US3780753A - In-line explosion arrester - Google Patents

In-line explosion arrester Download PDF

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US3780753A
US3780753A US3780753DA US3780753A US 3780753 A US3780753 A US 3780753A US 3780753D A US3780753D A US 3780753DA US 3780753 A US3780753 A US 3780753A
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pipeline
flange
bore
ribbon
pair
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L Jablansky
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US Department of Navy
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US Department of Navy
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00Flanged joints
    • F16L23/02Flanged joints the flanges being connected by members tensioned axially
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K17/00Safety valves; Equalising valves, e.g. pressure relief valves
    • F16K17/36Safety valves; Equalising valves, e.g. pressure relief valves actuated in consequence of extraneous circumstances, e.g. shock, change of position
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17DPIPE-LINE SYSTEMS; PIPE-LINES
    • F17D1/00Pipe-line systems
    • F17D1/08Pipe-line systems for liquids or viscous products
    • F17D1/086Pipe-line systems for liquids or viscous products for explosives
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17DPIPE-LINE SYSTEMS; PIPE-LINES
    • F17D3/00Arrangements for supervising or controlling working operations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42DBLASTING
    • F42D5/00Safety arrangements
    • F42D5/04Rendering explosive charges harmless, e.g. destroying ammunition; Rendering detonation of explosive charges harmless
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/1624Destructible or deformable element controlled
    • Y10T137/1632Destructible element
    • Y10T137/1647Explosive actuation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/1624Destructible or deformable element controlled
    • Y10T137/1632Destructible element
    • Y10T137/1669Tensile or sheer pin or bolt

Definitions

  • This invention relates to a system for arresting detonations in a continuous process explosive pipe-line such as those used in the manufacture of molten TNT and similar explosive materials.
  • Prior art devices using explosive arresters were not capable of stopping a detonation from propagation in a conduit containing molten explosive such as tri-nitrotoluene.
  • Devices used in the past have attempted'to arrest the propagation of an initial explosion in a line carrying the explosive by controlling and limiting the diameter of the pipe and/or by the insertion of loops in the production line. Both of these methods have been found to be of limited merit.
  • the present invention is a system for interrupting the propagation of a detonation wave in a conduit carrying explosive material such as molten tri-nitro-toluene by attenuating the aforesaid wave to a minimum energy level, either upstream and/or downstream from the explosion point, thereby rendering the initial explosion ineffective in initiating and propagating further explosions along the line.
  • explosive material such as molten tri-nitro-toluene
  • One of the objects of this invention is to provide quenching action in an explosive train in approximately one millisecond.
  • Another object of this invention is to provide an arresting device for quenching pipeline explosions which is suitable for more than one type of explosive.
  • Another object of this invention is to provide a system for interrupting the propagation of a detonation wave in a conduit containing a molten explosive which system does not restrict the normal material flow through the conduit.
  • Another object of this invention is to provide a means for interrupting the detonation wave in an explosive carrying pipeline without substantially limiting the physical size or shape of the line.
  • Another object of this invention is to provide a simple, cheap and compact means for effectively quenching an accidental explosion in an explosive carrying pipeline.
  • FIG. 1 is a schematic and block diagram of an in-line explosion arrester, which closes a passageway when activated by an electronic sensing circuit and switch.
  • FIG. 2 is a modification of the schematic and block diagram shown in FIG. l,'showing a means for arresting a detonation by opening a passageway when the arresting means is activated by an electronic sensing circuit and switch.
  • FIG. 3 is an electrical schematic of the electronic switch circuit l6 shown in FIGS. 1 and 2.
  • FIG. 4 is a cross-sectional view-ofthe in-line explosion arrester schematically illustrated in FIG. 1.
  • FIG. 5 is a sectional view of an in-line explosion arrester illustrated in FIG. 4, and taken along line 5-5.
  • FIG. 6 is a sectional view of aforementioned in-line explosion arrester illustrated in FIG. 4, and taken along line 66.
  • FIG. 7 is .a cross-sectional expanded, elevational, view of one of the two detonation arresting means schematically illustrated in FIG. 2.
  • FIG. 8 is a partial sectional and plan view of the detonation arresting means of FIG. 7 taken along line 8-8.
  • FIG. 9 is a cross section of the detonation arresting means taken along line 9--9 of FIG. 7.
  • a detonation sensor breakwire 10 is coiled about the longitudinal circumference of the liquid explosive pipe-line 12 having a product flow 14.
  • the detonation breakwire sensor 10 is electrically connected to a pair of input terminals 18 and 20 of an electronic switch circuit 16.
  • Circuit 16 maintains an in-line explosion arresting means 26 in FIG. 1 and two arresting means 28, 28 in FIG. 2 nonoperative so long as the breakwire sensor is intact.
  • the electronic switch circuit 16 When an explosion causes the breakwire 10 to rupture anywhere along pipe-line 12 or 12, the electronic switch circuit 16 will energize the detonation arresting means 26 and 28 through detonator leads 23 and 25 and to arresting means 28' through a parallel connection at junctions 27 and 29.
  • the in-Iine explosion arresting means 26 prevents the propagation of the explosive train by blocking the line. A barrier attenuates the detonation wave to a minimum energy level rendering the wave incapable of further explosive propagation.
  • the explosion arresting means 28 and 28' cause the explosive sectional pipe-line 12' to separate from line 12 thereby opening up the explosive pipe-line 12 causing a critical discontinuity in the explosive fluid and thereby preventing propagation of the explosion.
  • the arresting means will interrupt the propagation of the detonating wave in approximately 1 millisecond after rupture of the breakwire sensor.
  • FIG. 3 is an electrical schematic of the electronic switch 16 illustrated in FIGS. 1 and 2.
  • a power source 17 is connected through a switch 19 and charging resistor 30 across the series combination silicon controlled rectifier 34 and electric detonator 52, also shown on FIGS. 4 and 7.
  • Electric detonator leads 23 and 25 are connected to the switch 16 output terminals 22 and 24.
  • a capacitor 35 is connected in parallel with the series combination of the silicon controlled rectifier and electric detonator 52 at junctions 42 and 21.
  • a voltage dividing resistor 32 is connected at one end to the common junction 42 between the limiting resistor 30, an anode lead 36 and capacitor 35, and the other end to the common junction 46 between the trigger electrode 40 and the electrical connection 47. The other end of the electrical connection 47 is connected to terminal 18.
  • Junction 21 is also connected to terminal 20.
  • the low resistance path of the breakwire sensor 10 when connected to terminals 18 and 20 keeps the trigger electrode 40 of silicon controlled rectifier 34 at a low potential and therefore in a cut-off non-conducting condition.
  • the breakwire sensor 10 is broken the potential at junction 46 is raised to a voltage approaching anode potential causing the siliconcontrolled rectifier 34 to conduct thereby discharging the energy stored in capacitor 35 to the electric detonator 52, and initiating the detonation arresting means 26, 28 and 28'.
  • FIG. 4 shows the details of an in-line explosion arrester 26 illustrated in FIG. 1.
  • a threaded detonator holder and closure 48 has an axial bore 51 which is filled with an insulating cement 50 which holds detonator leads 23 and 25.
  • a smaller axial bore 53 permits the passage of leads 23 and 25 to a larger axial bore 55 which contains an electrical detonator 52.
  • the detonator holder 48 is coaxially threaded into a bushing 54 which is in turn threaded into one end of the detonation trap housing 60.
  • a space 56 is provided between the threaded portion 49 of the detonator holder 48 and an inner bore 57 of the threaded bushing 54.
  • a hollow steel cylindrical plug 68 is operatively positioned below the threaded bushing 54 and slidably engages the inner wall of the longitudinal bore 61 of housing 60 at one end of its outer peripheral surface.
  • Steel plug 68 at said first end has a first annular O ring groove 65 which contains a first ring 64 and a transverse bore on one side of said first end for holding a shear pin 62.
  • the shear pin 62 fits in a shear pin housing groove 63 permitting the bottom surface 67 of the threaded bushing 54 to mate with the bottom surface of the threaded housing bore 69.
  • Steel plug 68 has a first threaded bore 59 on an open end and a second smaller axially aligned bore 81 on a closed end.
  • a steel threaded insert 70 is threaded onto the first threaded steel plug bore 59 closing the second plug bore 81 and retaining therein a low density polyurethane foam 72.
  • the steel threaded insert 70 has a central axially aligned bore 79 and inserted therein is a compressible wafer 58 oppositely disposed and in line with the electric detonator 52. The purpose of the compressible wafer 58 is to absorb some of the shock caused by detonator 52.
  • the purpose of the polyurethane foam 72 is to further attenuate the detonation wave and to prevent spalling of wall of plug bore 81.
  • the TEFLON sleeve transverse port member 66 retains the other smaller closed end of steel plug 68 in a cup shaped recess 66' therein and lines up the transverse bore 71 transverse bores 60' with housing 60.
  • a second annular O ring groove 65' is located in the bottom peripheral surface of the TEF LON sleeve 66 transverse to the longitudinal axis 86 and adjacent to the transverse bore 71; a second 0 ring 64' is located in the aforesaid second 0 ring groove 65.
  • O ring 64' acts as a seal to prevent the molten explosive product from entering into the space between housing 60 and TEFLON sleeeve 66.
  • a third annular O ring groove 65" is located transverse to the longitudinal axis 86 and adjacent to transverse bore 71 and has therewithin a third 0 ring 64" which acts as a seal to retain the molten explosive material within the transverse bore 71 and the housing-60.
  • An aluminum decelerating stop 76 which is circular in cross section when viewed along line 6-6 is attached to the underneath side of the transverse bore wall 71' by screws 84 and is slightly smaller in diameter than the inside diameter of the longitudinal central bore wall 61 of housing 60.
  • Pipe flanges 74 and 74 are circumferentially welded at 73, 73' to housing 60 so that the flange bore 75, 75' are axially aligned with the transverse bore 60.
  • Fourth annular O ring grooves 65" and fourth 0 rings 64" are located in the flange mating faces 77, 77' to form a seal with mating flanges (not shown) which are hermetically attached to pipe line 12 so that the explosive molten material may be maintained therein.
  • Housing 60 has a threaded boss 83 on its other end and to which a threaded tapered stop 82 is screwed thereon.
  • tapered bore 80 located adjacent to clearance space 78, gradually slows decelerating stop 76 which has been given motion by electrical detonator 52, effectinga closure of transverse bores 60 with a minimum of shock impact thereby safely attenuating the approaching detonating wave along pipe-line 12.
  • An initiating pulse from the electronic switch 16 through leads 23 and 25 will activate electric detonator 52 causing gases to be generated above wafer 58; the pressure of these gases creates a force against steel plug 68 causing shear pin 62 to shear and the TEFLON sleeve 66 to move in a direction in line with longitudinal axis 86 closing the transverse bores 60 and thereby attenuating any subsequent detonation wave from being propagated along explosive line 12.
  • FIG. 5 a cross-sectional view taken along line 5-5 of FIG. 4, we see the concentric arrangement of polyurethane foam 72, the retaining walls of steel plug 68 surrounding the foam 72, and the TEFLON sleeve wall 66 intermediate to the steel plug 68 and the surrounding housing 60.
  • F IG. 6 shows a cross-sectional view of the housing 60 and the decelerating stop 76 when the detonation arresting means 26 is in its open state.
  • Housing 60 is circumambient the decelerating stop 76 and separated therefrom by clearance space 85.
  • a plurality of screws 84, 84' holds the decelerating stop 76 affixed to the transverse bore wall 71' (not shown).
  • FIG. 7 shows, in partial cross-section, one of two identical detonation arresting means 28 and 28 which upon receipt of an intiating signal from electronic switch 16 will cause sectional pipeline 12' in FIG. 2 to separate from pipe line 12.
  • Upper flange 90 has an axial first central bore 104 on its outer surface 91 and concentric therewith a second central bore 106; pipeline 12 is positioned in the upper flange first bore 104 and welded to the outer surface 91 at weld 99.
  • lower flange 92 has an outer surface 93 welded to sectional pipeline 12 at weld 99'.
  • Sectional pipe-line 12' is axially aligned with pipeline 12 by the lower flange first central bore 112 and a concentric second central bore of smaller diameter 108.
  • the upper flange 90 is connected to the lower flange 92 by a plurality of bolts 102, 102, 102" and 102" (see H65. 8 and 9) which pass through upper flange clearance holes 105,
  • a circular upper fuze ribbon channel 95 is positioned immediately adjacent to electric detonator hole 109 which holds the electric detonator 52.
  • a matching circular lower fuze ribbon channel 97 is positioned opposite to the upper fuze ribbon channel 95 so that when both flanges are assembled together a closed annular channel is formed for containing the detonating fuze ribbon 94 therein.
  • An annular O ring channel 101 of smaller diameter than the upper flange tongue 98 is intermediate to a central bore 104 and the upper flange tongue 98 and located in the same flange face as the upper fuze ribbon channel 95.
  • An ring 100 is positioned within the O ring channel 101 and space formed between channel 101 and lower flange inner surface 111.
  • the O ring 100 in contact with the inner surface 111 of the lower flange 92 acts as an effective seal preventing the molten explosive in pipe line 12 and sectional pipe line 12' from escaping or from contacting detonating fuze ribbon 94 or the electrical detonator 52.
  • a threaded hole 110 is opposite to and connected with electric detonator hole 109 thereby permitting detonator holder 48 and electric detonator 52 to be operatively positioned immediately adjacent to the detonating fuze ribbon 94.
  • FIG. 8 shows a plan and partial cross-section taken along line 88 of FIG. 7 of the upper flange outer surface 91 with a plurality of screws 102. 102, 102", 102" positioned between pipeline l2 and the outside diameter of the upper flange 90.
  • FIG. 9 shows a view of the upper flange inner surface taken along line 99, a cross-section of detonating fuze ribbon 94, electric detonator 52, detonator holder 48, and a plurality of screws 102, 102', 102" and 102" in clearance holes 105, 105, 105" and 105" respectively.
  • This view shows the concentric positions of the O ring 100, O ring groove 101 and the detonating fuze ribbon 94 about the second central bore 106.
  • Detonator holder closure 48 and electric detonator hole 109 are axially in line and radially positioned with respect to detonating ribbon 94 so that the electric detonator 52, located in electric detonator hole 109, is adjacent to detonating ribbon 94.
  • An initiating pulse from the electronic switch 16 through leads 23 and 25 and 23' and 25' in parallel connection at junctions 27 and 29, as shown in FIG. 2, will cause the electric detonator 52, as shown in FIG. 9, in detonation arresting means 28 and 28' respectively to fire the detonating fuze ribbon 94.
  • the mild explosive force of detonating ribbons 94 and 94' (not shown) in arresting means 28' will cause the lower flange halves 92 and 92' (not shown) of detonating arresting means 28 and 28 to simultaneously separate from the upper flange 90 and 90 (not shown) causing line 12' to be opened, thereby preventing the propagation of the detonation wave along pipe-line 12.
  • the invention provides a system for rapidly detecting an explosion in an explosive material carrying pipe-line and arresting the detonation wave thereby preventing further propagation of the explosion.
  • a system for detecting an initial explosion in a pipeline carrying explosive materials and arresting said explosion prior to the propagation of a detonation wave along said pipeline which comprises:
  • a breakwire sensor operatively positioned around said pipeline
  • an electronic switch having a pair of inputterminals electrically connected to said breakwire for maintaining said electronic switch non-operative when said breakwire is intact, an a pair of output terminals for supplying a voltage pulse when said breakwire is broken, and which includes;
  • a silicon controlled rectifier having an anode terminal connected to a positive terminal of said power source through a series connected charging resistor and switch, a trigger electrode connected to the common junction of a first terminal of said pair of input terminals and to one end of a voltage dividing resistor, said voltage dividing resistor having its other end connected to the common junction of said charging resistor and said anode terminal, a cathode terminal connected to a first terminal of said pair of output terminals;
  • a load capacitor having one terminal connected to the common junction of a second terminal of said pair of input terminals and a second terminal of said output pair of terminals and the negative side of said power source, and a second terminal connected to the common junction of said anode terminal, said voltage dividing resistor, and said charging resistor,whereby said capacitor discharges its stored energy to said pair of output terminals when said breakwire sensor is broken, causing said silicon rectifier trigger electrode to be more positively biased, triggeringsaid silicon rectifier;
  • means for arresting a detonation disposed proximate said pipeline electrically coupled to said pair of output terminals and responsive to said voltage pulse which includes;
  • an upper flange having a central counter-bore located on an outer surface of said flange to which said pipeline is welded, a second smaller central bore coaxial with said counter-bore and said pipeline connecting to an inner surface of said upper flange, an annular O-ring groove in said inner surface of larger diameter than said counter-bore and concentric thereto, an annular upper flange tongue larger in diameter than said O-ring groove, concentric therewith and protruding from said inner surface, an upper fuze ribbon channel in said inner surface of larger diameter than said annular upper flange tongue and intermediate to said upper flange outside diameter; a lower flange having a central bore equal in diameter to said upper flange central bore and oppositely disposed on the inner surface of said lower flange, a central counter-bore on an outer surface of said lower flange concentric with said lower flange central bore and oppositely disposed to said upper flange counter-bore and to which one end of said pipeline is welded, a lower flange annular tongue groove

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  • General Engineering & Computer Science (AREA)
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Abstract

This invention relates to a system for detecting an explosion in a pipeline carrying molten explosive material and halting the spread thereof by blocking the propagation of the detonating wave by a detonation arresting means that is electrically activated by an electronic switch which is sensitive to the initial detonation.

Description

United States Patent 1 Jablansky [4 Dec. 25, 1973 IN-LINE EXPLOSION ARRESTER [75] Inventor: Louis Jablansky, Fair Lawn, NJ.
[73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.
[22] Filed: Dec. 12, 1972 [21] Appl. No.: 314,299
Related US. Application Data [62] Division of Ser. No. 139,337, May 3, 1971, Pat. No.
[52'] US. Cl. 137/68, 285/3 [51] Int. Cl.. Fl6k 13/00 [58] Field of Search ..137/6771; 317/D1G. 8;
285/3, 4, l8, DIG. 21; 85/D1G. l
[56] References Cited UNITED STATES PATENTS 1,284,197 11/1918 Lamer et al. 137/68 2,399,843 5/1946 Adams 137/67 X 3,032,356 5/1962 Bot sford 3,509,942 5/1970 Lindberg 137/67 X Primary ExaminerHenry T. Klinksiek Assistant ExaminerRichard Gerard Attorney-Edward J. Kelly [5 7 ABSTRACT 1 Claim, 9 Drawing Figures I as 97 m3 /07 RATENTED DEC 2 5 i873 SHEET 3 BF 7 WENIED DEC 2 5 I975 SHEET 3 [If 7 "ATENTED DEC 2 5 I975 sum 5 [1F 7 PATENTED DEC 2 5 I975 SHEET E OF 7 PATENTED DEC 2 5 I975 SHEET 7 UF 7 IN-LINE EXPLOSION ARRESTER This is a division, of application Ser. No. 139,337, filed 3 May 1971 now US. Pat. No. 3,739,796.
BACKGROUND OF THE INVENTION The invention described herein may be manufactured, used and licensed by or for the Government for governmental purposes without the payment to me of any royalty thereon.
BACKGROUND OF THE INVENTION This invention relates to a system for arresting detonations in a continuous process explosive pipe-line such as those used in the manufacture of molten TNT and similar explosive materials.
Prior art devices using explosive arresters were not capable of stopping a detonation from propagation in a conduit containing molten explosive such as tri-nitrotoluene. Devices used in the past, have attempted'to arrest the propagation of an initial explosion in a line carrying the explosive by controlling and limiting the diameter of the pipe and/or by the insertion of loops in the production line. Both of these methods have been found to be of limited merit. In manufacturing operations, where molten explosive is being transported from one processing operation to another, limiting the conduit to a critical diameter which will inhibit the propagation will not permit adequate volume of material to flow; likewise where loops of sufficient number are introduced into the line to substantially inhibit propagation of a detonation their resultant effect in restricting the volume of flow through the conduit has proved objectionable.
SUMMARY OF THE INVENTION The present invention is a system for interrupting the propagation of a detonation wave in a conduit carrying explosive material such as molten tri-nitro-toluene by attenuating the aforesaid wave to a minimum energy level, either upstream and/or downstream from the explosion point, thereby rendering the initial explosion ineffective in initiating and propagating further explosions along the line.
One of the objects of this invention is to provide quenching action in an explosive train in approximately one millisecond.
Another object of this invention is to provide an arresting device for quenching pipeline explosions which is suitable for more than one type of explosive.
Another object of this invention is to provide a system for interrupting the propagation of a detonation wave in a conduit containing a molten explosive which system does not restrict the normal material flow through the conduit.
Another object of this invention is to provide a means for interrupting the detonation wave in an explosive carrying pipeline without substantially limiting the physical size or shape of the line.
Another object of this invention is to provide a simple, cheap and compact means for effectively quenching an accidental explosion in an explosive carrying pipeline.
For a better understanding of the present invention, together with other and further objects thereof, reference is made to the following description taken in connection with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic and block diagram of an in-line explosion arrester, which closes a passageway when activated by an electronic sensing circuit and switch.
FIG. 2 is a modification of the schematic and block diagram shown in FIG. l,'showing a means for arresting a detonation by opening a passageway when the arresting means is activated by an electronic sensing circuit and switch.
FIG. 3 is an electrical schematic of the electronic switch circuit l6 shown in FIGS. 1 and 2.
FIG. 4 is a cross-sectional view-ofthe in-line explosion arrester schematically illustrated in FIG. 1.
FIG. 5 is a sectional view of an in-line explosion arrester illustrated in FIG. 4, and taken along line 5-5.
FIG. 6 is a sectional view of aforementioned in-line explosion arrester illustrated in FIG. 4, and taken along line 66.
FIG. 7 is .a cross-sectional expanded, elevational, view of one of the two detonation arresting means schematically illustrated in FIG. 2.
FIG. 8 is a partial sectional and plan view of the detonation arresting means of FIG. 7 taken along line 8-8.
FIG. 9 is a cross section of the detonation arresting means taken along line 9--9 of FIG. 7.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring now to FIGS. 1 and 2, a detonation sensor breakwire 10 is coiled about the longitudinal circumference of the liquid explosive pipe-line 12 having a product flow 14. The detonation breakwire sensor 10 is electrically connected to a pair of input terminals 18 and 20 of an electronic switch circuit 16. Circuit 16 maintains an in-line explosion arresting means 26 in FIG. 1 and two arresting means 28, 28 in FIG. 2 nonoperative so long as the breakwire sensor is intact. When an explosion causes the breakwire 10 to rupture anywhere along pipe- line 12 or 12, the electronic switch circuit 16 will energize the detonation arresting means 26 and 28 through detonator leads 23 and 25 and to arresting means 28' through a parallel connection at junctions 27 and 29. In the arrangement shown in FIG. 1 the in-Iine explosion arresting means 26 prevents the propagation of the explosive train by blocking the line. A barrier attenuates the detonation wave to a minimum energy level rendering the wave incapable of further explosive propagation. In FIG. 2 the explosion arresting means 28 and 28' cause the explosive sectional pipe-line 12' to separate from line 12 thereby opening up the explosive pipe-line 12 causing a critical discontinuity in the explosive fluid and thereby preventing propagation of the explosion. In both arrangements described above the arresting means will interrupt the propagation of the detonating wave in approximately 1 millisecond after rupture of the breakwire sensor.
FIG. 3 is an electrical schematic of the electronic switch 16 illustrated in FIGS. 1 and 2. A power source 17 is connected through a switch 19 and charging resistor 30 across the series combination silicon controlled rectifier 34 and electric detonator 52, also shown on FIGS. 4 and 7. Electric detonator leads 23 and 25 are connected to the switch 16 output terminals 22 and 24. A capacitor 35 is connected in parallel with the series combination of the silicon controlled rectifier and electric detonator 52 at junctions 42 and 21. A voltage dividing resistor 32 is connected at one end to the common junction 42 between the limiting resistor 30, an anode lead 36 and capacitor 35, and the other end to the common junction 46 between the trigger electrode 40 and the electrical connection 47. The other end of the electrical connection 47 is connected to terminal 18. Junction 21 is also connected to terminal 20. The low resistance path of the breakwire sensor 10 when connected to terminals 18 and 20 keeps the trigger electrode 40 of silicon controlled rectifier 34 at a low potential and therefore in a cut-off non-conducting condition. When the breakwire sensor 10 is broken the potential at junction 46 is raised to a voltage approaching anode potential causing the siliconcontrolled rectifier 34 to conduct thereby discharging the energy stored in capacitor 35 to the electric detonator 52, and initiating the detonation arresting means 26, 28 and 28'.
FIG. 4 shows the details of an in-line explosion arrester 26 illustrated in FIG. 1. A threaded detonator holder and closure 48 has an axial bore 51 which is filled with an insulating cement 50 which holds detonator leads 23 and 25. A smaller axial bore 53 permits the passage of leads 23 and 25 to a larger axial bore 55 which contains an electrical detonator 52. The detonator holder 48 is coaxially threaded into a bushing 54 which is in turn threaded into one end of the detonation trap housing 60. A space 56 is provided between the threaded portion 49 of the detonator holder 48 and an inner bore 57 of the threaded bushing 54. This inner space 56 permits gases generated by the detonator 52 to expand, thereby minimizing any shock wave generated by detonator 52. A hollow steel cylindrical plug 68 is operatively positioned below the threaded bushing 54 and slidably engages the inner wall of the longitudinal bore 61 of housing 60 at one end of its outer peripheral surface. Steel plug 68 at said first end has a first annular O ring groove 65 which contains a first ring 64 and a transverse bore on one side of said first end for holding a shear pin 62. The shear pin 62 fits in a shear pin housing groove 63 permitting the bottom surface 67 of the threaded bushing 54 to mate with the bottom surface of the threaded housing bore 69. Steel plug 68 has a first threaded bore 59 on an open end and a second smaller axially aligned bore 81 on a closed end. A steel threaded insert 70 is threaded onto the first threaded steel plug bore 59 closing the second plug bore 81 and retaining therein a low density polyurethane foam 72. The steel threaded insert 70 has a central axially aligned bore 79 and inserted therein is a compressible wafer 58 oppositely disposed and in line with the electric detonator 52. The purpose of the compressible wafer 58 is to absorb some of the shock caused by detonator 52. The purpose of the polyurethane foam 72 is to further attenuate the detonation wave and to prevent spalling of wall of plug bore 81. The TEFLON sleeve transverse port member 66 retains the other smaller closed end of steel plug 68 in a cup shaped recess 66' therein and lines up the transverse bore 71 transverse bores 60' with housing 60. A second annular O ring groove 65' is located in the bottom peripheral surface of the TEF LON sleeve 66 transverse to the longitudinal axis 86 and adjacent to the transverse bore 71; a second 0 ring 64' is located in the aforesaid second 0 ring groove 65. O ring 64' acts as a seal to prevent the molten explosive product from entering into the space between housing 60 and TEFLON sleeeve 66. A third annular O ring groove 65" is located transverse to the longitudinal axis 86 and adjacent to transverse bore 71 and has therewithin a third 0 ring 64" which acts as a seal to retain the molten explosive material within the transverse bore 71 and the housing-60. An aluminum decelerating stop 76 which is circular in cross section when viewed along line 6-6 is attached to the underneath side of the transverse bore wall 71' by screws 84 and is slightly smaller in diameter than the inside diameter of the longitudinal central bore wall 61 of housing 60. Pipe flanges 74 and 74 are circumferentially welded at 73, 73' to housing 60 so that the flange bore 75, 75' are axially aligned with the transverse bore 60. Fourth annular O ring grooves 65" and fourth 0 rings 64" are located in the flange mating faces 77, 77' to form a seal with mating flanges (not shown) which are hermetically attached to pipe line 12 so that the explosive molten material may be maintained therein. Housing 60 has a threaded boss 83 on its other end and to which a threaded tapered stop 82 is screwed thereon. The wall of tapered bore 80, located adjacent to clearance space 78, gradually slows decelerating stop 76 which has been given motion by electrical detonator 52, effectinga closure of transverse bores 60 with a minimum of shock impact thereby safely attenuating the approaching detonating wave along pipe-line 12.
An initiating pulse from the electronic switch 16 through leads 23 and 25 will activate electric detonator 52 causing gases to be generated above wafer 58; the pressure of these gases creates a force against steel plug 68 causing shear pin 62 to shear and the TEFLON sleeve 66 to move in a direction in line with longitudinal axis 86 closing the transverse bores 60 and thereby attenuating any subsequent detonation wave from being propagated along explosive line 12.
In FIG. 5, a cross-sectional view taken along line 5-5 of FIG. 4, we see the concentric arrangement of polyurethane foam 72, the retaining walls of steel plug 68 surrounding the foam 72, and the TEFLON sleeve wall 66 intermediate to the steel plug 68 and the surrounding housing 60.
F IG. 6 shows a cross-sectional view of the housing 60 and the decelerating stop 76 when the detonation arresting means 26 is in its open state. Housing 60 is circumambient the decelerating stop 76 and separated therefrom by clearance space 85. A plurality of screws 84, 84' holds the decelerating stop 76 affixed to the transverse bore wall 71' (not shown).
FIG. 7 shows, in partial cross-section, one of two identical detonation arresting means 28 and 28 which upon receipt of an intiating signal from electronic switch 16 will cause sectional pipeline 12' in FIG. 2 to separate from pipe line 12. Upper flange 90 has an axial first central bore 104 on its outer surface 91 and concentric therewith a second central bore 106; pipeline 12 is positioned in the upper flange first bore 104 and welded to the outer surface 91 at weld 99. In a similar manner lower flange 92 has an outer surface 93 welded to sectional pipeline 12 at weld 99'. Sectional pipe-line 12' is axially aligned with pipeline 12 by the lower flange first central bore 112 and a concentric second central bore of smaller diameter 108. The upper flange 90 is connected to the lower flange 92 by a plurality of bolts 102, 102, 102" and 102" (see H65. 8 and 9) which pass through upper flange clearance holes 105,
105, 105" and 105" into aligned holes 103, 103, 103" and 103". A circular upper fuze ribbon channel 95 is positioned immediately adjacent to electric detonator hole 109 which holds the electric detonator 52. A matching circular lower fuze ribbon channel 97 is positioned opposite to the upper fuze ribbon channel 95 so that when both flanges are assembled together a closed annular channel is formed for containing the detonating fuze ribbon 94 therein. A circularly shaped upper flange tongue 98, of smaller diameter than the fuze ribbon channels 95 and 97, mates with an annular channel 96 located in the lower flange 92. An annular O ring channel 101 of smaller diameter than the upper flange tongue 98 is intermediate to a central bore 104 and the upper flange tongue 98 and located in the same flange face as the upper fuze ribbon channel 95. An ring 100 is positioned within the O ring channel 101 and space formed between channel 101 and lower flange inner surface 111. The O ring 100 in contact with the inner surface 111 of the lower flange 92 acts as an effective seal preventing the molten explosive in pipe line 12 and sectional pipe line 12' from escaping or from contacting detonating fuze ribbon 94 or the electrical detonator 52. A threaded hole 110 is opposite to and connected with electric detonator hole 109 thereby permitting detonator holder 48 and electric detonator 52 to be operatively positioned immediately adjacent to the detonating fuze ribbon 94.
FIG. 8 shows a plan and partial cross-section taken along line 88 of FIG. 7 of the upper flange outer surface 91 with a plurality of screws 102. 102, 102", 102" positioned between pipeline l2 and the outside diameter of the upper flange 90.
FIG. 9 shows a view of the upper flange inner surface taken along line 99, a cross-section of detonating fuze ribbon 94, electric detonator 52, detonator holder 48, and a plurality of screws 102, 102', 102" and 102" in clearance holes 105, 105, 105" and 105" respectively. This view shows the concentric positions of the O ring 100, O ring groove 101 and the detonating fuze ribbon 94 about the second central bore 106. Detonator holder closure 48 and electric detonator hole 109 are axially in line and radially positioned with respect to detonating ribbon 94 so that the electric detonator 52, located in electric detonator hole 109, is adjacent to detonating ribbon 94.
An initiating pulse from the electronic switch 16 through leads 23 and 25 and 23' and 25' in parallel connection at junctions 27 and 29, as shown in FIG. 2, will cause the electric detonator 52, as shown in FIG. 9, in detonation arresting means 28 and 28' respectively to fire the detonating fuze ribbon 94. The mild explosive force of detonating ribbons 94 and 94' (not shown) in arresting means 28' will cause the lower flange halves 92 and 92' (not shown) of detonating arresting means 28 and 28 to simultaneously separate from the upper flange 90 and 90 (not shown) causing line 12' to be opened, thereby preventing the propagation of the detonation wave along pipe-line 12.
From the above description it will be evident that the invention provides a system for rapidly detecting an explosion in an explosive material carrying pipe-line and arresting the detonation wave thereby preventing further propagation of the explosion.
I wish it to be understood that I do not desire to be limited to the exact detail of construction shown and described for obvious modification will occur to a person skilled in the art.
What is claimed is:
l. A system for detecting an initial explosion in a pipeline carrying explosive materials and arresting said explosion prior to the propagation of a detonation wave along said pipeline which comprises:
a breakwire sensor operatively positioned around said pipeline;
an electronic switch having a pair of inputterminals electrically connected to said breakwire for maintaining said electronic switch non-operative when said breakwire is intact, an a pair of output terminals for supplying a voltage pulse when said breakwire is broken, and which includes;
a power source;
a silicon controlled rectifier having an anode terminal connected to a positive terminal of said power source through a series connected charging resistor and switch, a trigger electrode connected to the common junction of a first terminal of said pair of input terminals and to one end of a voltage dividing resistor, said voltage dividing resistor having its other end connected to the common junction of said charging resistor and said anode terminal, a cathode terminal connected to a first terminal of said pair of output terminals;
a load capacitor having one terminal connected to the common junction of a second terminal of said pair of input terminals and a second terminal of said output pair of terminals and the negative side of said power source, and a second terminal connected to the common junction of said anode terminal, said voltage dividing resistor, and said charging resistor,whereby said capacitor discharges its stored energy to said pair of output terminals when said breakwire sensor is broken, causing said silicon rectifier trigger electrode to be more positively biased, triggeringsaid silicon rectifier; and
means for arresting a detonation disposed proximate said pipeline electrically coupled to said pair of output terminals and responsive to said voltage pulse which includes;
an upper flange having a central counter-bore located on an outer surface of said flange to which said pipeline is welded, a second smaller central bore coaxial with said counter-bore and said pipeline connecting to an inner surface of said upper flange, an annular O-ring groove in said inner surface of larger diameter than said counter-bore and concentric thereto, an annular upper flange tongue larger in diameter than said O-ring groove, concentric therewith and protruding from said inner surface, an upper fuze ribbon channel in said inner surface of larger diameter than said annular upper flange tongue and intermediate to said upper flange outside diameter; a lower flange having a central bore equal in diameter to said upper flange central bore and oppositely disposed on the inner surface of said lower flange, a central counter-bore on an outer surface of said lower flange concentric with said lower flange central bore and oppositely disposed to said upper flange counter-bore and to which one end of said pipeline is welded, a lower flange annular tongue groove on said inside surface of said lower flange oppositely disposed from said annular upper flange tongue and mating therewith when said upper and lower flanges inner surfaces are held together, a lower fuze ribbon annular channel in said lower flange inner surface oppositely disposed from said upper fuze ribbon channel and mating therewith;
means for holding said upper and lower flanges together;
a fuze detonating ribbon angularly contained in said upper and lower fuze ribbon channels;
an O-ring located in said O ring groove contacts said lower flange inner surface and prevents said UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,780,753 Dated December 1973 Louis Jablansky Inventor-(s) It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
On the cover sheet I73] Assignee: "The United States of America as represented by the Secretary of the Navy" should read The United States of America as represented by the Secretary of the Army signed 'andfsealed this 3rd day of September 1974.
(SEAL) Attest:
MCCOY M. GIBSON JR. C. MARSHALL DANN Attesting Officer Commissioner" of Patents -'ORM PO-105O (10-69) v -gg 503764569 v w 0.5. GOVERNMENT nmmuo OFFICE I90 o-asu-asl,

Claims (1)

1. A system for detecting an initial explosion in a pipeline carrying explosive materials and arresting said explosion prior to the propagation of a detonation wave along said pipeline which comprises: a breakwire sensor operatively positioned around said pipeline; an electronic switch having a pair of input terminals electrically connected to said breakwire for maintaining said electronic switch non-operative when said breakwire is intact, an a pair of output terminals for supplying a voltage pulse when said breakwire is broken, and which includes; a power source; a silicon controlled rectifier having an anode terminal connected to a positive terminal of said power source through a series connected charging resistor and switch, a trigger electrode connected to the common junction of a first terminal of said pair of input terminals and to one end of a voltage dividing resistor, said voltage dividing resistor having its other end connected to the common junction of said charging resistor and said anode terminal, a cathode terminal connected to a first terminal of said pair of output terminals; a load capacitor having one terminal connected to the common junction of a second terminal of said pair of input terminals and a second terminal of said output pair of terminals and the negative side of said power source, and a second terminal connected to the common junction of said anode terminal, said voltage dividing resistor, and said charging resistor,whereby said capacitor discharges its stored energy to said pair of output terminals when said breakwire sensor is broken, causing said silicon rectifier trigger electrode to be more positively biased, trIggering said silicon rectifier; and means for arresting a detonation disposed proximate said pipeline electrically coupled to said pair of output terminals and responsive to said voltage pulse which includes; an upper flange having a central counter-bore located on an outer surface of said flange to which said pipeline is welded, a second smaller central bore coaxial with said counter-bore and said pipeline connecting to an inner surface of said upper flange, an annular O-ring groove in said inner surface of larger diameter than said counter-bore and concentric thereto, an annular upper flange tongue larger in diameter than said Oring groove, concentric therewith and protruding from said inner surface, an upper fuze ribbon channel in said inner surface of larger diameter than said annular upper flange tongue and intermediate to said upper flange outside diameter; a lower flange having a central bore equal in diameter to said upper flange central bore and oppositely disposed on the inner surface of said lower flange, a central counter-bore on an outer surface of said lower flange concentric with said lower flange central bore and oppositely disposed to said upper flange counter-bore and to which one end of said pipeline is welded, a lower flange annular tongue groove on said inside surface of said lower flange oppositely disposed from said annular upper flange tongue and mating therewith when said upper and lower flanges inner surfaces are held together, a lower fuze ribbon annular channel in said lower flange inner surface oppositely disposed from said upper fuze ribbon channel and mating therewith; means for holding said upper and lower flanges together; a fuze detonating ribbon angularly contained in said upper and lower fuze ribbon channels; an O-ring located in said O ring groove contacts said lower flange inner surface and prevents said explosive material from escaping between said upper and lower flanges; an electrical detonator; and means for holding said electrical detonator in said upper and lower flanges so that said detonator is immediately adjacent to said fuze detonating ribbon, permitting said ribbon to explode when said electrical detonator receives said voltage pulse from said electronic switch, said ribbon explosion causing separation of said upper and lower flanges and separation of said pipeline sufficient to prevent propagation of the detonating wave along said pipeline.
US3780753D 1971-05-03 1972-12-12 In-line explosion arrester Expired - Lifetime US3780753A (en)

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US13933771A 1971-05-03 1971-05-03
US31429972A 1972-12-12 1972-12-12

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2775771A1 (en) * 1998-03-05 1999-09-10 Nobel Explosifs France Explosion trap for bulk explosives pumping circuit
US20050005966A1 (en) * 2001-09-20 2005-01-13 Klaus Biester Shut-off device
US20190195371A1 (en) * 2017-12-22 2019-06-27 Key Safety Systems, Inc. Line blocker

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US1284197A (en) * 1917-12-10 1918-11-05 Chester W Larner Valve control.
US2399843A (en) * 1942-11-09 1946-05-07 Bendix Aviat Corp Emergency valve
US3032356A (en) * 1960-01-26 1962-05-01 Neilan B Botsford Explosive means to separate casing members
US3509942A (en) * 1966-08-15 1970-05-05 John E Lindberg System for detecting structural failure

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US1284197A (en) * 1917-12-10 1918-11-05 Chester W Larner Valve control.
US2399843A (en) * 1942-11-09 1946-05-07 Bendix Aviat Corp Emergency valve
US3032356A (en) * 1960-01-26 1962-05-01 Neilan B Botsford Explosive means to separate casing members
US3509942A (en) * 1966-08-15 1970-05-05 John E Lindberg System for detecting structural failure

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2775771A1 (en) * 1998-03-05 1999-09-10 Nobel Explosifs France Explosion trap for bulk explosives pumping circuit
BE1013718A3 (en) * 1998-03-05 2002-07-02 Nobel Explosifs France Device for circuit breaker detonation pumping of explosives in bulk.
ES2177356A1 (en) * 1998-03-05 2002-12-01 Nobel Explosifs France Explosion trap for bulk explosives pumping circuit
US20050005966A1 (en) * 2001-09-20 2005-01-13 Klaus Biester Shut-off device
US7231934B2 (en) * 2001-09-20 2007-06-19 Cameron International Corporation Shut-off actuator with gas generation device
US20190195371A1 (en) * 2017-12-22 2019-06-27 Key Safety Systems, Inc. Line blocker
US10794498B2 (en) * 2017-12-22 2020-10-06 Key Safety Systems, Inc. Line blocker

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