US2475875A - Explosive assembly - Google Patents
Explosive assembly Download PDFInfo
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- US2475875A US2475875A US783976A US78397647A US2475875A US 2475875 A US2475875 A US 2475875A US 783976 A US783976 A US 783976A US 78397647 A US78397647 A US 78397647A US 2475875 A US2475875 A US 2475875A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D1/00—Blasting methods or apparatus, e.g. loading or tamping
- F42D1/04—Arrangements for ignition
- F42D1/06—Relative timing of multiple charges
Description
L. A. BURROWS ET AL July 12, 1949.
EXPLOS IVE AS SEMBLY Original Filed Aug. 7, 1943 lll Il II IIS JNVENToRS LAURRon/J By RM GJRDLER A T TORNEV Patented July l2, 1949 v EXPLOSIVE ASSEMBLY Lawton A. Burrows, Mendenhall, Pa., and Robert M. Girdler, Wenonah, N. J.,'assignors to E. I.
du Pont de Nemours & Company, Wilmington, Del., a. corporation of Delaware Continuation of application Serial' No. 497,736,y August 7, 1943. This application November 4, 1947, Serial No. 783,976
This invention relates to 'a novel method of blasting wherel a number of explosive charges are to be red and more particularly to the use of a new type of detonator in the firing of explosives.
This application is a continuation of copending application No. 497,736.
A common practicegin quarrying limestone and other types of rock is to drill deep vertical holes at denite distances back fromthe face and to load these with the desired amount of explosive. Such vertical holes may be from 30 to 100 feet deep and perhaps 20 feet apart. In many quarry blasts, it may be desired to shoot a large number of drill holes, up to 40 or- 50 for example. In such a case it is customary to drill a certain number of these parallel to the face and at the desired distance therefrom and to arrange the remainder of the holes in one or more rows further removed from the face and substantially parallel to the front row. l
Blast holes such as the above may be up to 9 inches in diameter and are loaded with the desired amount of explosive in cartridge diameter corresponding to the diameter of the holes. With such charges in deep holes, a safe and convenient method of detonating the explosive is by use of detonating fuse, which consists of a core of high velocity explosive enclosed in an outer casing of fabric or metal. Such fuseunder the influence of a blasting cap may detonate at a velocity as high as 20,000 feet per second. With a deep bore-hole loaded with explosive, the introduction of a length of detonating fuse to the bottom of the hole alongside the cartridges insures the practically instantaneous detonation of all the explosive, When anumber of holes are charged in the same manner and are connected by trunk lin'esof detonating fuse, the electiveness and certainty of the blastrare assured.
The same procedure may be used when several rows of holes back of vthe quarryrface are to be blasted and where the back rows are joinedto the trunk line of detonating fuse by connecting lines.y With such a large number of blast holes 'and with the quantity of explosive involved, the simultaneous explosion of all the charges may cause anundesirable degreel of earth vibration. If such explosions could bevfcaused to take place successively, hole by hole, such excessive vibration would be avoided. also, from the pointvof view of blasting execution, to have theI front row holes shoot rst, followed at a proper time interval bythe second row, etc.
An object of the present invention is an im- -proved method of blasting' where explosion of A It may be advantageous 3 Claims. (Cl. 102-22) vare by means of detonating fuse.
more than one charge is desired, v said blaststo be separated by denite time intervals. A furtheir object'is such a method applied to quarry blasting Where the connections between charges A still further object is an explosion-retarding device adapted to be inserted in the lines connecting the various holes for successive firing and to bring about such result. A further object is an explosive assembly comprising such arrangement of` lines of detonating fuse and delay devices adapted to accomplish successive firing of charges. Additional objects will be disclosed as the invention is described with greater exactness and detail in the following.
We accomplish the foregoing objects by connecting the explosive charges by means of detonating fuse, and introducing into the line lead.- ing to the charge or charges intended for later ring a delay element, that is to say a device that may be connected to the two lines of fuse and that comprises a container having at one end an ignition charge capable of initiation by the detonating fuse coming from the rst charge, a deagrating charge adjacent to the ignition charge and capable of being fired by said ignition charge, of burning at a predetermined rate and of igniting and bringing todetonation a charge at the second end of the delay element container.
This latter charge is capable of propagating the explosion to the second line of detonating fuse and thence to the explosivecharge Whose later firing is desired. While we preferably use a separate ignition charge, this may be omitted if adelay composition is employed that can be ignited by the detonating fuse. e
While the invention is applicable to any group of two or more explosive charges for firing by detonating fuse where successive rather than instantaneous detonation of the`various. charges is desired, a particular application will be to quarry blasting Where deep holes of relatively large vdiameter yare charged with highexplosive and lines of detonatingfuse go to the bottom of each hole, hence are in contact with the entire charge. In suchya caseI the earth vibrations and the noise aregreatly rcducedand practically all the objectionable features overcome if the method of our invention is followed. f
As a delay element for insertion in the line of detonating fuse, We employ a containerfor explosive charges, preferably aY cylindrical metal shell into which. or against which. the detonating fuse is introduced. The various combustible and explosive charges are enclosed in said container.
in any way. Figure 1 is a view of a delay device interposed between two lines of detonating fuse. Figure 2 is a diagrammatic representation of a layout of a quarry shot, showing the position of the blast holes with reference to the quarry face, one scheme for connecting said holes, and showing also the place of introduction of the delay elements.
In Figure 1, which shows a suitable delay device, I represents aline of detonating fuse having a core 2 of PETN and butting against a small diameter cylindrical column 3 of combustible ignition mixture contained in the constricted end positions can be used, a suitable one comprises 51% mercury fulminate, 23% potassium chlorate, 9% nitrostarch, and 17% charcoal, this being made into a paste with a suitable solvent.
'Adjoining the ignition mixture is a charge 5 of an 88-12 blend of barium peroxide and magneslum, e. g., 2.5 grams, which is adapted to burn relatively slowly and which gives 01T substantially of the steel carrier 4. While various comno gas on combustion. This delay charge fills the enlarged portion of the steel carrier 5 and extends into a, portion of the copper shell 6, within which the steel carrier is partly enclosed. The base of the copper shell contains a pressed charge 'I of l gram of an 80-20 mixture of mer-l potassium chlorate. The
cury fulminate and copper shell butts against the line of detonating fuse having the core 8 of compressed PETN. A cardboard tube 9 surrounds the copper shell and the detonating fuse at each end and holds these objects rmly together when the metal bands, IIJ and II, are crimped thereto.
In actual use, where at least two explosive charges are to be detonated with a predetermined time interval between, the detonating fuse I coming from the charge rst red propagates the explosion at a velocity of around 20,000 feet per second and eiects the ignition of the composition 3, which in turn ignites the defiagrating charge 5. This burns at a relatively slow predetermined rate and, after the desired retardation, effects ignition of the charge 1 which rapidly picksup to high velocity and brings about the high velocity detonation of the detonating fuse B, leading to the second explosive charge.
In Figure 2, I3 represents a quarry face with vertical drill holes of approximately 6 inches diameter and 50 feet deep. A row of 5 holes, 14A to IIE, parallels the face, about 20 feet back from said face and spaced about I6 feet apart. A second row of 5 holes, I5A to I5E, and a third row of holes, IGA to IEE, are still farther back from the face. These are loaded with a suitable explosive, for example 60% ammonia gelatin dynamite, about 750 lb. per hole. A trunk line of detonating fuse, which comprises an explosive core of PETN contained within a waterproofed textile covering, connects the holes in the row nearest the face, IIA to ME, and branch lines of this same fuse run to the bottom of each hole, being held in contact with the individual explosive cartridges so that the detonation of the fuse will cause the substantially instantaneous detonation of all the explosive. Connecting lines of detonating fuse lead off from the main trunk line, in advance of the rst hole,
NA, and beyond the last hole, IAE. These lines connect the second row of holes, I5A to I5E. Similarly additional connecting lines of fuse go to the third row of holes, IGA to ISE. Interposed in each line leading from the front row of hole:` tothe second row and from' they second to the third row are delay elements, I8 and I9, of the type shown in Figure 1, which contain charges of relatively slow rates of combustion adapted to cause the explosive in the-s rows to re at successively later times. Double connections between the row of holes for successive blasting are shown in the drawing and will ordinarily be employed as assurance against misflres, though only one connection is actually required.
In the quarry assembly shown in Figure 2, the connections are such as to cause a whole row of holes to re at one time. By the use of delay devices between the successive rows of holes, time intervals of a few hundredths of a second are effected between the times of detonation of the successive shots. The detonating fuse commonly used, Primacord, explodes at a velocity of around 20,000 feet per second, so that when this fuse is initiated by means of an electric blasting cap I1, on application of the electric current by means of a blasting machine, the charges in the holes in the front row detonate almost instantaneously and simultaneously. This causes the blasted rock to move away from the face. After a suitable delay interval, charges in the second row of holes I5A to I5E, detonate. Delay elements I9 in the fuse lines leading from the second to the third row of holes cause a similar time interval' between the firing of charges in holes in these respective rows. The moving away of a large amount of rock in front of each row of holes before the blasting in such rows adds to the effectiveness of the blast. An even greater advantage is the very considerable reduction in the noise and particularly the vibrational eil'ects of the blast. Delay intervals of from 0.01 to 0.08 seconds may be used, the
preferable delay intervals being from 0.01 to 0.05 seconds. We may carry out the invention and bring about an even greater reduction in earth vibrations by causing the holes to detonate one at a time, rather than by rows. This necessitates interposing delay elements in the line of Primacord before each hole, with the exception of the rst hole.
In carrying out the present invention, any type of detonating fuse is applicable. The specific example has shown the use of Primacord, which is a detonating fuse having a core of PETN enclosed in a fabric covering and having a velocity of around 20,000 feet per second. Cordeau is likewise applicable, a lead-wrapped fuse of somewhat lower velocity, around 17,500 feet per second, having a core of TNT.
Various compositions may be used for the delay charge in the connecting element or detonator, for example blends of barium peroxide and magnesium, barium peroxide and selenium, potassium permanganate and antimony, and the like. The foregoing are advantageous in that they produce substantially no gases on combustion. Various gas-producing compositions are applicable also, however,'such as black powder and nitrocellulose compositions.
It is recognized that delay electric blasting caps are known in the art which bring about the explosion of charges after definite time intervals. The delay devices of the present invention are novel, however, in that they are adapted to be nitiated by an extremely high velocity detonation vave. The explosion is transmitted to the igni- ;ion composition of the delay device. thence to the lelay composition, where it travels at a low 'elocity, possibly around 0.5 meter and well under ive meters per second. The delay composition :auses the subsequent ignition of the detonating gomposition at the base of the shell which picks lp rapidly to detonating velocity, such that it `lfectively detonates the juxtaposed line of deto- .ating fuse. Any ignition composition Ithat is apable of receiving a detonation wave and transhitting it as simple combustion under the condiions outlined is suitable. We have found an tfective composition to comprise 51% mercury ulminate, 23% potassium chlorate, 9% nitrotarch and 17% charcoal, thoroughly blended nd made into a paste by use of a suitable solvent. rarious compositions are likewise adapted to Jllow the delayA composition, for example an 20 fulminate-chlorate mixture. lead azide ompositions, nitromannite, diazodinitrophenol nd the like. A
In carrying out the invention', it will be under- ;ood that it is not limited in any way by the Vpe of explosive in the holes to be blasted, or sewhere, except that they must be detonating zplosives adapted for explosion by means of etonating fuse. In the case of quarrying operaons, such high explosives are commonly used as nmonia dynamites, Straight dynamites, gelatin mamites, blasting agents containing high perentages of ammonium nitrate and free from luid explosive, and many others. Many variations in exact'procedures and details assembly may be employed, therefore, without aparture from the scope of the invention. While s use in such operations as quarry blasting and le like has been emphasized, it will be underood that it is applicable to all uses of explosive, nether commercial or military, where more than le explosive charge is to be red by means of etonating fuse, and in fact to all ring of sucssive lengths of detonating fuse, which are sepated by delay elements of the type described. `e intend to be limited only by the following .tent claims:
We claim:
1. An explosive assembly for use where two nnected lengths of detonating fuse are prest and Where the second length is to be red at lelayed time interval after the iirst length, said sembly comprising an explosion-retarding elernt interposed between said lengths of detonatg fuse and butted up against them in detonating relationship therewith, said element containing at the end adjacent to the rst length of fuse an initiating dei'lagrating charge, at the end adjacent to the second length of fuse a detonating charge, and intermediate the initiating and detonating charges a delay composition, said charges being cent to the iirst length of4 fuse an initiating deiiagrating charge, at the end adjacentto the second length of fuse a detonating charge, and intermediate the deiiagrating and the detonating charges a delay composition, said charges in said retarding elements being such as to propagate the explosion at renewed high velocity beyond the retarding elements from the ilrst length to the second length of detonating fuse.
3. An explosive assembly according to claim 2, in which more than one series of explosive charges are to be fired, where practically instantaneous ring of the charges within each series is desired and where a delayed time interval is desired between the successive series of charges for instantaneous ring, said assembly comprising the connection of each of the series of charges for instantaneous iiring by the explosion-retarding element.
LAWION A. BURROWS.
ROBERT M. GIRDLER.
REFERENCES CITED 'The following references are of record in the le of this patent:
UNITED STATES PATENTS .113,411 Australia July 2, 1941
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US783976A US2475875A (en) | 1943-08-07 | 1947-11-04 | Explosive assembly |
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Application Number | Priority Date | Filing Date | Title |
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US588613XA | 1943-08-07 | 1943-08-07 | |
US783976A US2475875A (en) | 1943-08-07 | 1947-11-04 | Explosive assembly |
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US2475875A true US2475875A (en) | 1949-07-12 |
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US783976A Expired - Lifetime US2475875A (en) | 1943-08-07 | 1947-11-04 | Explosive assembly |
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Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2546686A (en) * | 1947-03-21 | 1951-03-27 | Du Pont | Blasting device |
US2609750A (en) * | 1946-05-16 | 1952-09-09 | Atlas Powder Co | Process of blasting |
US2736263A (en) * | 1956-02-28 | Blasting explosive device | ||
US2770193A (en) * | 1952-02-01 | 1956-11-13 | Stanolind Oil & Gas Co | Seismic wave generation |
US2788461A (en) * | 1952-11-28 | 1957-04-09 | Ici Ltd | Method of firing explosive charges and apparatus therefor |
US2814991A (en) * | 1952-05-21 | 1957-12-03 | Ici Ltd | Art of delay electric shot-firing of blasting explosive charges and appliances suitable for use in delay electric shot-firing circuits |
US2923239A (en) * | 1957-07-26 | 1960-02-02 | Ensign Bickford Co | Ignition transmission line and systems including the same |
US3021786A (en) * | 1958-07-21 | 1962-02-20 | Du Pont | Blasting device |
DE1153307B (en) * | 1961-09-22 | 1963-08-22 | Dynamit Nobel Ag | Detonating cord connector |
US4185554A (en) * | 1960-07-28 | 1980-01-29 | The United States Of America As Represented By The Secretary Of The Navy | Sweeping acoustic mines |
US4350097A (en) * | 1980-05-19 | 1982-09-21 | Atlas Powder Company | Nonelectric delay detonator with tubular connecting arrangement |
US4632034A (en) * | 1984-03-08 | 1986-12-30 | Halliburton Company | Redundant detonation initiators for use in wells and method of use |
EP0296053A1 (en) * | 1987-06-16 | 1988-12-21 | AEROSPATIALE Société Nationale Industrielle | Pyrotechnic network |
US4821645A (en) * | 1987-07-13 | 1989-04-18 | Atlas Powder Company | Multi-directional signal transmission in a blast initiation system |
US4938143A (en) * | 1987-04-29 | 1990-07-03 | Trojan Corporation | Booster shaped for high-efficiency detonating |
US4953464A (en) * | 1987-07-13 | 1990-09-04 | Atlas Powder Company | Multi-directional signal transmission in a blast initiation system |
FR2733314A1 (en) * | 1995-04-20 | 1996-10-25 | Aerospatiale | Gas generator e.g. thruster for space applications |
US20030200891A1 (en) * | 2002-04-25 | 2003-10-30 | Yu Peter Sung Yan | Fireworks fuse connector |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB189815647A (en) * | 1898-07-16 | 1898-08-20 | Heinrich Bettermann | Improvements in Electrically Ignited Fuses for Blasting Purposes. |
US663724A (en) * | 1899-03-24 | 1900-12-11 | Caleb F Bryant | Blasting. |
US1999820A (en) * | 1931-06-24 | 1935-04-30 | Hercules Powder Co Ltd | Delay cap |
US2139581A (en) * | 1936-10-27 | 1938-12-06 | Hercules Powder Co Ltd | Delay electric blasting cap |
-
1947
- 1947-11-04 US US783976A patent/US2475875A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB189815647A (en) * | 1898-07-16 | 1898-08-20 | Heinrich Bettermann | Improvements in Electrically Ignited Fuses for Blasting Purposes. |
US663724A (en) * | 1899-03-24 | 1900-12-11 | Caleb F Bryant | Blasting. |
US1999820A (en) * | 1931-06-24 | 1935-04-30 | Hercules Powder Co Ltd | Delay cap |
US2139581A (en) * | 1936-10-27 | 1938-12-06 | Hercules Powder Co Ltd | Delay electric blasting cap |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2736263A (en) * | 1956-02-28 | Blasting explosive device | ||
US2609750A (en) * | 1946-05-16 | 1952-09-09 | Atlas Powder Co | Process of blasting |
US2546686A (en) * | 1947-03-21 | 1951-03-27 | Du Pont | Blasting device |
US2770193A (en) * | 1952-02-01 | 1956-11-13 | Stanolind Oil & Gas Co | Seismic wave generation |
US2814991A (en) * | 1952-05-21 | 1957-12-03 | Ici Ltd | Art of delay electric shot-firing of blasting explosive charges and appliances suitable for use in delay electric shot-firing circuits |
US2788461A (en) * | 1952-11-28 | 1957-04-09 | Ici Ltd | Method of firing explosive charges and apparatus therefor |
US2923239A (en) * | 1957-07-26 | 1960-02-02 | Ensign Bickford Co | Ignition transmission line and systems including the same |
US3021786A (en) * | 1958-07-21 | 1962-02-20 | Du Pont | Blasting device |
US4185554A (en) * | 1960-07-28 | 1980-01-29 | The United States Of America As Represented By The Secretary Of The Navy | Sweeping acoustic mines |
DE1153307B (en) * | 1961-09-22 | 1963-08-22 | Dynamit Nobel Ag | Detonating cord connector |
US4350097A (en) * | 1980-05-19 | 1982-09-21 | Atlas Powder Company | Nonelectric delay detonator with tubular connecting arrangement |
US4632034A (en) * | 1984-03-08 | 1986-12-30 | Halliburton Company | Redundant detonation initiators for use in wells and method of use |
US4938143A (en) * | 1987-04-29 | 1990-07-03 | Trojan Corporation | Booster shaped for high-efficiency detonating |
EP0296053A1 (en) * | 1987-06-16 | 1988-12-21 | AEROSPATIALE Société Nationale Industrielle | Pyrotechnic network |
FR2616900A1 (en) * | 1987-06-16 | 1988-12-23 | Aerospatiale | PYROTECHNIC NETWORK |
US4821645A (en) * | 1987-07-13 | 1989-04-18 | Atlas Powder Company | Multi-directional signal transmission in a blast initiation system |
US4953464A (en) * | 1987-07-13 | 1990-09-04 | Atlas Powder Company | Multi-directional signal transmission in a blast initiation system |
FR2733314A1 (en) * | 1995-04-20 | 1996-10-25 | Aerospatiale | Gas generator e.g. thruster for space applications |
US5827993A (en) * | 1995-04-20 | 1998-10-27 | Societe Nationale Industrielle Et Aerospatiale | Pyrotechnic ignition device for a gas generator |
US20030200891A1 (en) * | 2002-04-25 | 2003-10-30 | Yu Peter Sung Yan | Fireworks fuse connector |
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