emission system is used for emitting a primary magnetic field on the ground to excite an underground target body to generate a secondary induction magnetic field;
the three-component aerial receiving system comprises an unmanned aerial vehicle and a carrying platform arranged below the unmanned aerial vehicle, wherein a receiver is arranged on the carrying platform, the lower part of the carrying platform is connected with a three-component sensor through a lifting rope, and the receiver is connected with the three-component sensor through an induction coil connecting wire; the three-component aerial receiving system is used for measuring the three-component response of a secondary induction magnetic field generated by the excitation of the underground target body by the magnetic source transmitting system;
the synchronization system is used for timing and positioning the three-component air receiving system.
Further, the synchronization system comprises a GPS synchronization device arranged on the unmanned aerial vehicle, and the GPS synchronization device is respectively connected with the transmitter and the receiver.
Furthermore, the three-component sensor comprises two coil transverse supports corresponding to the X-axis direction and the Y-axis direction, two coil vertical supports corresponding to the Z-axis direction, three hollow coils corresponding to Z, X, Y and an orientator corresponding to the horizontal component, wherein the coil transverse supports are connected with the coil vertical supports and are perpendicular to each other in pairs, the hollow coils are connected with the coil transverse supports and the coil vertical supports to form a spherical structure, the hollow coils are connected to a receiver through induction coil connecting wires respectively, and the orientator is arranged at the intersection position of the coil transverse supports and the coil vertical supports.
Further, the initial direction of the director is aligned with the X component coil normal axis and perpendicular to the Y component coil normal axis.
Further, the outside of induction coil connecting wire wraps up shielded cable.
A magnetic source ground-space transient electromagnetic three-component measurement method comprises the following steps:
s1, arranging a return wire emission source on the ground; transmitting a primary field to the underground by using a magnetic source transmitting system to generate a secondary field;
s2, preparing a three-component aerial receiving system, measuring three-component response of a secondary induction magnetic field generated by exciting an underground target body by a magnetic source transmitting system through a three-component sensor, and orienting X, Y horizontal component measured data through an orienting device to provide a basis for subsequent data correction;
s3, the unmanned aerial vehicle of the three-component air receiving system takes off and flies to a specified line measuring end point to start working, simultaneously measuring three-component response of a secondary field and data of a director, only recording a secondary field signal after the measurement is switched off, and performing continuous measurement and synchronization through a synchronization system;
and S4, after each measuring point is measured in sequence, correcting the three-component data of the actually measured secondary field according to the orientation data actually measured by the orientation device to obtain corrected three-component data.
Further, in step S3, the flying speed of the unmanned aerial vehicle does not exceed 5m/S, and the flying height is below 50 meters.
Further, in step S3, the measurement is performed with the coil normal direction set perpendicular to the ground as the Z component and the coil normal direction set as the X component in the flight direction, and the Y component is determined again according to the right-handed screw rule.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model discloses an unmanned aerial vehicle carries on receiver and three-component sensor, three-component sensor includes two coil horizontal braces corresponding to X axle and Y axle direction, erect the support corresponding to the coil of Z axle direction, corresponding to the hollow coil of Z, X, Y three component and the director corresponding to horizontal component, the coil horizontal brace erects the support with the coil and is connected and two liang of perpendicular, hollow coil erects the leg joint with the coil through erecting the leg joint with the coil horizontal brace and constitutes spherical structure, hollow coil is connected to the receiver through the induction coil connecting wire respectively, the director sets up in the crossing position that the support was erect with the coil to the coil horizontal brace. The utility model discloses can fly fast and measure the measurement station, realize the quick collection of three-component transient electromagnetic data to utilize the director on the three-component sensor to rectify original data, obtain normalized three-component data, the center and the boundary reaction of data measured to the abnormal body are more sensitive, reliable for current single component coil, and the three-component data after the correction are more accurate.
Drawings
FIG. 1 is a schematic overall structure diagram of a magnetic source ground-air transient electromagnetic three-component measurement system;
fig. 2 is a schematic structural diagram of a three-component sensor of a magnetic source ground-air transient electromagnetic three-component measurement system.
Wherein: 1-unmanned plane; 2-carrying a platform; 3-a receiver; 4-lifting a rope; 5-a GPS synchronizer; 6-connecting the induction coil; 7-a shielded cable; 8-coil horizontal support; 9-coil vertical support; 10-air core coil; 11-director.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
As shown in fig. 1 and fig. 2, a magnetic source ground-to-air transient electromagnetic three-component measurement system includes a magnetic source transmitting system, a three-component air receiving system, and a synchronization system.
The magnetic source emission system is used for emitting a primary magnetic field on the ground to excite an underground target body to generate a secondary induction magnetic field. The magnetic source emission system comprises a transmitter, a rectifier, a generator and an emission frame. One end of the rectifier is connected with the generator, the other end of the rectifier is connected with the transmitter, and the transmitter is connected with two joints of the transmitting frame through special binding posts. The generator is used for generating 220V alternating-current voltage, the alternating-current voltage is converted into direct-current voltage through the rectifier, the converted direct-current voltage is converted into bipolar square waves with the duty ratio of 50% through the transmitter, the bipolar square waves are transmitted through the transmitting frame, and a primary field is generated in the underground medium and then excited to generate a secondary field.
The three-component aerial receiving system is used for measuring the three-component response of a secondary induction magnetic field generated by a subsurface target body. The three-component aerial receiving system comprises an unmanned aerial vehicle 1 and a carrying platform 2 arranged below the unmanned aerial vehicle, wherein a receiver 3 is arranged on the carrying platform 2, and a three-component sensor is connected below the carrying platform 2 through a lifting rope 4; the receiver 3 is connected with the GPS synchronizer 5 through a GPS connecting wire, the receiver 3 is connected with the three-component sensor through an induction coil connecting wire 6, and the outside of the induction coil connecting wire 6 is wrapped with a shielding cable 7. The carrying platform 2 is used for carrying the receiver 3 and the suspension three-component sensor to realize rapid flight measurement; the receiver 3 mainly functions to receive the secondary field signals of the three-component sensor.
The three-component sensor comprises two coil transverse supports 8 corresponding to an X axis and a Y axis, three coil vertical supports 9 and Z, X, Y corresponding to a Z axis, hollow coils 10 of three components and a director 11 of a horizontal component, wherein the coil transverse supports 8 are connected with the coil vertical supports 9 and are perpendicular to each other in pairs, the hollow coils 10 are connected with the coil vertical supports 9 through the coil transverse supports 8 to form a spherical structure, the hollow coils 10 are connected to a receiver 3 through induction coil connecting wires 6 respectively, and the director 11 is arranged at the intersection positions of the coil transverse supports 8 and the coil vertical supports 9. The three-component sensor is used to measure the three-component secondary field signal and the orientation function of the orienter 11 is used to correct the horizontal component signal, where the initial direction of the orienter 11 is coincident with the X-component coil normal axis and perpendicular to the Y-component coil normal axis.
The synchronizing system comprises a GPS synchronizing device 5 arranged on the unmanned aerial vehicle, the GPS synchronizing device 5 is respectively connected with the transmitter and the receiver 3, and the functions of the synchronizing system are mainly time service and positioning.
A magnetic source ground-air transient electromagnetic three-component measurement method comprises the following steps:
s1, arranging a return wire emission source on the ground; transmitting a primary field to the underground by using a magnetic source transmitting system to generate a secondary field;
s2, preparing a three-component aerial receiving system, measuring three-component response of a secondary induction magnetic field generated by exciting an underground target body by a magnetic source transmitting system through a three-component sensor, and orienting X, Y horizontal component measured data through an orienting device to provide a basis for subsequent data correction;
s3, the unmanned aerial vehicle of the three-component air receiving system takes off and flies to a specified line measuring end point to start working, simultaneously measuring three-component response of a secondary field and data of a director, only recording a secondary field signal after the measurement is switched off, and performing continuous measurement and synchronization through a synchronization system;
and S4, after each measuring point is measured in sequence, correcting the three-component data of the actually measured secondary field according to the orientation data actually measured by the orientation device to obtain corrected three-component data.
The following uses the three-component measurement system of the transient electromagnetism in the air-ground of the magnetic source to detect the irregular massive metal ore body buried several hundred meters deep underground as an example to the utility model discloses it is right to further explain in detail:
s1, arranging a loop emitting source on the ground, wherein the side length of an emitting frame is 200-800 m, the emitting current is more than 10A, and the emitting fundamental frequency is less than 25 Hz;
s2, transmitting a primary field to the underground by using a magnetic source transmitting system according to the set transmitting parameters, and exciting the underground metal ore body to generate a secondary field;
s3, assembling a three-component aerial receiving system, setting a Z component generally in a manner that the normal direction of a coil is vertical to the ground, setting an X component in the normal direction of the coil along the flight direction, and determining the Y air volume according to the right-hand spiral criterion; the flying speed of the unmanned aerial vehicle does not exceed 5m/s, and the flying height is below 50 meters, so that high-quality signals can be received better.
And S4, only recording the secondary field signals after being switched off by measurement, and setting the number of times of measurement superposition not to exceed 128 times. The measurement mode is continuous measurement, GPS synchronization, initial point number is set to be 0001, and the point number is automatically added with 1.
And S5, simultaneously measuring the secondary field responses of the three components and the orientation data of the director by using the three-component air receiving system.
And S6, storing the three-component data and the director data after multiple times of superposition as a data measurement result of one point in a 0001 point number.
And S7, continuing flight measurement, and sequentially storing the data of the subsequent measuring points in point numbers of 0002, 0003 … … … and the like.
And S8, after the flight measurement is finished, transmitting the three-component data back to the computer, processing the three-component data in corresponding data processing software, and correcting the three-component data point by point according to the data of the direction finder to obtain the corrected three-component data.
And S9, inverting the corrected three-component data to obtain a more accurate and reliable interpretation result.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise forms disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical application, to thereby enable others skilled in the art to best understand the invention for and with the various embodiments. The present invention is limited only by the claims and their full scope and equivalents.
Claims (5)
1. A three-component measurement system for ground-to-air transient electromagnetism of a magnetic source is characterized in that: the system comprises a magnetic source transmitting system, a three-component air receiving system and a synchronizing system;
the magnetic source transmitting system comprises a transmitter, a rectifier, a generator and a transmitting frame, wherein one end of the rectifier is connected with the generator, the other end of the rectifier is connected with the transmitter, and the transmitter is connected with two joints of the transmitting frame through a binding post; the magnetic source emission system is used for emitting a primary magnetic field on the ground to excite an underground target body to generate a secondary induction magnetic field;
the three-component aerial receiving system comprises an unmanned aerial vehicle (1) and a carrying platform (2) arranged below the unmanned aerial vehicle (1), wherein a receiver (3) is arranged on the carrying platform (2), the lower part of the carrying platform (2) is connected with a three-component sensor through a lifting rope (4), and the receiver (3) is connected with the three-component sensor through an induction coil connecting wire (6); the three-component aerial receiving system is used for measuring three-component response of a secondary induction magnetic field generated by exciting an underground target body by the magnetic source transmitting system;
the synchronous system is used for carrying out time service and positioning on the three-component air receiving system.
2. The system for measuring three components of electromagnetic field transient of ground-air of magnetic source according to claim 1, characterized in that: the synchronous system comprises a GPS (global positioning system) synchronous device (5) arranged on the unmanned aerial vehicle (1), the GPS synchronous device (5) is respectively connected with a transmitter and a receiver (3), and the synchronous system is used for time service and positioning.
3. The system for measuring three components of electromagnetic field transient of ground-air of magnetic source according to claim 2, characterized in that: the three-component sensor comprises two coil transverse supports (8) corresponding to the X-axis direction and the Y-axis direction, coil vertical supports (9) corresponding to the Z-axis direction, hollow coils (10) corresponding to Z, X, Y three components and orientation devices (11) corresponding to horizontal components, wherein the coil transverse supports (8) and the coil vertical supports (9) are connected and are pairwise perpendicular to each other, the hollow coils (10) are connected with the coil vertical supports (8) and the coil vertical supports (9) to form a spherical structure, the hollow coils (10) are connected to the receiver (3) through induction coil connecting wires (6) respectively, and the orientation devices (11) are arranged at the intersection positions of the coil transverse supports (8) and the coil vertical supports (9).
4. The system for measuring the three components of the ground-to-air transient electromagnetic field of the magnetic source according to claim 3, is characterized in that: the initial direction of the orientator is consistent with the normal axis of the X-component coil and is vertical to the normal axis of the Y-component coil.
5. The system for measuring the three components of the transient electromagnetic field in the ground and air of the magnetic source according to claim 4, is characterized in that: and the outer side of the induction coil connecting wire (6) is wrapped with a shielding cable (7).
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