Not applicable.
Not applicable.
Seismic surveying, or reflection seismology, is used to map the Earth's subsurface. During a seismic survey, a controlled seismic source emits low frequency seismic waves that travel through the subsurface of the Earth. At interfaces between dissimilar rock layers, the seismic waves are partially reflected. The reflected waves return to the surface where they are detected by one or more seismic sensors. In particular, the seismic sensors detect and measure vibrations induced by the waves. Ground vibrations detected by the seismic sensors at the earth surface can have a very wide dynamic range, with displacement distances ranging from centimeters to angstroms. Data recorded by the seismic sensors is analyzed to reveal the structure and composition of the subsurface.
Some embodiments disclosed herein are directed to a sensor assembly for a seismic sensor. In an embodiment, the sensor assembly includes an electrically conductive outer housing, and an electrically insulating holder disposed within the outer housing. The holder comprises a recess. In addition, the sensor assembly includes a sensor element disposed within the recess of the holder. The sensor comprises a sensing element, and is electrically insulated from outer housing by the holder.
Other embodiments disclosed herein are directed to a seismic sensor. In an embodiment, the seismic sensor includes an outer housing having a central axis, an upper end, a lower end, and an inner cavity. In addition, the seismic sensor includes a proof mass moveably disposed in the inner cavity, wherein the outer housing is configured to move axially relative to the proof mass, and a plurality of biasing members disposed within the inner cavity and configured to flex in response to axial movement of the outer housing relative to the proof mass. Further, the seismic sensor includes a sensor assembly disposed in the inner cavity and axially positioned between the proof mass and the lower end of the outer housing. The sensor assembly includes an electrically conductive sensor housing, and an electrically insulating holder disposed within the sensor housing. The holder includes a recess. In addition, the sensor assembly includes a sensor element disposed within the recess of the holder. The sensor comprises a piezoelectric element, and wherein the sensor element is electrically insulated from the sensor housing by the holder.
Still other embodiments disclosed herein are directed to a method of manufacturing a seismic sensor. In an embodiment, the method includes (a) inserting a sensor element within a recess of an electrically insulating holder, (b) enclosing the holder and the sensor element within an electrically conductive sensor housing after (a), and (c) engaging the sensor housing with an end of a carrier after (b). In addition, the method includes (d) suspending a proof mass within the carrier via a plurality of biasing members. Further, the method includes (f) inserting the carrier, the sensor housing, and the proof mass within an outer housing after (c) and (d) such that the sensor element is deflected when the carrier moves relative to the proof mass.
Embodiments described herein comprise a combination of features and characteristics intended to address various shortcomings associated with certain prior devices, systems, and methods. The foregoing has outlined rather broadly the features and technical characteristics of the disclosed embodiments in order that the detailed description that follows may be better understood. The various characteristics and features described above, as well as others, will be readily apparent to those skilled in the art upon reading the following detailed description, and by referring to the accompanying drawings. It should be appreciated that the conception and the specific embodiments disclosed may be readily utilized as a basis for modifying or designing other structures for carrying out the same purposes as the disclosed embodiments. It should also be realized that such equivalent constructions do not depart from the spirit and scope of the principles disclosed herein.
For a detailed description of various exemplary embodiments, reference will now be made to the accompanying drawings in which:
The following discussion is directed to various exemplary embodiments. However, one of ordinary skill in the art will understand that the examples disclosed herein have broad application, and that the discussion of any embodiment is meant only to be exemplary of that embodiment, and not intended to suggest that the scope of the disclosure, including the claims, is limited to that embodiment.
The drawing figures are not necessarily to scale. Certain features and components herein may be shown exaggerated in scale or in somewhat schematic form and some details of conventional elements may not be shown in interest of clarity and conciseness.
In the following discussion and in the claims, the terms “including” and “comprising” are used in an open-ended fashion, and thus should be interpreted to mean “including, but not limited to . . . .” Also, the term “couple” or “couples” is intended to mean either an indirect or direct connection. Thus, if a first device couples to a second device, that connection may be through a direct connection of the two devices, or through an indirect connection that is established via other devices, components, nodes, and connections. In addition, as used herein, the terms “axial” and “axially” generally mean along or parallel to a given axis (e.g., central axis of a body or a port), while the terms “radial” and “radially” generally mean perpendicular to the given axis. For instance, an axial distance refers to a distance measured along or parallel to the axis, and a radial distance means a distance measured perpendicular to the axis. Further, when used herein (including in the claims), the word “about,” “generally,” “substantially,” “approximately,” and the like mean within a range of plus or minus 10%.
As previously described, during a seismic survey, seismic sensors are used to detect reflected seismic waves to reveal the structure and composition of the subsurface. One type seismic sensor relies on capacitance to generate the electrical signal. With one example, these sensors can be constructed as Microelectromechanical systems (MEMS) using micro machined silicon with metal plating applied to facing components on opposite sides of a small plated and spring loaded mass. These MEMS sensors often have the advantage of small size and weight compared to a moving coil geophone. The movement of the MEMS proof mass relative to the outer fixed plates creates variable capacitance that is detected as a signal proportional to the acceleration of the sensor displacement. During operations, electromagnetic interference from other electromagnetic components both within and around the seismic sensor may interfere with the MEMS sensor's ability to produce quality data.
Accordingly, embodiments disclosed herein include seismic sensors, particular MEMS type seismic sensors that include enclosed sensor assemblies for providing electromagnetic shielding for the sensor element(s) housed therein. In at least some embodiments, the enclosed and shielded sensor assemblies are insulated (partially or totally) from any surrounding electromagnetic interference, so that the data quality may be improved (e.g., from that captured by a non-shielded sensor assembly). In addition, at least some embodiments of the sensor assemblies disclosed herein include an electrically insulating holder, which may allow the sensor element(s) within the sensor assembly to be separated (and thus insulated) from an electrically conductive outer housing (or shielding) of the sensor assembly. Further, without being limited to this or any other theory, embodiments of the sensor assemblies disclosed herein may be easier to manufacture and assemble than other sensor assembly designs.
Referring now to
Surveying system 50 includes a seismic source 54 disposed on the surface 56 of the earth and a plurality of seismic sensors 64, 66, 68 firmly coupled to the surface 56.
The seismic source 54 generates and outputs controlled seismic waves 58, 60, 62 that are directed downward into the subsurface 51 and propagate through the subsurface 51. In general, seismic source 54 can be any suitable seismic source including, without limitation, explosive seismic sources, vibroseis trucks and accelerated weight drop systems also known as thumper trucks. For example, a thumper truck may strike the surface 56 of the earth with a weight or “hammer” creating a shock which propagates through the subsurface 51 as seismic waves.
Due to the differences in the density and/or elastic velocity of layer 52 as compared to the remainder of subsurface 51, the seismic waves 58, 60, 62 are reflected, at least partially, from the surface of the layer 52. The reflected seismic waves 58′, 60′, 62′ propagate upwards from layer 52 to the surface 56 where they are detected by seismic sensors 64, 66, 68.
The seismic source 54 may also induce surface interface waves 57 that generally travel along the surface 56 with relatively slow velocities, and are detected concurrently with the deeper reflected seismic waves 58′, 60′, 62′. The surface interface waves 57 generally have a greater amplitude than the reflected seismic waves 58′, 60′, 62′ due to cumulative effects of energy loss during propagation of the reflected seismic waves 58′, 60′, 62′ such as geometrical spreading of the wave front, interface transmission loss, weak reflection coefficient and travel path absorption. The cumulative effect of these losses may amount to a 75 dB, and in cases more than 100 dB, in amplitude difference between various waveforms recorded by sensors 64, 66, 68.
The sensors 64, 66, 68 detect the various waves 57, 58′, 60′, 62′, and then store and/or transmit data indicative of the detected waves 57, 58′, 60′, 62′. This data can be analyzed to determine information about the composition of the subsurface 51 such as the location of layer 52.
Although seismic surveying system 50 is shown and described as a surface or land-based system, embodiments described herein can also be used in connection with seismic surveys in transition zones (e.g., marsh or bog lands, areas of shallow water such as between land and sea) and marine seismic survey systems in which the subsurface of the earthen formation (e.g., subsurface 51) is covered by a layer of water. In marine-based systems, the seismic sensors (e.g., seismic sensors 64, 66, 68) may be positioned in or on the seabed, or alternatively on or within the water. In addition, in such marine-based systems, alternative types of seismic sources (e.g., seismic sources 54) may be used including, without limitation, air guns and plasma sound sources.
Referring now to
In this embodiment seismic sensor 100 includes an outer housing 101, an inductive spool assembly 130 disposed within housing 101, a carrier 140 disposed in housing 101, and a sensor assembly 300 disposed within housing 101 and coupled to carrier 140. Housing 101 has a central or longitudinal axis 105, a first or upper end 101a, a second or lower end 101b, and an inner chamber or cavity 102. Ends 101a, 101b are closed and inner cavity 102 is sealed and isolated from the environment surrounding sensor 100, thereby protecting the sensitive components disposed within housing 101 from the environment (e.g., water, dirt, etc.). In addition, housing 101 includes a generally cup-shaped body 110 and an inverted cup-shaped cap 120 fixably attached to body 110.
Body 110 has a central or longitudinal axis 115 that is coaxially aligned with axis 105, a first or upper end 110a, and a second or lower end 110b defining lower end 101b of housing 101. In addition, body 110 includes a base 111 at lower end 110b and a tubular sleeve 112 extending axially upward from base 111 to upper end 110a. Base 111 closes sleeve 112 at lower end 110b; however, sleeve 112 and body 110 are open at upper end 110a. As a result, body 110 includes a receptacle 113 extending axially from upper end 110a to base 111. Receptacle 113 forms part of inner cavity 102 of housing 101.
In this embodiment, body 110 of outer housing 101 includes a pair of connectors 118a, 118b. Connector 118a is provided on base 111 and connector 118b is provided along sleeve 112. Connector 118a includes rectangular throughbore 119a extending radially therethrough and a hole 119b extending axially from lower end 110b to throughbore 119a. Hole 119b is internally threaded and threadably receives the externally threaded end of a spike (not shown) used to secure sensor 100 to the ground during seismic survey operations. Throughbore 119a enables a rope or the like (not shown) to be attached to sensor 100 for storage or deployment. In particular, the rope may be folded double and inserted throughbore 119a. Thus, bore 119a has a width of at least twice the diameter of the rope. The loop formed by the portion of folded rope extending through bore 119a is then placed around the sensor 100. In this manner, a plurality of sensors 100 can be coupled to a single rope without side ropes, hooks or other mechanisms that can complicate the handling of multiple sensors 100.
The connector 118b is disposed along the outside of sleeve 112 proximal upper end 101a. In general, connector 118b provides an alternative connection point for handling of sensor 100 during deployment and retrieval. In this embodiment, connector 118b is an eye connector or throughbore to which a rope, lanyard, hook, carabiner or the like can be releasably attached. Connector 118b can also be used in a manner similar to throughbore 119a, thereby allowing a rope to be folded double and inserted through the hole of connector 118b. Thus, the bore of connector 118a has a width of at least twice the diameter of the rope. The loop formed by the portion of folded rope extending through the bore of connector 118b is then placed around the sensor 100. In this manner, a plurality of sensors 100 can be coupled to a single rope without side ropes, hooks or other mechanisms that can complicate the handling of multiple sensors. In this embodiment, the entire body 110 (including base 111 and sleeve 112) is made via injection molding.
Referring still to
Cap 120 is fixably attached to body 110 such that cap 120 is coaxially aligned with body 110 and such that lower end 120b of cap 120 seated within upper end 110a of body 110 and upper end 110a of body 110 coupled to flange 126. Body 110 and cap 120 are sized such that an interference fit is provided between lower end 120b of cap 120 and upper end 110a of body 110. In this embodiment, body 110 and cap 120 are made of the same material (polycarbonate), and thus, are can be ultrasonically welded together to fixably secure cap 120 to body 110. More specifically, as shown in
Referring still to
Inductive spool assembly 130 is used to inductively charge the battery 190 from the outside of sensor 100 (e.g., wirelessly). In this embodiment, spool assembly 130 is mounted within cavity 123 of cap 120 and includes a cylindrical sleeve-shaped body 131 and a coil 136 wound around body 131. Coil 136 is electrically coupled to circuit board 195 with wires or other suitable conductive paths (not shown) that enable the transfer of current to circuit board 195, which in turn charges battery 190 during charging operations.
Referring still to
Carrier 140 has a central or longitudinal axis 145 coaxially aligned with axis 105, a first or upper end 140a extending through inductive spool assembly 130, and a second or lower end 140b axially adjacent base 111. Carrier 140 has an axial length that is substantially the same as the axial length of cavity 102. Thus, upper end 140a engages top 121 of cap 120 and lower end 140b is coupled to sensor assembly 300 which in turn is supported by base 111 of body 110. More specifically, carrier 140 is axially compressed between cap 120 and body 110. As a result, movement of carrier 140 relative to outer housing 101 is generally restricted (or prevented entirely) during operations, so that carrier 140 is fixably secured or mounted within housing 101.
Referring still to
Referring specifically now to
Referring still to
Referring now to
In this embodiment, each tab 200 is a resilient, semi-rigid element through which battery 190 is supported within pocket 144 of carrier 140. As best shown in
For purposes of clarity and further explanation, the tab 200 coupled to upper end 190a of battery 190 may be referred to as the upper tab 200a and the tab 200 coupled to lower end 190b of battery 190 may be referred to as the lower tab 200b. Generic references herein to “tabs 200” refer to both the upper tab 200a and lower tab 200b. The semi-circular edge 201b of upper tab 200a is seated in upper recess 150 of carrier 140, and the semi-circular edge 201b of lower tab 200b is seated in lower recess 151 of carrier 140. As best shown in
Referring still to
Lower tab 200b does not include a projection 208 and recess 206 as described above for upper tab 200a and instead includes a cylindrical post 163 extending axially therefrom (see
Referring still to
As previously described, tabs 200 provide electrical couplings between battery 190 and circuit board 195. In addition, tabs 200 function like flexures or biasing members for suspending battery 190 within pocket 144. Accordingly, tabs 200 may also be referred to as flexures or biasing members. In particular, tabs 200 are resilient flexible elements that flex and elastically deform in response to relative axial movement of outer housing 101 and carrier 140 relative to battery 190. In addition, tabs 200 radially bias battery 190 to a central or concentric position within pocket 144 radially spaced from carrier 140. In particular, the presence of spiral slots 207 enhances the flexibility of tab 200 in the region along which slots 207 are disposed, thereby allowing that region to flex in the axial direction (up and down) with relative ease. Spiral slots 207 also enhance the flexibility of each tab 200 in the radial direction. However, spiral slots 207 may generally resist some flexing of tabs 200 in the radial direction. Due to the relatively high degree of flexibility of tabs 200 in the axial direction, when an axial load is applied to tabs 200 by carrier 140 or battery 190, slots 207 generally allow free relative axial movement between central projection 208 and edges 201a, 201b on upper tab 200a and free relative axial movement between post 163 and edges 201a, 201b on lower tab 200b. However, due to the more limited flexibility in the radial direction, when a radial load is applied to tabs 200 by carrier 140 or battery 190, slots 207 may generally resist relative some (but not necessarily all) radial movement between the central projection 208 and edges 291a, 291b of upper tab 200a and between post 163 and edges 201a, 201b of lower tab 200b. Thus, tabs 200 bias battery 190 and carrier 140 back into substantial coaxial alignment with axes 105, 145 (but with the radial offset of battery 190 as previously described above).
Referring still to
As shown in
Referring now to
Referring still to
In addition, a plurality of holes or apertures extend into recess 325 through the base plate 322 and wall segments 324. In particular, cup 320 includes a plurality of first apertures 326, a plurality of second apertures 327, and a plurality of third apertures 328.
The plurality of first apertures 326 each extend through corresponding ones of the wall segments 322 and through a portion of base plate 322 at the outer periphery 323. In this embodiment, the first apertures 326 are uniformly angularly spaced about axis 305. More specifically, there are a total of three first apertures 326 spaced approximately 120° apart from one another about axis 305. The plurality of second apertures 327 each extend through corresponding ones of the wall segments 324 at the intersection of the corresponding wall segments 324 and the periphery 323 of base plate 322. In this embodiment, second apertures 328 are uniformly angularly spaced about axis 305. More specifically, there are a total of two second apertures 327 disposed radially opposite one another (i.e., disposed approximately 180° from one another) about axis 305. The plurality of third apertures 328 each extend through corresponding ones of the wall segments 324 at points that are axially spaced from periphery 323. In this embodiment, third apertures 328 are uniformly angularly spaced about axis 305. More specifically, there are a total of three third apertures 328 spaced approximately 120° apart from one another about axis 305.
Cup 320 comprises a conductive material (e.g., a metal). In some specific embodiments, cup 320 may comprise, for example, steel, aluminum, copper, etc. As will be described in more detail below, cup 320 is configured to conduct electrical current and/or interference away from sensor element 360 during operations so as to improve operations thereof. In addition, in this embodiment, wall segments 324 are monolithically formed with base plate 322, and thus each comprises the same material. However, it should be appreciated that in other embodiments, wall segments 324 and base plate 322 may be formed as separate bodies or members that are connected or coupled together.
Referring still to
A pair of projections 350 extend radially outward from wall 344, and a pair of axially extending recesses 352 extend axially inward to wall 344 from annular surface 341 to projections 350. In this embodiment, each of the projections 350 and corresponding recesses 352 are radially opposite (i.e., disposed approximately 180° from) one another about axis 305.
In addition, holder 340 includes a receptacle 348 disposed along wall 344. In particular, receptacle 348 extends axially upward from annular wall 341 and includes a pair of slots 347. As will be described in more detail below, slots 347 are configured to receive corresponding electrical connectors therein for electrically connecting sensor element 360 to circuit board 195 (see
As is best shown in
Holder 340 comprises an electrically insulating material (e.g., a polymer, a composite (e.g., fiberglass), etc.). As will be described in more detail below, holder 340 is configured to electrically insulate sensor element 360 from other conductive portions of sensor assembly 300 during operations (e.g., cup 320, cover plate 380, etc.).
Referring still to
Cover plate 380 includes a planar base plate 382 that is oriented radially relative to axis 305 and that includes an outer periphery 383. A recess or notch 385 extends radially inward from periphery 383. In addition, an aperture 384 extends through plate 382 at a position that is spaced from periphery 383 but is radially shifted slightly from axis 305.
A plurality of tabs or projections extend generally axially from periphery 383 of base plate 382. In particular, base plate 382 includes a plurality of first tabs 387, a plurality of second tabs 388, and a plurality of third tabs 389. The plurality of first tabs 387 each extending from periphery 383 of base plate 382. In this embodiment, the first tabs 387 are uniformly angularly spaced about axis 305. More specifically, there are a total of three first tabs 387 spaced approximately 120° apart from one another about axis 305. The plurality of second tabs 387 each also extend from the periphery 383 of base plate 382. In this embodiment, there are two second tabs 388 disposed on opposing angular sides of recess 385. In particular, each second tab 388 is disposed angularly between recess 385 and corresponding ones of the first tabs 387. The plurality of third tabs 389 each also extend from the periphery 383 of base plate 382. In this embodiment, there are two third tabs 389 disposed along periphery 383 generally on a side of cover plate 380 that is radially opposite recess 385. In addition, a first connector tab 386 extends axially upward from a wall or border of notch 385.
Cover plate 380 comprises a conductive material, such as, for example, a metal. In some specific embodiments, cover plate 380 may comprise, for example, steel, aluminum, copper, etc. In addition, in some embodiments, cover plate 380 may comprise the same conductive material as cup 320; however, this may not be the case in other embodiments. As will be described in more detail below, cover plate 380 is configured to conduct electrical current and/or interference away from sensor element 360 and into cup 320 during operations so as to improve operations thereof.
Referring now to
Referring again to
Either before or after holder 340 is inserted within recess 325 of cup 320, sensor element 360 is installed within recess 325. In particular, sensor element 360 is inserted within recess 325 such that periphery 363 is inserted radially into retention recess 349 of holder 340. Thereafter, a pair of electrical leads or connectors 370, 371 are installed within slots 347 of receptacle 348 to provide electrical connection with sensor element 360 and other components within sensor 100 (e.g., circuit board 195).
In particular, the pair of electrical connectors 370, 371 comprises a first connector 370 and a second connector 371. First connector 370 includes a central body 372, a first conductive lead 374 extending from body 372, and a second conductive lead 376 extending from body 372. Similarly, second connector 371 includes a central body 373, a first conductive lead 375 extending from body 373, and a second conductive lead 377 extending from body 373. In this embodiment, the body 372 and leads 374, 376 of first connector 370 are all made of electrically conductive materials (e.g., a metal), and may, in some embodiments, be formed of the same material (e.g., such that body 372 and leads 374, 376 of first connector 370 are monolithically formed). Similarly, in this embodiment, body 373 and leads 375, 377 of second connector 371 are also all made of electrically conductive materials, and may, in some embodiments, be formed of the same material (e.g., such that body 373 and leads 375, 377 of second connector 371 are monolithically formed). As best shown in
Referring now to
Accordingly, when sensor assembly 300 is fully constructed as described above, cover plate 380 and cup 320 form an outer housing 310 (or sensor housing 310) that receives sensor element 360 and holder 340 therein. In addition, sensor element 360 is installed within housing 310 such that no contact is formed between sensor element 360 (or connectors 370, 371) and either cover plate 380 and cup 320. Rather, sensor element 360 and connectors 370, 371 are in contact with holder 340 within housing 310. Because cover plate 380 and cup 320 are constructed from electrically conductive materials, the housing 310 forms an electrically conductive shell around sensor element 360 that protects or shields sensor element 360 from electromagnetic interference generated outside of housing 310. In other words, housing 310 forms a so-called “Faraday cage” about sensor element 360.
Referring now to
Referring again to
Thus, the sensor assembly 300 may be assembled and electrically coupled to other components within seismic sensor 100 (e.g., circuit board 195) with relative ease (e.g., a technician does not need to route additional wiring between sensor assembly 300 and circuit board 195 after sensor assembly 300 is attached to lower end 140b of carrier 140). Rather, the arrangement and design of connectors 370, 371, and connector tab 386 may provide a predetermined alignment to the appropriate locations or contacts on circuit board 195, so that the mechanical attachment of sensor assembly 300 to lower end 140b of carrier 140 as described above also facilitates the above described electrical connections.
Referring to
Referring now to
Referring now to
The arrival of a compressional seismic wave causes outer housing 101 and the components fixably coupled thereto (e.g., spool assembly 130, carrier 140, circuit board 195, light guide 129, etc.) to move in a generally vertical direction. The inertia of the proof mass (which in this embodiment comprises battery 190 as previously described above) within outer housing 101 causes the proof mass to resist moving with the displacement of the outer housing 101 and carrier 140, and consequently the outer housing 101 and carrier 140 reciprocate axially relative to the proof mass, as permitted by tabs 200 and biasing member 250. This movement causes tabs 200 and free portion 254 (including engagement member 260) of biasing member 250 to flex or be deflected and the load of the proof mass to be taken up by the sensor element 360, via post 163. The axial reciprocation of the outer housing 101 and carrier 140 relative to the proof mass generally continues as the compressional seismic wave passes across sensor 100.
During the axial reciprocations of the outer housing 101 and carrier 140 relative to the proof mass, the sensor element 360 is cyclically deflected by post 163. As previously described, when mechanical stress is applied to sensor element 360 due to deformation or deflection by post 163, the piezoelectric ceramic material of piezoelectric element 364 generates an electrical potential (piezoelectric effect). The electrical potential is conducted to circuit board 195 via leads 376, 374 of first connector 370 and/or leads 373, 373 of second connector 371 (see
During these operations, sensor element 360 is shielded from electromagnetic interference by the conductive housing 310 as previously described above. Such electromagnetic interference may be generated by other electronic components within sensor 100 (e.g., battery 190, inductive spool assembly 130, circuit board 195, etc.) or by sources disposed outside of sensor 100 (e.g., other electronic components disposed adjacent to sensor 100 during a seismic survey). Thus, by enclosing sensor element 360 within a conductive housing 310 as described above, the amount of signal noise caused by such electromagnetic interference may be reduced (or eliminated entirely). Accordingly, the quality of seismic signals collected by the seismic sensors disclosed herein (e.g., sensor 100) may be improved.
While exemplary embodiments have been shown and described, modifications thereof can be made by one skilled in the art without departing from the scope or teachings herein. The embodiments described herein are exemplary only and are not limiting. Many variations and modifications of the systems, apparatus, and processes described herein are possible and are within the scope of the disclosure. Accordingly, the scope of protection is not limited to the embodiments described herein, but is only limited by the claims that follow, the scope of which shall include all equivalents of the subject matter of the claims. Unless expressly stated otherwise, the steps in a method claim may be performed in any order. The recitation of identifiers such as (a), (b), (c) or (1), (2), (3) before steps in a method claim are not intended to and do not specify a particular order to the steps, but rather are used to simplify subsequent reference to such steps.
Filing Document | Filing Date | Country | Kind |
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PCT/RU2019/000370 | 5/28/2019 | WO | 00 |