WO2020115519A1 - Sonde destinée à être partiellement introduite dans un sol depuis un véhicule volant, ensemble et procédé associés - Google Patents

Sonde destinée à être partiellement introduite dans un sol depuis un véhicule volant, ensemble et procédé associés Download PDF

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Publication number
WO2020115519A1
WO2020115519A1 PCT/IB2018/001634 IB2018001634W WO2020115519A1 WO 2020115519 A1 WO2020115519 A1 WO 2020115519A1 IB 2018001634 W IB2018001634 W IB 2018001634W WO 2020115519 A1 WO2020115519 A1 WO 2020115519A1
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WO
WIPO (PCT)
Prior art keywords
probe
ground
longitudinal
compartment
emitter
Prior art date
Application number
PCT/IB2018/001634
Other languages
English (en)
Inventor
Ihme SAMI
Jokelainen KIMMO
Original Assignee
Total Sa
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Total Sa filed Critical Total Sa
Priority to PCT/IB2018/001634 priority Critical patent/WO2020115519A1/fr
Publication of WO2020115519A1 publication Critical patent/WO2020115519A1/fr

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V1/00—Seismology; Seismic or acoustic prospecting or detecting
    • G01V1/16—Receiving elements for seismic signals; Arrangements or adaptations of receiving elements
    • G01V1/168—Deployment of receiver elements
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V1/00—Seismology; Seismic or acoustic prospecting or detecting
    • G01V1/16—Receiving elements for seismic signals; Arrangements or adaptations of receiving elements
    • G01V1/162—Details
    • G01V1/166—Arrangements for coupling receivers to the ground
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V1/00—Seismology; Seismic or acoustic prospecting or detecting
    • G01V1/16—Receiving elements for seismic signals; Arrangements or adaptations of receiving elements
    • G01V1/18—Receiving elements, e.g. seismometer, geophone or torque detectors, for localised single point measurements
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V1/00—Seismology; Seismic or acoustic prospecting or detecting
    • G01V1/22—Transmitting seismic signals to recording or processing apparatus

Definitions

  • the present invention concerns a probe extending according to a longitudinal axis, intended to be partially introduced into a ground from a flying vehicle, to carry out measurements in the ground, the probe having at least an end to be placed in contact with the ground, the probe comprising:
  • the closed housing at least a sensor received in the closed housing, the sensor being able to sense a physical quantity related to the ground;
  • the emitter being able to send data representative of the physical quantity sensed by the sensor
  • the power source being able to power the sensor and/or the emitter.
  • the probe is intended to be partially introduced into a ground through its own velocity, mass and deceleration thereupon its impact with said ground from the flying vehicle.
  • Each probe is in particular intended to form a receiver including at least a seismic sensor to conduct a geophysical survey in a region of interest.
  • the region of interest is notably a region with a difficult access.
  • the region in particular comprises a high density of vegetation, such as a forest, such as a tropical forest.
  • the region may comprise rugged terrain such as hills (for example foothills), cliffs and/or mountains.
  • the region may comprise dangerous to access areas, such as areas with unexploded ordinances (UXO’s).
  • the probe can also be used in any region of interest.
  • Geophysical measurements obtained during such a survey are critical in building a sub-surface earth image representative of the particular geology in the region of interest, in particular to determine the location of potential reservoirs of oil and gas.
  • Such a geophysical survey is for example conducted by placing an array of seismic sources into the ground in the region of interest and by deploying seismic sensors able to record reflections of seismic signals produced by the successive sources on the different layers of the earth.
  • the survey generally requires implanting the sources at various locations, and partially introducing receivers in the ground along several lines to create a dense array of receivers.
  • the quality of the image obtained after the survey is generally a function of the surface density of sources and/or of receivers.
  • a significant number of receivers have to be put in place in the ground to obtain an image of good quality. This is in particular the case when a three-dimensional image is required.
  • the set-up of the receivers and/or the sources in the ground is a long process which often requires drilling the ground, and in the case of the receivers, ensuring that the coupling between the receiver and the ground is adequate.
  • This kind of geophysical survey requires numerous receivers, i.e. several ten of thousands, to be introduced in the ground by dropping from the flying vehicle.
  • One aim of the invention is to provide a probe for conducting a seismic survey which is resistant, especially to resist to the impact with the ground when dropped from the flying vehicle, easy to manufacture and cost-effective.
  • the subject-matter of the invention is a probe of the above-mentioned type, wherein the closed housing comprises at least one inner compartment and at least one outer compartment surrounding at least partially the inner compartment, the hollow casing comprising at least two assembled longitudinal parts, the at least two longitudinal parts defining the inner compartment and the outer compartment.
  • the probe according to the invention may comprise one or more of the following features, taken solely or according to any potential technical combination:
  • the inner compartment and/or the outer compartment is airtight and/or watertight;
  • the longitudinal parts are assembled along a contact plane, the contact plane extending according to the longitudinal axis or an axis parallel to the longitudinal axis;
  • the hollow casing comprises a first and a second assembled longitudinal half parts, the two longitudinal half parts defining the inner compartment and the outer compartment;
  • each longitudinal half part comprises at least two first walls extending in a direction parallel to the longitudinal axis and at least two second walls extending in a direction perpendicular to the longitudinal axis, the first walls and the second walls of each longitudinal half part forming the inner compartment;
  • the inner compartment and/or the outer compartment contain at least one of the sensor, the emitter and/or the power source;
  • the outer compartment is filed with a material intended to ballast the probe
  • the power source is a fuel cell and the outer compartment defines a reservoir for receiving an oxidizing agent or a reducing agent;
  • the outer compartment defines a water reservoir and the probe further comprises at least one collecting cup in fluidic communication with the outer compartment, the collecting cup being intended to collect water from a rainfall or from dew;
  • the emitter comprises an antenna and the longitudinal parts define a compartment for receiving the antenna
  • the longitudinal parts are biodegradable and/or chemically degradable
  • the probe further comprising a fixing device intended to be removably fixed to a launching unit of the flying vehicle.
  • the invention further concerns a ground survey assembly comprising:
  • launching unit able to separate the probe from the flying vehicle above the ground.
  • the flying vehicle is an unmanned aerial vehicle.
  • the invention further concerns a method for surveying a ground, comprising the following steps:
  • the invention also relates to a method for manufacturing a probe as described above, the probe comprising forming a hollow casing defining a closed housing receiving:
  • the senor being able to sense a physical quantity related to the ground
  • the emitter being able to send data representative of the physical quantity sensed by the sensor, - at least a power source, the power source being able to power the sensor and/or the emitter,
  • the method for manufacturing according to the invention may comprise one or more of the following features, taken solely or according to any potential technical combination:
  • the method comprises providing a first and a second longitudinal half parts and assembling said half parts to define at least one inner compartment and at least one outer compartment surrounding the inner compartment in the closed housing,
  • the method comprises a step for obtaining the first longitudinal part and the second longitudinal part by injection molding of plastic,
  • the method comprises, before the assembling step, inserting in the inner compartment or in the outer compartment at least one of the sensor, the emitter, and/or the power source,
  • FIG. 1 is a schematic view of a region of interest comprising a ground survey assembly according to the invention
  • FIG. 2 is an exploded view of a probe according to the invention.
  • figure 3 is longitudinal section of the probe of figure 2, taken along a median plane;
  • FIG. 4 is a schematic perspective view of a probe according to another embodiment of the invention.
  • FIG. 5 is a longitudinal section of a probe according to another embodiment of the invention.
  • FIG. 6 is a longitudinal section of a probe, partially introduced in the ground, according to another embodiment of the invention.
  • a first ground survey assembly 10 comprising at least a probe 12 according to the invention is disclosed schematically in figure 1.
  • the ground survey assembly 10 is for carrying out a geophysical survey of an onshore region of interest 14, schematically shown in figure 1.
  • the assembly 10 is used in particular to collect geophysical data and measurements for determining the physical properties of the subsurface 13 located in the region of interest and/or for building an image of the geology of the subsurface 13, preferably a tridimensional image of the subsurface 13.
  • the region of interest 14 is for example a region having an uneven terrain 16.
  • the uneven terrain 16 in particular comprises hills, mountains, cliffs or any type of rugged terrain.
  • the region of interest 14 is for example located on foothills which are difficult to access.
  • the region of interest 14 further comprises vegetation 18.
  • the vegetation 18 is for example a forest, in particular a tropical forest. It comprises a high density of vegetation, for example trees 20 forming a canopy 22 which covers a majority of the surface of the ground in the region of interest 14.
  • the subsurface 13 located below the ground comprises layers of geological formation and potentially oil and gas reservoirs.
  • the vegetation 18 defines a plurality of natural and/or artificial clearings 24 offering an access to the ground through openings in the canopy 22.
  • the vegetation 18 in the region of interest 14 also defines sky holes 26 in the canopy 22.
  • the clearings 24 are spread in the region of interest 14, at a distance generally comprised between 100 m and 500 m, preferentially around 300 m, taken along the line of sight between two adjacent clearings 24.
  • the clearings 24 generally have a surface area greater than 25 m 2 , at the ground level and generally greater than 900 m 2 at the top of the canopy 22.
  • the seismic sources 30 can be put in place in the clearings 24.
  • a clearing 24 is for example defined in a OGP Standard“OGP-Helicopter Guideline for Land Seismic and Helirig operations - Report 420 version 1.1 June 2013
  • Sky holes 26 are generally natural. They advantageously form a vertical“light tube” between the canopy 22 and the ground.
  • the sky holes 26 have a minimal surface area greater than 1 m 2 , preferentially greater than 3 m2, and comprised for example between 3 m 2 and 20 m 2 .
  • the probes 12 are able to be dropped in each sky hole 26, as will be described later.
  • At least a sky hole 26 has a surface area which is smaller than the surface area of the clearings 24.
  • the ground survey assembly 10 comprises a plurality of sources 30, able to generate a geophysical stimulus in the ground, in particular a seismic signal.
  • the ground survey assembly 10 further comprises a plurality of at least partially biodegradable probes 12 spread in the region of interest 14 to collect geophysical data arising from the seismic signal generated by the sources 30.
  • the ground survey assembly 10 further comprises a fleet of flying vehicles 32, able to fly above the vegetation 18 to carry each probe 12 above its point of installation, and, for each flying vehicle 32, a launching unit 34 able to separate each probe 12 carried by the flying vehicle 32 to let the probe 12 free fall to its installation point in the ground.
  • the probe 12 can be launched toward the ground.
  • the launching impulse can be obtained by the integration of a thruster (ex: pyrotechnic, turbine, propeller%) in the probe 12, or by the use of a propulsion mechanism onboard the probe carrier flying vehicle 32 (e.g. launching actuator or the decompression of a spring).
  • the impulse accelerates the fall of the probe 12 to help it penetrate further into the canopy 22 and / or the ground.
  • the fall of the probe 12 can be slowed down by a braking mechanism (e.g. a parachute attached to the rear part 64). Slowing down the fall of the probe 12 can for instance avoid damages to the probe.
  • a braking mechanism e.g. a parachute attached to the rear part 64. Slowing down the fall of the probe 12 can for instance avoid damages to the probe.
  • the ground survey assembly 10 further comprises at least a base 36 (or secondary camp), comprising at least a collection and/or analysis unit 38 and a telecommunication system 40 able to transfer data measured by the probes 12 to the collection and/or analysis unit 38, and from the collection and/or analysis unit 38 to an external station (not shown).
  • a base 36 or secondary camp
  • a collection and/or analysis unit 38 and a telecommunication system 40 able to transfer data measured by the probes 12 to the collection and/or analysis unit 38, and from the collection and/or analysis unit 38 to an external station (not shown).
  • the base 36 advantageously comprises a helipad, night facilities for crews, and/or antenna for collecting data. It is used for management of the take-off and landing. It may be used for first aid (e.g. medevac).
  • first aid e.g. medevac
  • the external station may be located at a main camp (not shown).
  • the main camp advantageously comprises facilities for collecting data, as well as a main computing unit, and/or a control center.
  • the ground survey assembly 10 comprises at least an additional flying vehicle 42 such as a helicopter, an airship, able to fly over the vegetation to carry the sources 30 in the clearings 24.
  • an additional flying vehicle 42 such as a helicopter, an airship, able to fly over the vegetation to carry the sources 30 in the clearings 24.
  • Each seismic source 30 is able to generate a controlled seismic energy generating a geophysical stimulus, in particular a seismic signal in the ground.
  • the source 30 for example may comprise an explosive, in particular dynamite, able to generate the geophysical stimulus.
  • the source 30 is inserted in a hole drilled into the ground, for example at a depth comprised between 0 meter and 100 meters, preferably between 5 meters and 80 meters.
  • the source 30 comprises a mechanical device such as a hammer, a vibrator.
  • the density of sources 30 locations laid in the region of interest 14 is generally comprised between 10 source locations per km 2 and 100 source locations per km 2 .
  • Each source location can comprise one or more source 30.
  • Each source 30 is preferably arranged in a clearing 24.
  • the source 30 is generally brought to the clearing 24 by the additional flying vehicle 42. It can be put in place by a unmanned ground vehicle, such as a semi-automatic drilling platform.
  • Each probe 12 is partially introduced in the ground to sense in particular the seismic signals resulting from interactions of the seismic stimulus generated by a source 30 with the geology of the subsurface 13.
  • the density of probes 12 is comprised for example between 10 probes per km 2 and 1000 probes per km 2 , in particular between 300 probes per km 2 and 500 probes per km 2 , notably 400 probes per km 2 .
  • each probe 12 has the shape of a dart extending along a longitudinal axis L.
  • the probe 12 has the shape of a ball or of a parallel pipe.
  • the probe 12 comprises a hollow casing 50 defining a closed housing 52, at least a sensor unit 54 comprising at least one sensor 54A received in the closed housing 52 to sense at least a physical quantity related to the ground, in particular a seismic signal.
  • the probe 12 further comprises an emitter 56 able to collect and send data representative of the physical quantity sensed by the sensor unit 54, and at least a power source 58 able to power the sensor unit 54 and/or the emitter 56.
  • the emitter 56 and the power source 58 are also received in the closed housing 52 of the hollow casing 50.
  • the hollow casing 50 advantageously comprises a tapered lower end 60 to penetrate the ground, a central tubular partition 62, and a rear part 64 mounted at the rear of the central partition 62 opposite from the tapered lower end 60.
  • the tapered lower end 60 comprises a profiled wall 66 defining an inner cavity 68, and advantageously, a needle-shaped solid end part 70 protruding from the profiled wall 66.
  • the inner cavity 68 may comprise reinforcing elements for reinforcing the tapered lower end 60 when it is impacted on the ground.
  • the inner cavity 68 contains the sensor unit 54 including the or each sensor 54A.
  • the tubular central partition 62 is here cylindrical.
  • the central partition 62 defines an outer surface 73A defining an outer surface of the probe 12 intended to be in contact with a mass of air in which the probe 12 falls from the flying vehicle 32. It also defines an inner surface 73B externally delimiting the closed housing 52.
  • the rear part 64 comprises a least a radially protruding fly control member 76, which provide guidance to the probe 12 when it free falls from the flying vehicle 32.
  • the rear part 64 further comprises a fixing device 77 intended to be removably fixed to a launching unit 34 of the flying vehicle 32.
  • the fixing device 77 is a ring as shown in figure 2.
  • the fixing device 77 is a hook.
  • the fixing device is a metal part or a magnet able to be fixed to the drone using an electromagnet acting as a retainer, deactivation of said electromagnet releases the dart.
  • the hollow casing 50 comprises at least two assembled longitudinal parts 78.
  • the hollow casing 50 comprises two assembled longitudinal half parts 78.
  • the closed housing 52 comprises an inner compartment 80 and an outer compartment 82 surrounding partially the inner compartment 80.
  • the two longitudinal half parts 78 define the inner compartment 80 and the outer compartment 82.
  • Each longitudinal half part 78 comprises at least two first walls 84 extending in a direction parallel to the longitudinal axis L and at least two second walls 86 extending in a direction perpendicular to the longitudinal axis L.
  • each half part 78 defines the inner compartment 80, when the half parts 78 are assembled.
  • Each longitudinal half 78 part is obtained by injection molding of plastic.
  • the longitudinal half parts 78 are similar and obtained by injection molding using the same mold.
  • the longitudinal half parts 78 are biodegradable and/or chemically degradable.
  • biodegradable it is meant that the longitudinal half parts 78 are made of a material which is able to be mineralized by soil microorganisms and or by air microorganisms.
  • a biodegradable material is a material in which more than 90% of the material is converted into carbon dioxide and water by the actions of microorganisms within two years, preferably within one year, more preferably within six months.
  • Biodegradability can be measured for example according to standard ASTM D5988-12 whose title is“Standard test methods for determining aerobic biodegradation of plastic materials in soil”.
  • chemically degradable it is meant that the longitudinal half parts 78 are made of a material which is able to be mineralized by chemical reactions with components of the soil and/or with light, in particular with UV light.
  • a chemically degradable material is a material in which more than 90% of the material loses its structure within two years, preferably within one year, more preferably within six months.
  • the biodegradable material and/or chemically degradable material is degraded in less than within 2 years, preferably within one year, more preferably within 6 months after the contact of the probe 12 with the ground.
  • the longitudinal half parts 78 are made of biodegradable plastic.
  • Biodegradable plastics are for example components which are derived from renewable raw materials.
  • biodegradable plastics are aliphatic polyesters, such as polyhydroxyalkanoates (PHA), like poly-3-hydroxybutyrate (PHB), polyhydroxyvalerate (PHV), and polyhydroxyhexanoate (PHH).
  • PHA polyhydroxyalkanoates
  • PBS polybutenesuccinate
  • PCL polycaprolactone
  • the longitudinal half parts 78 are assembled along a contact plane P.
  • the contact plane P extends according to the longitudinal axis L.
  • the longitudinal half parts 78 are ultrasonic welded. This method for fixing the longitudinal half parts 78 is particularly advantageous since it does not require any external material such as a glue to fix the half parts 78. Ultrasonic welding is fast and ensures a strong fixing between the half parts 78 which resists to the impact with the ground.
  • the longitudinal half parts 78 are for example fixed by bonding.
  • a cyanoacrylate glue is used.
  • the longitudinal half parts 78 are intended not to be disassembled.
  • the inner compartment 80 and the outer compartment 82 are air tight and/or watertight.
  • only one of the inner compartment 80 and of the outer compartment 82 is air tight or water tight.
  • the inner compartment 80 contains the sensor unit 54, the emitter 56 and the power source 58.
  • the sensor unit 54, the emitter 56 and the power source 58 are protected against moisture and rain when the probe 12 is dropped from the flying vehicle 32 and introduced in the ground.
  • the outer compartment 82 is for example filled with a material intended to ballast the probe 12.
  • the material is sand or water.
  • the center of gravity of the probe 12 is located closer to the tapered lower end 60 than to the rear part 64.
  • the sensor unit 54 comprises at least a geophysical sensor 54A such as a geophone or a microelectromechanical system (MEMS) sensor.
  • a geophysical sensor 54A such as a geophone or a microelectromechanical system (MEMS) sensor.
  • MEMS microelectromechanical system
  • the sensor unit 54 comprises at least an accelerometer, and/or a thermometer.
  • the sensor unit 54 advantageously comprises at least one geophone, in particular three geophones and/or an accelerometer.
  • Each sensor 54A of the sensor unit 54 is able to sense a physical quantity, in particular a ground movement and to convert it into a signal which may be recorded.
  • the emitter 56 comprises a data recovery unit able to digitalize, process and store the data measured by each sensor 54A.
  • the emitter 56 for example comprises a processor and a memory.
  • the emitter 56 is able to communicate with another emitter 56 of another probe 12 located in the vicinity of the probe 12 and/or with an antenna of the telecommunication system 40. It is able to transfer data representative of the physical quantity measured by each sensor 54A along time to another probe 12 and/or to an antenna of the telecommunication system 40.
  • the emitter 56 comprises an antenna 88 extending along the longitudinal axis L of the probe 12.
  • the longitudinal half parts 78 define a compartment 90 for receiving the antenna 88. Therefore, the antenna 88 is maintained motionless and vertical in the compartment 90 when the probe 12 is introduced in the ground. Moreover, the antenna 88 is protected when the probe 12 impacts the ground.
  • the senor unit 54 and/or the emitter 56 are at least partially biodegradable as defined above. Moreover, the sensor unit 54 and/or the emitter 56 can also be at least partially chemically degradable.
  • They comprise for example a support 92 and electronic circuit 94 carried on the support 92, at least the support 92 being at least partly biodegradable. At least the support 92 may be also at least partially chemically degradable.
  • the power source 58 comprises a battery.
  • the battery is able to power the emitter 56 and/or each sensor 56A of the sensor unit 54.
  • the battery for example comprises a casing 96 and electrochemical material.
  • the casing 96 or the whole battery 58 is at least partially biodegradable. It may also be at least partially chemically degradable. Overall, the mass content of biodegradable material in the probe 12 is advantageously greater than 90% in mass, in particular greater than 95% in mass, preferably greater than 99% in mass, for example greater than 99.8% in mass.
  • the content of material which is not biodegradable and/or not chemically degradable in the probe 12 is less than 10% in mass, in particular less than 5% in mass, preferably less than 1 % in mass, more preferably less than 0.2 % in mass of the total mass of the probe 12.
  • non-degradable i.e it remains structured for at least six months, in particular for at least one year, in particular for at least two years after the probe 12 has been put in contact with the ground.
  • the hollow casing 50, the sensor unit 54, the emitter 56 and the power source 58 being at least partially biodegradable and/or at least partially chemically degradable, the probes 12 have a reduced environmental impact in the ground.
  • the low non-degradable content of the probes 12 diminishes the environmental impact when the probe 12 biodegrades or chemically degrades.
  • the flying vehicle 32 is for example an unmanned aerial vehicle (UAV) piloted from the base 36 or automatically configured to reach a launching point above a skyhole 26.
  • UAV unmanned aerial vehicle
  • the launching unit 34 comprises a mechanical retainer able to be operated from a probe retaining configuration in which the retainer holds the probe 12 with the fixing means 77 and a dropping configuration, in which the retainer frees the probe 12 to let it fall down from the flying vehicle 32.
  • the telecommunication system 40 comprises antennas located in at least part of the clearings 24, and/or flying antennas. It is able to collect data received from the emitter 56 of each probe 12 and to convey it to the collection and analysis unit 38 at the base 34.
  • the additional flying vehicle 42 is for example a helicopter, an airship or a balloon which is able to carry equipment such as the sources 30 towards each clearing 24.
  • a location of a plurality of sources 30 and the location of a plurality of probes 12 in the region of interest 14 are defined respectively into artificial or natural clearings 24 of the region of interest 14 and into sky holes 26 of the region of interest 14.
  • the sources 30 and the probes 12 are carried to the base 36.
  • the sources 30 are then put in place in the clearings 24, advantageously by flying the additional flying vehicle 42 to each clearing 24 and by unloading each source 30 in a clearing 24.
  • each source 30 is then installed in a hole drilled in the ground. Then, each flying vehicle 32 is loaded with at least one probe 12 in the launching unit 34, preferably with several probes 12. Then, the flying vehicle 32 is flown over successive sky holes 26 and the launching unit 34 is triggered to let each probe 12 fall down, as shown in figure 5.
  • the insertion of the probes 12 in the ground is made without the need of a man intervention on the ground. It is extremely simple and accurate, and it allows dropping a large number of probes 12, for example more than 1 ,000 probes, in particular more than 10,000 probes.
  • At least one source 30 is triggered to generate a seismic stimulus.
  • the seismic stimulus propagates in the ground and reflects against the different layers in the subsurface 13.
  • a seismic signal is captured by the sensors 54A of the sensor unit 54.
  • the signal is digitalized, conditioned and/or processed by the data recovery unit, and is stored.
  • the collected data is then transmitted to the base 36 through the emitter 56 and the telecommunication system 40.
  • the data is then transmitted to the collection and analysis unit 38 by the antennas of the telecommunication system 40.
  • the sources 30 are recovered. Nevertheless, the probes 12 remain in place and at least partially degrade, directly in the soil, by biodegradation and/or chemical degradation.
  • the degradation process advantageously occurs in less than two years, in particular in in less one year, preferably in six months, with more of 90% in mass of the total mass of the probe 12 being transformed.
  • the method for surveying the ground with the assembly 10 is therefore extremely simple to operate and has a minimal impact on the environment.
  • the method does not require opening large areas of vegetation 18 to put in place the sources 30 and the probes 12. It greatly reduces human intervention and limits the risks for human safety and environment.
  • the probes 12 are able to remain in place in the ground, without the need of a further human intervention to recover the probes 12.
  • the degradation of the probes 12 reduces the impact on the environment. A large number of probes 12 can therefore be used, which enhances the image quality.
  • the method comprises obtaining a first longitudinal half part 78 and a second longitudinal half part 78 by injection molding of plastic.
  • a same half mold is used for providing the first longitudinal half part 78 and the second longitudinal half part 78.
  • the plastic is for example biodegradable.
  • biodegradable plastics are aliphatic polyesters, such as polyhydroxyalkanoates (PHA), like poly-3-hydroxybutyrate (PHB), polyhydroxyvalerate (PHV), and polyhydroxyhexanoate (PHH).
  • PHA polyhydroxyalkanoates
  • PBS polybutenesuccinate
  • PCL polycaprolactone
  • the two longitudinal half parts 78 are then assembled to define at least one inner compartment 80 and at least one outer compartment 82 surrounding the inner compartment 80 in the hollow casing 50.
  • the method comprises, before the assembling step, inserting in the inner compartment 80 or in the outer compartment 82 at least one of the sensor 54A, the emitter 56, and/or the power source 58.
  • the two longitudinal parts 78 are advantageously assembled by ultrasonic welding.
  • a package of biological entities such as enzymes, nutriments favoring the development of microorganisms or chemicals (for instance oxydants or acids) able to increase the speed of biodegradation and/or chemical degradation of the hollow casing 50 and/or of the sensor unit 54 and/or of the emitter 56 and/or of the power source 58, is included in the hollow casing 50 to enhance biodegradability and/or chemical degradability after impact with the ground.
  • enzymes such as lipase, esterase, and alcalase, or more generally enzymes which are known to hydrolyze polylacticacid effectively, can be included in the hollow casing 50.
  • seeds of vegetation are included in the hollow casing to favor reforestation of the region of interest.
  • the rear part 64 of the probe 12 degrades first to generate a top opening enabling rainwater to penetrate quickly the hollow casing and ease degradation of the rest of the probe.
  • the mechanical strength of the biodegradable material in the lower part of the probe 12 is greater than the mechanical strength of the biodegradable material in the upper part of the probe 12.
  • the biodegradable material in the upper part of the probe advantageously has a rate of degradation greater than the rate of degradation of the biodegradable material in the lower part of the probe 12.
  • the hollow casing 50 defines openings. Tabs of a first material are inserted into the hollow casing 50 made of a second material, in order to close openings. The rate of degradation of the first material is greater than the rate of degradation of the second material.
  • the rate of degradation is defined by the relative amount of material, able to degrade in a unit of time.
  • the relative amount of material is taken as the ratio of the mass of material which has been degraded to the initial mass of material.
  • the openings are quickly opened to enable rainwater to penetrate the hollow casing 50 and ease degradation of the rest of the probe 12.
  • the longitudinal half parts 78 comprise a plurality of longitudinal reinforcing elements, at least in the central partition 62.
  • the longitudinal reinforcing elements increase the robustness of the probe 12, especially to allow resisting to the impact with the ground, and moreover, the areas located between the longitudinal reinforcing elements degrade more rapidly compared to the longitudinal reinforcing elements. In this way, the global degradation process of the probe 12 is accelerated.
  • each longitudinal half part 78 is obtained using a different half mold.
  • the first half part 78 and the second half part 78 are different.
  • the longitudinal half parts 78 are assembled along a contact plane P extending according to an axis parallel to the longitudinal axis L.
  • the support 92 and the electronic circuit 94 of the sensor unit 54 and/or the emitter 56 are flexible.
  • the support 92 is for example rolled in a tubular shape and disposed inside the outer compartment 82 of the probe 12.
  • the power source 58 is a fuel cell 98 and the outer compartment 82 defines a reservoir 100 for receiving an oxidizing agent or a reducing agent 102. Moreover, as mentioned above, the oxidizing agent or the reducing agent 102 is also used as a material intended to ballast the probe 12.
  • the outer compartment 82 defines a water reservoir 104 and the probe 12 comprises at least one collecting cup 106 in fluidic communication with the outer compartment 82.
  • the collecting cup 106 is indented to collect water 108 from a rainfall or from dew. Therefore, the collected water 106 is used as fuel for the fuel cell 98 and the lifetime of the probe 12 is improved.
  • the probe 12 comprises means to avoid the probe 12 to be introduced totally in the ground. The means comprise for example protruding elements extending outward from the probe 12.
  • the hollow casing 56 is not intended to be directly in contact with the ground.
  • the probe comprises an external casing surrounding the hollow casing 56.
  • the external casing comprises an end to be placed in contact with the ground.
  • the external casing is overmolded on the hollow casing 55.
  • the hollow casing 56 or more generally the probe 12, is provided with at least one passage intended to allow an access to a connecting port to the electronic circuit 94.
  • a connecting port is for instance used to configure the electronic circuit 94 without having to open the probe 12.
  • Said connecting port is preferably sealed in the passage and water proof.

Abstract

L'invention concerne une sonde (12) destinée à être partiellement introduite dans un sol depuis un véhicule volant, pour effectuer des mesures dans le sol, la sonde (12) comprenant : - un boîtier creux (50) délimitant un boîtier fermé (52), - au moins un capteur (54A) logé dans le boîtier fermé (52), le capteur (54A) étant apte à détecter une grandeur physique liée au sol ; - au moins un émetteur (56) logé dans le boîtier fermé (52), l'émetteur (56) étant apte à envoyer des données représentatives de la grandeur physique détectée par le capteur (54A); - au moins une source d'alimentation (58) logée dans le boîtier fermé (52). Le boîtier fermé (52) comprend au moins un compartiment interne (80) et au moins un compartiment externe (82) entourant au moins partiellement le compartiment interne (80), le boîtier creux (52) comprenant au moins deux parties longitudinales assemblées (78) délimitant le compartiment interne (80) et le compartiment externe (82).
PCT/IB2018/001634 2018-12-07 2018-12-07 Sonde destinée à être partiellement introduite dans un sol depuis un véhicule volant, ensemble et procédé associés WO2020115519A1 (fr)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120174659A1 (en) * 2010-09-17 2012-07-12 Jerome Johnson Impact penetrometer systems for characterizing soil properties
EP2664945A1 (fr) * 2012-05-15 2013-11-20 The Boeing Company Capteurs au sol automatiques
US20140126329A1 (en) * 2012-11-02 2014-05-08 Fairfield Industries Incorporated Land based unit for seismic data acquisition
EP2741264A1 (fr) * 2012-12-07 2014-06-11 The Boeing Company Système de déploiement et de surveillance de capteur de forêt
WO2018224620A1 (fr) * 2017-06-08 2018-12-13 Total Sa Sonde destinée à être partiellement introduite dans un sol depuis un véhicule volant, ensemble et procédé associés

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120174659A1 (en) * 2010-09-17 2012-07-12 Jerome Johnson Impact penetrometer systems for characterizing soil properties
EP2664945A1 (fr) * 2012-05-15 2013-11-20 The Boeing Company Capteurs au sol automatiques
US20140126329A1 (en) * 2012-11-02 2014-05-08 Fairfield Industries Incorporated Land based unit for seismic data acquisition
EP2741264A1 (fr) * 2012-12-07 2014-06-11 The Boeing Company Système de déploiement et de surveillance de capteur de forêt
WO2018224620A1 (fr) * 2017-06-08 2018-12-13 Total Sa Sonde destinée à être partiellement introduite dans un sol depuis un véhicule volant, ensemble et procédé associés

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