US3244099A - Controlled velocity explosive charge for seismic exploration - Google Patents
Controlled velocity explosive charge for seismic exploration Download PDFInfo
- Publication number
- US3244099A US3244099A US322758A US32275863A US3244099A US 3244099 A US3244099 A US 3244099A US 322758 A US322758 A US 322758A US 32275863 A US32275863 A US 32275863A US 3244099 A US3244099 A US 3244099A
- Authority
- US
- United States
- Prior art keywords
- explosive
- charge
- detonation
- tube
- velocity
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002360 explosive Substances 0.000 title claims description 104
- 238000005474 detonation Methods 0.000 claims description 55
- 239000000203 mixture Substances 0.000 claims description 16
- 239000000463 material Substances 0.000 claims description 10
- 208000011616 HELIX syndrome Diseases 0.000 claims 1
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 description 17
- 230000015572 biosynthetic process Effects 0.000 description 10
- 238000005755 formation reaction Methods 0.000 description 10
- 239000002131 composite material Substances 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 239000000835 fiber Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000000153 supplemental effect Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 229920002457 flexible plastic Polymers 0.000 description 3
- 239000000295 fuel oil Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 230000037452 priming Effects 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical compound [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 description 2
- 239000000026 Pentaerythritol tetranitrate Substances 0.000 description 2
- 241000364021 Tulsa Species 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000005422 blasting Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 239000012188 paraffin wax Substances 0.000 description 2
- 229960004321 pentaerithrityl tetranitrate Drugs 0.000 description 2
- 239000013589 supplement Substances 0.000 description 2
- XTFIVUDBNACUBN-UHFFFAOYSA-N 1,3,5-trinitro-1,3,5-triazinane Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)C1 XTFIVUDBNACUBN-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 239000001828 Gelatine Substances 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000003575 carbonaceous material Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 239000002283 diesel fuel Substances 0.000 description 1
- 239000003337 fertilizer Substances 0.000 description 1
- 239000011094 fiberboard Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 229920000159 gelatin Polymers 0.000 description 1
- 235000019322 gelatine Nutrition 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 239000012169 petroleum derived wax Substances 0.000 description 1
- 235000019381 petroleum wax Nutrition 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 239000004800 polyvinyl chloride Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D3/00—Particular applications of blasting techniques
- F42D3/06—Particular applications of blasting techniques for seismic purposes
Definitions
- FIG. 2 CONTROLLED VELOCITY EXPLOSIVE CHARGE FOR SEISMIC EXPLORATION Filed Nov. 12, 1963 FIG. 2
- This invention relates to controlled velocity explosive charges, and more particularly, it is directed to an improvement in the generation of seismic waves for use in geophysical surveying.
- elongated distributed explosive charges have been proposed for use in seismic surveying, wherein the effective detonation velocity of the charge is matched approximately to the seismic wave transmision velocities of the medium surrounding the charge.
- Such distributed charges have been found very useful in discriminating against the generation of seismic noise and in preventing undue damage to the surrounding medium.
- An example of the above-mentioned distributed charge is Silverman U.S. Patent 2,609,885 disclosing an explosive charge employing a helix of a linear explosive, such as Primacord detonating fuse, the helix having a pitch providing an effective detonation velocity equal to the wave transmission velocity of the surrounding formations in the direction of detonation.
- Lang US. Patent 2,846,019 discloses a method of generating seismic waves employing an explosive mixture of fuel gas and oxygen wherein the composition of the explosive gas mixture is adjusted to provide a velocity of detonation matched with the seismic wave transmission velocity of the adjacent formations.
- these lumps usually detonate at a velocity greater than that of the helical linear explosive, presenting considerable difficulties in designing such a charge to match the velocity of a specified formation. Additionally, the concentrated energy of such a charge lump may damage the ensuing distributed charge elements to cause failure of the detonation.
- a primary object of the present invention is an improved distributed charge useful as an energy source for generating seismic waves, which charge has a controllable velocity of detonation and an adjustable weight of explosive.
- a further object is such an energy source providing a uniform flow of explosive energy.
- Still a further object is such an energy source having a uniform detonation velocity.
- a still further object of the invention is such an energy source which is readily fabricated to provide the desired explosive weight and detonation velocity, while at the same time being relatively economical.
- FIGURE 1 illustrates a vertical cross-sectional view of a preferred form of an energy source according to the invention.
- FIGURE 2 illustrates a cross-sectional view of a bore hole with an energy source of the invention positioned in the bore hole.
- the continuous priming principle is employed to provide a unique explosive charge having a controllable velocity of detonation
- An elongated composite charge is provided utilizing a first explosive component producing a preselected effective velocity of detonation and being capable of self-sustaining detonation, and a second explosive component being incapable of self-sustaining detonation, but being detonable by the first component.
- the two explosive components are placed in detonation relation with each other so that, upon detonation of the first component, detonation proceeds along the length of the composite charge at a velocity substantially equal to the effective velocity of detonation of the first component.
- a linear explosive having a known velocity of detonation which is at least as great as the seismic wave velocity of the surrounding medium, may be arranged in a helix or other suitable shape to provide a vertical distributed charge having an effective velocity of detonation matched with the seismic wave transmission velocity of the formations surrounding the charge.
- effective detonation velocity refers to that component of the detonation velocity in the direction of the vertical axis of the charge.
- Various linear explosives may be employed in practicing the present invention to provide the desired velocity and directional properties and to continuously prime the supplemental charge.
- a detonating fuse such as the material known as Primacord
- Primacord is granular pentaerythritol tetranitrate (PETN) in a braided cord with a plastic sheath confining and protecting the explosive.
- PETN pentaerythritol tetranitrate
- Other similar explosives such as cyclotrimethylenetrinitramine (RDX), or the like, suitable for use as a detonating fuse or priming material may be used,
- Other forms such as a tube or rod of the explosive, typically formed by inserting a powder or granules of explosive in a sheath, such as flexible plastic tube, or a precast rigid groove may be utilized. Certain explosives of this type must be waterproofed.
- linear explosives are available in differing explosive weights and velocities of detonation, and the shape of the particular linear explosive selected may be varied to produce the desired effective velocity of detonation, as by controlling the pitch of the helical turns.
- shape of the particular linear explosive selected may be varied to produce the desired effective velocity of detonation, as by controlling the pitch of the helical turns.
- the turns spaced as closely as possible and the smallest linear explosive capable of initiating and sustaining detonation of the supplemental explosive is therefore preferred so that the possibility of cross-firing, i.e., firing across the turns, is reduced.
- the composite charge comprises a second explosive component employed as a booster charge to supplement the linear explosive and provide the desired total charge weight.
- the booster charge be formed of an explosive which is incapable of self-sustaining detonation, but which is detonable by the continuous priming action of the adjacent linear explosive. It has been determined that elongated slender cartridges, or slender columns, of ammonium nitrate explosives, such as a mixture of ammonium nitrate and fuel oil (AN/F0), are incapable of selfpropagation of detonation when the diameter of the column falls below a critical minimum diameter, although the explosive is self-sustaining when formed into large diameter columns.
- ammonium nitrate explosives such as a mixture of ammonium nitrate and fuel oil (AN/F0)
- a well-packed column of AN/FO with a diameter of 1 /2 inches is capable of self-sustaining detonation, while for diameters less than about 1 /2 inches, detonation, once beyond the influence of the primer, will slow and fail in about 2 /2 column diameters.
- Other of the well-known explosives are likewise incapable of self-sustaining detonation when formed into a shape having a cross section less than the minimum necessary, and these are suitable for use in the practice of our invention, although all are not necessarily of equal effectiveness for this purpose.
- the various ammonium nitrate explosives such as ammonium nitrate mixed with up to about percent of a carbonaceous material may be used.
- a liquifiabl-e hydrocarbon such as fuel oil
- ammonium nitrate explosive may be formulated with any of the well-known organic or inorganic sensitizers, and a light metal, such as magnesium or aluminum, may be incorporated in the explosive, if desired.
- the straight dynamites, ammonia dynamites or gelatine dynamites may be employed.
- the critical minimum cross section of the booster charge will vary, depending upon the particular explosive formulation, the method of manufacture, the density and other such factors. It is known that certain explosives, such as AN/FO or the like, are rendered less sensitive to detonation by moisture pick-up or by an increase in density, so that a charge of the explosive which is otherwise capable of self-sustaining detonation may be made incapable of self-sustaining detonation when such factors are varied. If the cross section of such a charge is increased above the critical dimension, the charge will again become selfpropagating.
- the critical cross section may be determined readily by various well-known tests. For example, a cone-shaped sample of the explosive may be detonated at the base of the cone and the diameter of the point of failure of propagation determined. It is critical to the invention that this critical diameter of the booster charge not be exceeded, or the booster will become self-propagating, and the elfectiveness of the composite charge will be reduced.
- a preferred construction of the composite explosive charge comprises a helical linear explosive surrounding a long slender column of otherwise nondetonable booster charge.
- the linear explosive and the booster charge are positioned closely adjacent each other, so that the two are in detonation relation over the length of the charge.
- the linear explosive continuously primes the otherwise nondetonable booster, and the two must be positioned so that the shock wave from the primer is of great enough magnitude to induce and sustain detonation in the column of booster. If this condition is absent, detonation of the column of booster charge will not proceed along its length, but will slow and fail, even though once begun. If the two explosive components are in detonation relation, the detonation will proceed at a velocity substantially equal to the eflective velocity of detonation of the linear explosive.
- FIGURE 1 there is shown a preferred embodiment of the explosive charge of the invention.
- An elongated, slender cartridge, or column which may be solid or cored, of AN/FO explosive is formed from a mixture of commercial grade ammonium nitrate and about 2 to 10 percent fuel oil.
- the mixture is inserted into a long, relatively thin-wall tubular mandrel 11 having an internal diameter suitable for holding a column of booster charge of a diameter less than the critical minimum diameter required for self-propagation of detonation of the ammonium nitrate explosive.
- the tube, or mandrel is formed of fiber or cardboard which may be waterproofed by impregnation with paraffin or a suitable resin.
- the diameter and length of the column 12 of the ammonium nitrate explosive may be varied according to the total explosive charge weight desired. In the instance of the ammonium nitrate explosive referred to above, this diameter typically may vary from A inch to 1% inches.
- a helix of linear explosive 13 formed of Prirnacord detonating fuse which encloses the ammonium nitrate column for substantially its complete length.
- an electric blasting cap 14 Connected to one end of the linear explosive is an electric blasting cap 14, or another suitable detonator, connected by electrical leads 16 to a suitable power source.
- perforations 17 may be provided in the mandrel wall to permit the entry of fluids into the mandrel interior to reduce buoyancy so that the explosive charge may be more easily placed at a desired depth in water of a fluid-filled bore hole.
- the column of booster may be enclosed in a waterproofed container, such as flexible plastic bag 18.
- the pitch of the helix is chosen to provide the desired effective velocity of detonation in the manner herein described, and a suitable weight of linear explosive is employed so that the total explosive weight is as desired, the weight and spacing of the turns are such as to prevent cross-firing from one turn to another.
- FIGURE 2 shows the above embodiment of the invention positioned in a bore hole 21 penetrating a plurality of formations 22, 23 and 24.
- formation 23 and 24 are the formations of interest, and each has a different seismic-wave-propagation velocity.
- the helix diameter and pitch in that portion of the charge traversing each formation of interest are varied to provide an effective velocity of detonation approximately matching the velocity of the formation.
- the total explosive weight will be determined by the amount of the ammonium nitrate in the booster cartridge and the weight and length of the linear explosive.
- unit charges of varying lengths and varying angles of helical pitch may be made up beforehand.
- modular units of the AN/FO mixture may be provided, with the supplemental charge units inserted into the mandrel in the desired charge weight.
- linear explosive may be placed on the inside of the tube or in the tube wall, and the booster charge may be provided by an elongated slender sheath of AN/FO which is attached to the outside of the tubular mandrel so that it is in detonation relation with the linear explosive.
- the booster charge may be in tubular form, and the linear explosive may be in a suitable form other than a helix.
- the booster charge may be placed in a tube, such as a flexible plastic tube, with the linear explosive positioned directly on the surface of the tube, so that the composite charge may be wound upon a reel.
- the charge is used by unwinding and allowing it to be pulled down into the bore hole by a suitable weight.
- the following examples illustrate the effectiveness of the energy source described above.
- a number of tests were conducted in a shot hole in the earth at depths ranging from to feet.
- the explosive charges comprised long, slender plastic bags filled with an AN/FO mixture upon which were wound lengths of Primacord detonating fuse.
- a high-speed recorder was used to record the time interval required for detonation to proceed from end-to-end of the elongated test charge assembly, and a seismometer placed near the mouth of the shot hole was employed to measure the increase in seismic energy produced by the supplemental explosive detonated within the Primacord helices. The output of the seismometer was recorded on the recorder with the detonation velocity data.
- test charge assemblies were constructed using a mixture of prilled ammonium nitrate fertilizer and No. 2 diesel fuel in an amount of 6 percent by weight.
- the mixture was formed by pouring the oil over a measured quantity of ammonium nitrate and stirring in a plastic vessel to uniformly distribute the oil throughout the mass.
- the AN/FO mixture was inserted in polyvinyl chloride tubing having a wall thickness of about 0.020 inch and the ends were sealed with electrical tape and petroleum wax to provide a watertight enclosure for the explosive.
- the tubes were %inch ID. by 36-inches long and contained a net charge weight of /2 pound.
- the tubes filled with the explosive mixture were then inserted into larger diameter fiber tubes having an ID. of approximately 4 inch and which had been boiled in paraffin to increase their water resistance.
- the fiber tubes were then coupled end-to-end by inserting into their ends lengths of smaller tubing serving as couplings which provided a strong, forced fit.
- Primacord detonating fuse was then wound upon the outside of the tubes in the form of a helix and the ends of the Primacord winding were protected from water entry by aluminum thimbles. Detonation of the Primacord from one length of tube to the next was assured by lapping the ends of the cord from adjacent tubes and taping them in this position.
- An electric blasting cap was connected to the lower end of the Primacord. The time interval used in determining the velocity of detonation was measured between the instant of rupture of the cap at the lower end of the charge assembly and an electrical conductor broken by the blast as detonation neared the upper end of the Primacord helix.
- test A and test B 100 grain/foot Primacord was wound upon the mandrel with a helix spacing of 1 /2 inches to provide a total Primacord length of 17 feet over each of three 56-inch long by l /z-inch outside diameter fiber tubes described above.
- no ammonium nitrate booster was employed, while in test B three of the %-inch diameter by 36-inch long tubes of AN/FO mixture were employed as boosters, one in each of the above fiber tubes.
- the explosives were detonated in a bore hole under approximately 150 feet of water and the measured velocities were 7,610 feet per second for both tests.
- the measured seismic amplitude of test B was approximately double that measured in test A.
- test C was carried out as described above employing 60 grain per foot Primacord helically wound upon the above tubes with a l fir-inch spacing between the turns to provide a total Primacord length of 20 /2 feet on each 5-foot mandrel. Three mandrels were employed as before, with test D using no booster, while test C employed three of the boosters described above. The measured velocity of each of the detonations was 6,860 feet per second. The measured seismic amplitude in test C was approximately double that of test D.
- the present invention provides an improved method of increasing the total explosive Weight of the charge while maintaining the desired velocity of detonation, so that a more powerful, smoth-flowing energy source can be provided readily and economically.
- a controlled velocity explosive charge for use in seismic surveying which comprises:
- a first explosive element including a rigid tube of a selected length
- a second explosive element comprising a selected material in a slender cylindrical shape having a diameter D substantially smaller than the inner diameter of said tube so that said material can be freely inserted into said tube in a loosely fitting manner so that there is space between the interior of the tube and the second explosive element, said material chosen such that when in the form of a cylinder of diameter D it is not capable of self-sustaining detonation;
- (c) means to detonate said first explosive element.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
Description
April 1966 H. M. LANG ETAL 3,244,099
CONTROLLED VELOCITY EXPLOSIVE CHARGE FOR SEISMIC EXPLORATION Filed Nov. 12, 1963 FIG. 2
l7 HAROLD M. LANG THOMAS K. FULTON INVENTORS.
I 4% BY ATTORNEY.
United States Patent Othce 3,244,099 Patented Apr. 5, 1966 3,244,099 CONTROLLED VELOCITY EXPLOSIVE CHARGE FOR SEISMHC EXPLORATION Harold M. Lang and Thomas K. Fulton, Tulsa, Okla,
assignors to Pan American Petroleum Corporation,
Tulsa, Okla., a corporation of Delaware Filed Nov. 12, 1963, Ser. No. 322,758 3 Claims. (Cl. 102-20) This invention relates to controlled velocity explosive charges, and more particularly, it is directed to an improvement in the generation of seismic waves for use in geophysical surveying.
Heretofore, elongated distributed explosive charges have been proposed for use in seismic surveying, wherein the effective detonation velocity of the charge is matched approximately to the seismic wave transmision velocities of the medium surrounding the charge. Such distributed charges have been found very useful in discriminating against the generation of seismic noise and in preventing undue damage to the surrounding medium. An example of the above-mentioned distributed charge is Silverman U.S. Patent 2,609,885 disclosing an explosive charge employing a helix of a linear explosive, such as Primacord detonating fuse, the helix having a pitch providing an effective detonation velocity equal to the wave transmission velocity of the surrounding formations in the direction of detonation. Also, Lang US. Patent 2,846,019 discloses a method of generating seismic waves employing an explosive mixture of fuel gas and oxygen wherein the composition of the explosive gas mixture is adjusted to provide a velocity of detonation matched with the seismic wave transmission velocity of the adjacent formations.
With such seismic charges as mentioned above, it is oftentimes desirable to increase the explosive weight of the charges over that inherent in the velocity matching charge itself so that a greater force is applied to the (formation upon detonation of the charge. Certain limitations exist on the explosive weight of the helical linear explosive and the explosive gas method has so far found only limited use in its application. In the use of the helical linear explosive, a practice has been to supplement the charge weight by coupling spaced-apart packages of canned explosives, such as Nitramon, into the linear explosive array. However, such addition of explosives to the distributed charge assembly results in lump charges, which cause the flow of explosive energy into the earth to be pulsed, rather than providing a smooth flow of energy, as is desirable from a uniformly distributed charge. Also, these lumps usually detonate at a velocity greater than that of the helical linear explosive, presenting considerable difficulties in designing such a charge to match the velocity of a specified formation. Additionally, the concentrated energy of such a charge lump may damage the ensuing distributed charge elements to cause failure of the detonation.
A primary object of the present invention is an improved distributed charge useful as an energy source for generating seismic waves, which charge has a controllable velocity of detonation and an adjustable weight of explosive. A further object is such an energy source providing a uniform flow of explosive energy. Still a further object is such an energy source having a uniform detonation velocity. A still further object of the invention is such an energy source which is readily fabricated to provide the desired explosive weight and detonation velocity, while at the same time being relatively economical. These and further objects of the invention will become more apparent by reference to the following description of the invention and to the accompanying drawings wherein:
FIGURE 1 illustrates a vertical cross-sectional view of a preferred form of an energy source according to the invention; and
FIGURE 2 illustrates a cross-sectional view of a bore hole with an energy source of the invention positioned in the bore hole.
According to the invention, the continuous priming principle is employed to provide a unique explosive charge having a controllable velocity of detonation, An elongated composite charge is provided utilizing a first explosive component producing a preselected effective velocity of detonation and being capable of self-sustaining detonation, and a second explosive component being incapable of self-sustaining detonation, but being detonable by the first component. The two explosive components are placed in detonation relation with each other so that, upon detonation of the first component, detonation proceeds along the length of the composite charge at a velocity substantially equal to the effective velocity of detonation of the first component.
As disclosed by the above-mentioned US. Patent 2,609,- 885, a linear explosive having a known velocity of detonation, which is at least as great as the seismic wave velocity of the surrounding medium, may be arranged in a helix or other suitable shape to provide a vertical distributed charge having an effective velocity of detonation matched with the seismic wave transmission velocity of the formations surrounding the charge. As used herein, the term effective detonation velocity refers to that component of the detonation velocity in the direction of the vertical axis of the charge. Various linear explosives may be employed in practicing the present invention to provide the desired velocity and directional properties and to continuously prime the supplemental charge. Preferably, a detonating fuse, such as the material known as Primacord, is employed as the linear explosive. Primacord is granular pentaerythritol tetranitrate (PETN) in a braided cord with a plastic sheath confining and protecting the explosive. Other similar explosives, such as cyclotrimethylenetrinitramine (RDX), or the like, suitable for use as a detonating fuse or priming material may be used, Other forms such as a tube or rod of the explosive, typically formed by inserting a powder or granules of explosive in a sheath, such as flexible plastic tube, or a precast rigid groove may be utilized. Certain explosives of this type must be waterproofed. Various linear explosives are available in differing explosive weights and velocities of detonation, and the shape of the particular linear explosive selected may be varied to produce the desired effective velocity of detonation, as by controlling the pitch of the helical turns. Generally, when employing a helical shape it is advantageous to have the turns spaced as closely as possible and the smallest linear explosive capable of initiating and sustaining detonation of the supplemental explosive is therefore preferred so that the possibility of cross-firing, i.e., firing across the turns, is reduced.
The composite charge comprises a second explosive component employed as a booster charge to supplement the linear explosive and provide the desired total charge weight. It is an essential feature of the invention that the booster charge be formed of an explosive which is incapable of self-sustaining detonation, but which is detonable by the continuous priming action of the adjacent linear explosive. It has been determined that elongated slender cartridges, or slender columns, of ammonium nitrate explosives, such as a mixture of ammonium nitrate and fuel oil (AN/F0), are incapable of selfpropagation of detonation when the diameter of the column falls below a critical minimum diameter, although the explosive is self-sustaining when formed into large diameter columns. For example, a well-packed column of AN/FO with a diameter of 1 /2 inches is capable of self-sustaining detonation, while for diameters less than about 1 /2 inches, detonation, once beyond the influence of the primer, will slow and fail in about 2 /2 column diameters. Other of the well-known explosives are likewise incapable of self-sustaining detonation when formed into a shape having a cross section less than the minimum necessary, and these are suitable for use in the practice of our invention, although all are not necessarily of equal effectiveness for this purpose. For example, the various ammonium nitrate explosives, such as ammonium nitrate mixed with up to about percent of a carbonaceous material may be used. Typically, about 4 to 8 percent of a liquifiabl-e hydrocarbon, such as fuel oil is employed. The ammonium nitrate explosive may be formulated with any of the well-known organic or inorganic sensitizers, and a light metal, such as magnesium or aluminum, may be incorporated in the explosive, if desired. Also, the straight dynamites, ammonia dynamites or gelatine dynamites may be employed.
The critical minimum cross section of the booster charge will vary, depending upon the particular explosive formulation, the method of manufacture, the density and other such factors. It is known that certain explosives, such as AN/FO or the like, are rendered less sensitive to detonation by moisture pick-up or by an increase in density, so that a charge of the explosive which is otherwise capable of self-sustaining detonation may be made incapable of self-sustaining detonation when such factors are varied. If the cross section of such a charge is increased above the critical dimension, the charge will again become selfpropagating. However, the critical cross section may be determined readily by various well-known tests. For example, a cone-shaped sample of the explosive may be detonated at the base of the cone and the diameter of the point of failure of propagation determined. It is critical to the invention that this critical diameter of the booster charge not be exceeded, or the booster will become self-propagating, and the elfectiveness of the composite charge will be reduced.
As mentioned above, a preferred construction of the composite explosive charge comprises a helical linear explosive surrounding a long slender column of otherwise nondetonable booster charge. The linear explosive and the booster charge are positioned closely adjacent each other, so that the two are in detonation relation over the length of the charge. The linear explosive continuously primes the otherwise nondetonable booster, and the two must be positioned so that the shock wave from the primer is of great enough magnitude to induce and sustain detonation in the column of booster. If this condition is absent, detonation of the column of booster charge will not proceed along its length, but will slow and fail, even though once begun. If the two explosive components are in detonation relation, the detonation will proceed at a velocity substantially equal to the eflective velocity of detonation of the linear explosive.
Turning now to FIGURE 1, there is shown a preferred embodiment of the explosive charge of the invention. An elongated, slender cartridge, or column which may be solid or cored, of AN/FO explosive is formed from a mixture of commercial grade ammonium nitrate and about 2 to 10 percent fuel oil. The mixture is inserted into a long, relatively thin-wall tubular mandrel 11 having an internal diameter suitable for holding a column of booster charge of a diameter less than the critical minimum diameter required for self-propagation of detonation of the ammonium nitrate explosive. Typically, the tube, or mandrel, is formed of fiber or cardboard which may be waterproofed by impregnation with paraffin or a suitable resin. Within the above-mentioned limits the diameter and length of the column 12 of the ammonium nitrate explosive may be varied according to the total explosive charge weight desired. In the instance of the ammonium nitrate explosive referred to above, this diameter typically may vary from A inch to 1% inches.
Wrapped around the mandrel 11 and in detonation relation with the ammonium nitrate booster is a helix of linear explosive 13, formed of Prirnacord detonating fuse which encloses the ammonium nitrate column for substantially its complete length. Connected to one end of the linear explosive is an electric blasting cap 14, or another suitable detonator, connected by electrical leads 16 to a suitable power source. If desired, perforations 17 may be provided in the mandrel wall to permit the entry of fluids into the mandrel interior to reduce buoyancy so that the explosive charge may be more easily placed at a desired depth in water of a fluid-filled bore hole. The column of booster may be enclosed in a waterproofed container, such as flexible plastic bag 18. The pitch of the helix is chosen to provide the desired effective velocity of detonation in the manner herein described, and a suitable weight of linear explosive is employed so that the total explosive weight is as desired, the weight and spacing of the turns are such as to prevent cross-firing from one turn to another.
The above-mentioned elongated composite explosive charge typically may be made up in 3- to 8-foot lengths and these lengths may be coupled together with a suitable coupling unit to provide a unit of the desired overall length. FIGURE 2 shows the above embodiment of the invention positioned in a bore hole 21 penetrating a plurality of formations 22, 23 and 24. Typically, formation 23 and 24 are the formations of interest, and each has a different seismic-wave-propagation velocity. The helix diameter and pitch in that portion of the charge traversing each formation of interest are varied to provide an effective velocity of detonation approximately matching the velocity of the formation.
As mentioned above, the total explosive weight will be determined by the amount of the ammonium nitrate in the booster cartridge and the weight and length of the linear explosive. Typically unit charges of varying lengths and varying angles of helical pitch may be made up beforehand. Similarly, modular units of the AN/FO mixture may be provided, with the supplemental charge units inserted into the mandrel in the desired charge weight.
While the abovedescribed helical configuration of linear explosives mounted upon a slender column of ammonium nitrate has been found to provide exceptional results, it is within the scope of the invention to employ other shapes of linear explosive and booster charge. For example, the linear explosive may be placed on the inside of the tube or in the tube wall, and the booster charge may be provided by an elongated slender sheath of AN/FO which is attached to the outside of the tubular mandrel so that it is in detonation relation with the linear explosive. Similarly, the booster charge may be in tubular form, and the linear explosive may be in a suitable form other than a helix. Also, the booster charge may be placed in a tube, such as a flexible plastic tube, with the linear explosive positioned directly on the surface of the tube, so that the composite charge may be wound upon a reel. In this latter instance the charge is used by unwinding and allowing it to be pulled down into the bore hole by a suitable weight.
The following examples illustrate the effectiveness of the energy source described above. A number of tests were conducted in a shot hole in the earth at depths ranging from to feet. The explosive charges comprised long, slender plastic bags filled with an AN/FO mixture upon which were wound lengths of Primacord detonating fuse. A high-speed recorder was used to record the time interval required for detonation to proceed from end-to-end of the elongated test charge assembly, and a seismometer placed near the mouth of the shot hole was employed to measure the increase in seismic energy produced by the supplemental explosive detonated within the Primacord helices. The output of the seismometer was recorded on the recorder with the detonation velocity data.
The test charge assemblies were constructed using a mixture of prilled ammonium nitrate fertilizer and No. 2 diesel fuel in an amount of 6 percent by weight. The mixture was formed by pouring the oil over a measured quantity of ammonium nitrate and stirring in a plastic vessel to uniformly distribute the oil throughout the mass. The AN/FO mixture was inserted in polyvinyl chloride tubing having a wall thickness of about 0.020 inch and the ends were sealed with electrical tape and petroleum wax to provide a watertight enclosure for the explosive. The tubes were %inch ID. by 36-inches long and contained a net charge weight of /2 pound.
The tubes filled with the explosive mixture were then inserted into larger diameter fiber tubes having an ID. of approximately 4 inch and which had been boiled in paraffin to increase their water resistance. The fiber tubes were then coupled end-to-end by inserting into their ends lengths of smaller tubing serving as couplings which provided a strong, forced fit. Primacord detonating fuse was then wound upon the outside of the tubes in the form of a helix and the ends of the Primacord winding were protected from water entry by aluminum thimbles. Detonation of the Primacord from one length of tube to the next was assured by lapping the ends of the cord from adjacent tubes and taping them in this position. An electric blasting cap was connected to the lower end of the Primacord. The time interval used in determining the velocity of detonation was measured between the instant of rupture of the cap at the lower end of the charge assembly and an electrical conductor broken by the blast as detonation neared the upper end of the Primacord helix.
In test A and test B, 100 grain/foot Primacord was wound upon the mandrel with a helix spacing of 1 /2 inches to provide a total Primacord length of 17 feet over each of three 56-inch long by l /z-inch outside diameter fiber tubes described above. In test A no ammonium nitrate booster was employed, while in test B three of the %-inch diameter by 36-inch long tubes of AN/FO mixture were employed as boosters, one in each of the above fiber tubes. The explosives were detonated in a bore hole under approximately 150 feet of water and the measured velocities were 7,610 feet per second for both tests. The measured seismic amplitude of test B was approximately double that measured in test A.
A similar test was carried out as described above employing 60 grain per foot Primacord helically wound upon the above tubes with a l fir-inch spacing between the turns to provide a total Primacord length of 20 /2 feet on each 5-foot mandrel. Three mandrels were employed as before, with test D using no booster, while test C employed three of the boosters described above. The measured velocity of each of the detonations was 6,860 feet per second. The measured seismic amplitude in test C was approximately double that of test D.
From the above-described tests it is apparent that the present invention provides an improved method of increasing the total explosive Weight of the charge while maintaining the desired velocity of detonation, so that a more powerful, smoth-flowing energy source can be provided readily and economically.
The above description and examples have been given for the purpose of illustrating our invention, and from the foregoing, various modifications and alterations in the details of construction and operation, falling within the spirit and scope of our invention will become apparent to the artisan.
We claim:
1. A controlled velocity explosive charge for use in seismic surveying which comprises:
(a) a first explosive element including a rigid tube of a selected length, and
a continuous helix of linear explosive composition wrapped around said tube with said helix having a pitch providing an effective selected detonation velocity along the length of said tube;
(b) a second explosive element comprising a selected material in a slender cylindrical shape having a diameter D substantially smaller than the inner diameter of said tube so that said material can be freely inserted into said tube in a loosely fitting manner so that there is space between the interior of the tube and the second explosive element, said material chosen such that when in the form of a cylinder of diameter D it is not capable of self-sustaining detonation; and
(c) means to detonate said first explosive element.
2. An explosive charge as defined in claim 1 in which said selected material of said second explosive element is enclosed in a water-proof bag and said rigid tube has a perforation in the wall thereof whereby When such explosive charge is placed in a hole containing water the buoyancy thereof is reduced so that the explosive charge may be more easily placed at a desired depth.
3. An explosive charge as defined in claim 1 in which said material of said second explosive element comprises an ammonium nitrate explosive having not over 10% carbonaceous fuel and a diameter in the range from about A to about 1%" such that it is incapable of self-sustaining detonation.
References Cited by the Examiner UNITED STATES PATENTS 2,468,274 4/ 1949 Riley 10224 2,586,706 2/1952 Parr 10222 X 2,837,997 6/1958 Woods 102-24 3,082,689 3/ 1963 Griffith et al. 102-24 3,095,812 6/1963 Coursen 10227 BENJAMIN A. BORCHELT, Primary Examiner. SAMUEL FEINBERG, Examiner.
V. R. PENDEGRASS, Assistant Examiner.
Claims (1)
1. A CONTROLLED VELOCITY EXPLOSIVE CHARGE FOR USE IN SEISMIC SURVEYING WHICH COMPRISES: (A) A FIRST EXPLOSIVE ELEMENT INCLUDING A RIGID TUBE OF A SELECTED LENGTH, AND A CONTINUOUS HELIX OF LINEAR EXPLOSIVE COMPOSITION WRAPPED AROUND SIDE TUBE WITH SAID HELIX HAVING A PITCH PROVIDING AN EFFECTIVE SELECTED DETONATION VELOCITY ALONG THE LENGTH OF SAID TUBE; (B) A SECOND EXPLOSIVE ELEMENT COMPRISING A SELECTED MATERIAL IN A SLENDER CYLINDRICAL SHAPED HAVING A DIAMETER D SUBSTANTIALLY SMALLER THAN THE INNER DIAMETER OF SAID TUBE SO THAT SAID MATERIAL CAN BE FREELY INSERTED INTO SAID TUBE IN A LOOSELY FITTING MANNER SO THAT THERE IS SPACE BETWEEN THE INTERIOR OF THE TUBE AND THE SECOND EXPLOSIVE ELEMENT, SAID MATERIAL CHOSEN SUCH THAT WHEN IN THE FORM OF A CYLINDER OF DIAMETER D IT IS NOT CAPABLE OF SELF-SUSTAINING DETONATION; AND (C) MEANS TO DETONATE SAID FIRST EXPLOSIVE ELEMENT.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US322758A US3244099A (en) | 1963-11-12 | 1963-11-12 | Controlled velocity explosive charge for seismic exploration |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US322758A US3244099A (en) | 1963-11-12 | 1963-11-12 | Controlled velocity explosive charge for seismic exploration |
Publications (1)
Publication Number | Publication Date |
---|---|
US3244099A true US3244099A (en) | 1966-04-05 |
Family
ID=23256275
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US322758A Expired - Lifetime US3244099A (en) | 1963-11-12 | 1963-11-12 | Controlled velocity explosive charge for seismic exploration |
Country Status (1)
Country | Link |
---|---|
US (1) | US3244099A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3760639A (en) * | 1972-10-20 | 1973-09-25 | Bio Data Corp | Pipette assembly |
US4240349A (en) * | 1978-09-11 | 1980-12-23 | Lash Charles C | Foldable linear explosive charge |
US4284006A (en) * | 1979-08-13 | 1981-08-18 | Davis Explosive Sources, Inc. | Linear explosive charge with constant detonation velocity and synchronous booster charges |
WO2000045123A2 (en) * | 1999-01-20 | 2000-08-03 | The Ensign-Bickford Company | Accumulated detonating cord charge, method and use |
WO2000055105A2 (en) * | 1999-03-17 | 2000-09-21 | Input/Output, Inc. | Explosive shear wave energy source |
US20060048664A1 (en) * | 2004-09-08 | 2006-03-09 | Tiernan John P | Propellant for fracturing wells |
US20090223668A1 (en) * | 2008-03-05 | 2009-09-10 | Schlumberger Technology Corporation | Sympathetic ignition closed packed propellant gas generator |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2468274A (en) * | 1944-07-29 | 1949-04-26 | Hercules Powder Co Ltd | Explosive device |
US2586706A (en) * | 1949-01-12 | 1952-02-19 | Olive S Petty | Seismic surveying |
US2837997A (en) * | 1954-08-03 | 1958-06-10 | Texas Co | Explosive container holder and explosive assembly employing same |
US3082689A (en) * | 1960-01-05 | 1963-03-26 | Trojan Powder Co | Detonatable cartridges having insensitive explosive cores |
US3095812A (en) * | 1957-09-10 | 1963-07-02 | Du Pont | Explosive means |
-
1963
- 1963-11-12 US US322758A patent/US3244099A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2468274A (en) * | 1944-07-29 | 1949-04-26 | Hercules Powder Co Ltd | Explosive device |
US2586706A (en) * | 1949-01-12 | 1952-02-19 | Olive S Petty | Seismic surveying |
US2837997A (en) * | 1954-08-03 | 1958-06-10 | Texas Co | Explosive container holder and explosive assembly employing same |
US3095812A (en) * | 1957-09-10 | 1963-07-02 | Du Pont | Explosive means |
US3082689A (en) * | 1960-01-05 | 1963-03-26 | Trojan Powder Co | Detonatable cartridges having insensitive explosive cores |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3760639A (en) * | 1972-10-20 | 1973-09-25 | Bio Data Corp | Pipette assembly |
US4240349A (en) * | 1978-09-11 | 1980-12-23 | Lash Charles C | Foldable linear explosive charge |
US4284006A (en) * | 1979-08-13 | 1981-08-18 | Davis Explosive Sources, Inc. | Linear explosive charge with constant detonation velocity and synchronous booster charges |
US6880465B2 (en) | 1999-01-20 | 2005-04-19 | Dyno Nobel Inc. | Accumulated detonating cord explosive charge and method of making and of use of the same |
WO2000045123A3 (en) * | 1999-01-20 | 2001-02-01 | Ensign Bickford Co | Accumulated detonating cord charge, method and use |
US6508176B1 (en) | 1999-01-20 | 2003-01-21 | The Ensign-Bickford Company | Accumulated detonating cord explosive charge and method of making and of use of the same |
US20040025734A1 (en) * | 1999-01-20 | 2004-02-12 | Badger Farrell G. | Accumulated detonating cord explosive charge and method of making and of use of the same |
WO2000045123A2 (en) * | 1999-01-20 | 2000-08-03 | The Ensign-Bickford Company | Accumulated detonating cord charge, method and use |
WO2000055105A2 (en) * | 1999-03-17 | 2000-09-21 | Input/Output, Inc. | Explosive shear wave energy source |
WO2000055105A3 (en) * | 1999-03-17 | 2001-05-31 | Input Output Inc | Explosive shear wave energy source |
US20060048664A1 (en) * | 2004-09-08 | 2006-03-09 | Tiernan John P | Propellant for fracturing wells |
US7409911B2 (en) * | 2004-09-08 | 2008-08-12 | Propellant Fracturing & Stimulation, Llc | Propellant for fracturing wells |
US20080264289A1 (en) * | 2004-09-08 | 2008-10-30 | Propellant Fracturing & Stimulation, Llc | Propellant for fracturing wells |
US20090223668A1 (en) * | 2008-03-05 | 2009-09-10 | Schlumberger Technology Corporation | Sympathetic ignition closed packed propellant gas generator |
US8186425B2 (en) * | 2008-03-05 | 2012-05-29 | Schlumberger Technology Corporation | Sympathetic ignition closed packed propellant gas generator |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10443361B2 (en) | Multi-shot charge for perforating gun | |
US10000994B1 (en) | Multi-shot charge for perforating gun | |
US4313380A (en) | Distributed charge for seismic prospecting | |
US5099763A (en) | Method of blasting | |
US4064935A (en) | Oil well stimulation apparatus | |
US4329925A (en) | Fracturing apparatus | |
US5388521A (en) | Method of reducing ground vibration from delay blasting | |
US6648097B2 (en) | Seismic methods having extended energy release | |
US5071496A (en) | Low level blasting composition | |
US3150590A (en) | Explosive charge unit | |
US3702635A (en) | Seismic energy source using liquid explosive | |
US2609885A (en) | Seismic-wave generation | |
US3244099A (en) | Controlled velocity explosive charge for seismic exploration | |
US2238939A (en) | Blasting assembly | |
US2823609A (en) | Device for seismic prospecting | |
US3021785A (en) | Counterforce initiation | |
US2992611A (en) | Seismic prospecting device | |
US3289583A (en) | Explosive charge | |
US3968724A (en) | Method for accurately varying the density of a powder or powder charge, and shrink tubes for use therewith | |
US4161142A (en) | Blasting booster and methods | |
US2846019A (en) | Generating seismic waves | |
US2953214A (en) | Seismic exploration | |
US3729060A (en) | Seismic prospecting | |
US4002119A (en) | Method for in situ assembly of charge for controlled shooting of wells | |
US4166417A (en) | Explosive boosting device for low-sensitivity blasting agents |