WO2003060290A1 - Dispositif de bourrage active - Google Patents

Dispositif de bourrage active Download PDF

Info

Publication number
WO2003060290A1
WO2003060290A1 PCT/ZA2002/000209 ZA0200209W WO03060290A1 WO 2003060290 A1 WO2003060290 A1 WO 2003060290A1 ZA 0200209 W ZA0200209 W ZA 0200209W WO 03060290 A1 WO03060290 A1 WO 03060290A1
Authority
WO
WIPO (PCT)
Prior art keywords
stemming
propellant charge
propellant
initiator
cartridge
Prior art date
Application number
PCT/ZA2002/000209
Other languages
English (en)
Other versions
WO2003060290B1 (fr
Inventor
Andre Van Dyk
Original Assignee
Nxco International Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nxco International Limited filed Critical Nxco International Limited
Priority to US10/500,356 priority Critical patent/US20060169162A1/en
Priority to DE60214041T priority patent/DE60214041D1/de
Priority to CA002472533A priority patent/CA2472533A1/fr
Priority to EP02796156A priority patent/EP1463871B1/fr
Priority to AU2002360867A priority patent/AU2002360867B2/en
Publication of WO2003060290A1 publication Critical patent/WO2003060290A1/fr
Publication of WO2003060290B1 publication Critical patent/WO2003060290B1/fr

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E21—EARTH OR ROCK DRILLING; MINING
    • E21C—MINING OR QUARRYING
    • E21C37/00—Other methods or devices for dislodging with or without loading
    • E21C37/06—Other methods or devices for dislodging with or without loading by making use of hydraulic or pneumatic pressure in a borehole
    • E21C37/14—Other methods or devices for dislodging with or without loading by making use of hydraulic or pneumatic pressure in a borehole by compressed air; by gas blast; by gasifying liquids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42D—BLASTING
    • F42D1/00—Blasting methods or apparatus, e.g. loading or tamping
    • F42D1/08—Tamping methods; Methods for loading boreholes with explosives; Apparatus therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42D—BLASTING
    • F42D1/00—Blasting methods or apparatus, e.g. loading or tamping
    • F42D1/08—Tamping methods; Methods for loading boreholes with explosives; Apparatus therefor
    • F42D1/20—Tamping cartridges, i.e. cartridges containing tamping material

Definitions

  • This invention is concerned generally with the breaking of rock and more particularly is concerned with the provision of stemming in order to confine high pressure forces, in a drill hole, which are generated during a rock breaking process, such as a tailored low energy method of breaking rock.
  • rock includes rock, ore, coal, concrete and any similar hard mass, whether above or underground, which is difficult to break or fracture. It is to be understood that “rock” is to be interpreted broadly.
  • stemming which is placed in a blast hole and which is consolidated by tamping. Nonetheless the stemming is capable of moving to some extent under the action of the forces which are generated when the propellant ignites. The degree to which the stemming confines the forces can have a considerable influence on the effectiveness of the propellant in breaking rock.
  • the invention provides stemming apparatus which includes a member, a propellant charge and an initiator for igniting the propellant charge which then acts on the member in a predetermined direction.
  • the member is driven by the ignited propellant charge in the predetermined direction.
  • the member may be shaped and include a tapered leading end or formation on a side which faces in the predetermined direction.
  • the member is conically shaped on the tapered leading end.
  • An opposing side of the member ie. on a side which is remote from the tapered leading end, may be planar or recessed or shaped in any appropriate way.
  • the member may be constructed so that it is capable of flaring outwardly when moved in a direction which is opposite to the predetermined direction.
  • the member is shaped so that a gas generated force is produced by the ignited propellant in a direction which is opposite to the predetermined direction.
  • the member may include a recessed formation which contains the propellant charge.
  • the recessed formation may be substantially conical.
  • the member may be made from any appropriate material and, for example, may be made from a high density plastics material, a metallic material or the like.
  • Control means may be provided for controlling the firing of the said initiator.
  • the control means may include an energy source and a timer for applying energy from the energy source to the initiator at a predetermined time.
  • the invention also provides a method of stemming which includes the steps of placing stemming material in a hole over a cartridge which includes a first propellant charge, positioning at least one member on the stemming material, locating a second propellant charge on or in the member, and igniting the second propellant charge at a predetermined time relatively to the time at which the first propellant charge is initiated.
  • a short time interval eg. less than 5 milliseconds may exist between the time at which the second propellant charge is ignited and the time at which the first propellant charge is initiated. It is also possible for the first propellant charge to be initiated substantially at the same time as the second propellant charge is ignited.
  • the member may be of any appropriate type and for example may be of a kind which has been described in connection with the aforementioned stemming apparatus.
  • the member is between the stemming material and the second propellant charge.
  • the second propellant charge is between the stemming material and the member.
  • the second propellant charge may be used to drive the member in a direction towards the cartridge.
  • the second propellant charge is used to produce a gas generated force which is directed towards the cartridge.
  • the second propellant charge may be ignited at a predetermined time relatively to the time at which the first propellant charge is initiated.
  • the second propellant charge and the first propellant change may be initiated substantially simultaneously or within a predetermined period of the initiation of the first propellant charge.
  • the method may include the step of precisely controlling this predetermined period.
  • the method may include the step of placing stemming material over the propellant charges in the hole prior to ignition of the propellant charges.
  • a confinement member may be placed over the propellant charges and the additional stemming may be placed over the confinement member.
  • Figure 1 is side view in cross section of stemming apparatus according to one form of the invention being used in a rock breaking process
  • Figure 2 is a view similar to Figure 1 but illustrating a different form of the stemming apparatus according to the invention
  • Figure 3 illustrates a control mechanism for use with the stemming apparatus of Figure 1 or Figure 2
  • Figure 4 is a side view in cross-section illustrating the use of stemming apparatus according to the invention during a rock breaking process
  • Figure 5 is a schematic illustration of a control mechanism used for controlling, on a time basis, a rock breaking process.
  • FIG. 1 of the accompanying drawings illustrates the use of stemming apparatus according to one form of the invention during a rock breaking process.
  • a hole 10 is drilled into a rock mass 12 from a face 14 using conventional drilling equipment, not shown.
  • the hole is drilled to a predetermined length which is at least four times the nominal diameter of the hole.
  • a cartridge 16 is loaded into the hole.
  • the cartridge has a base 18 which opposes a bottom 20 of the hole and a generally cylindrical wall 22 which extends upwards from the base and which, at an end which is remote from the base, has a rounded shape 24.
  • the cartridge is made from a malleable material which in this specification means a material which is capable of plastically deforming, without rupturing, at least to a predetermined extent eg. by at least 10%.
  • the cartridge may be made from a high density plastics material such as high density polypropylene.
  • the cartridge 16 forms an enclosure for a propellant material 26 which is of known composition and which is loaded into the cartridge under factory conditions using techniques which are known in the art.
  • An initiator 28 is loaded into the cartridge.
  • Control wires 30 lead from the initiator to a control unit, not shown, which is used in a known manner for initiating the blasting process.
  • Stemming 32 is placed into the hole 10 from the rock face 14 covering the cartridge to a desired extent.
  • the stemming is consolidated by being tamped in position.
  • the nature of the stemming and the way in which it is tamped are known in the art and for this reason are not further described herein.
  • a member 34 which is made from a plastics material such as polypropylene, is then placed over the stemming 32.
  • the member has a conical leading end 36 which faces downwardly into the stemming and, in this example, has a substantially planar trailing end 38 which faces upwardly.
  • the maximum diameter of the member 34 is slightly less than the nominal diameter of the hole 10.
  • a propellant charge 40 is placed on the member or, preferably, is incorporated in the member under factory conditions.
  • An initiator or igniter 42 is engaged with the propellant charge.
  • Control leads 44 lead from the initiator to the control unit which is used for firing the initiator 28.
  • the propellant 26 in the cartridge combusts and causes the release of high pressure jet material which is substantially in gaseous form.
  • the cartridge 16 expands outwardly and deforms, initially without rupturing, to confine the high pressure gas up to a stage at which the cartridge fractures at which point the high pressure jet material is released to cause fracture of the rock at one or more points at which high pressure stress regions are created.
  • substantial force is exerted on the stemming 32 and as the stemming is radially confined there is a tendency for the stemming to move upwardly and out of the hole.
  • This embodiment of the invention provides a technique for counteracting the force which tends to drive the stemming out of the hole and which originates from the propellant 26. This is achieved by firing the initiator 42 to initiate the propellant charge 40. When this occurs a force is applied to the trailing side 38 of the member and it is driven downwardly into the stemming 32 thereby producing a force which counteracts the upwardly directed force which is produced by the propellant 26. If the propellant charge 40 is ignited at a precisely determined time relatively to the instant at which the propellant 26 is ignited then the pressure waves which are transmitted through the stemming 32 from the propellant material 40 and from the propellant 26 on the other hand can, at least to a substantial extent, be cancelled out.
  • the member 34 When the propellant 40 is ignited the member 34 is driven downwardly.
  • additional stemming 50 may be placed over the member and the propellant material before deflagration takes place.
  • the member 34 has a conical leading end 36 but, on a trailing side, has a recessed formation 52.
  • the propellant charge 40 and the initiator 42 are located in the recessed formation.
  • stemming 50 is preferably placed over the member 34 and the propellant charge before ignition of the propellant charge takes place.
  • the member 34 When the charge is ignited the member 34 is driven downwardly thereby assisting in confining the underlying stemming 32.
  • the member 34 is however shaped so that there is a tendency for the member to expand radially outwardly when the member is driven towards the mouth of the hole. This may occur for example if the force which is released by the propellant 26 in the cartridge is significantly greater than the force which is produced by the propellant charge 40. A similar situation may also arise if the times at which the propellant 26 and the propellant charge 40 are initiated are such that there is no significant cancellation of the oppositely directed forces produced by these materials.
  • Figure 3 illustrates, somewhat schematically, a suitable control technique.
  • FIG 3 shows a control unit 60 which is connected to the control wires 30 and which is used to generate an electrical signal which is applied to the initiator 28 associated with the cartridge 16.
  • the control wires 44 shown in Figure 1 lead to a component 62 which is associated with the propellant charge 40.
  • the component 62 contains a capacitor 64 which is charged, preferably beforehand, by energy supplied by the control unit 60.
  • a timer 66 in the component 62 is started and after a predetermined time interval, which is programmed beforehand, the capacitor 64 is caused to discharge by closure of a switch 68, included in the timer, which then applies the energy stored in the capacitor to the initiator 42 which causes the propellant charge 40 to be fired.
  • the initiator 28 may have a similar timing mechanism associated with it.
  • the initiator 28 may be directly fired by means of a control signal from the control unit and this control signal may be used to start the timer 66 to ensure that the initiator 42 is fired a short interval after the initiator 28 is fired.
  • this technique can be reversed in that the initiator can be fired directly by means of a control signal from the control unit and the initiator 28 can then be fired a short interval after the propellant charge is ignited.
  • the important aspect here is that it is possible, through the use of suitable control techniques, to fire the propellant charge 40 and the propellant 26 within predetermined time intervals of each other in order to ensure that the pressure wave which is transferred to the stemming 32, by the propellant 26 is effectively counter-balanced by the member 34 which is driven into the stemming by the propellant charge 40.
  • Figure 4 illustrates another variation of the invention.
  • a hole 110 is drilled into a rock mass 112 from a face 114 using conventional drilling equipment, not shown.
  • the hole is drilled to a length which is at least four times the nominal diameter of the hole.
  • a cartridge 116 is placed into the hole.
  • the cartridge has a base 118 and a generally cylindrical wall 120 which extends upwards from the base and which, at an end which is remote from the base has a rounded shape 122.
  • the cartridge forms an enclosure for a propellant material 124 which is of known composition and which is loaded into the cartridge under factory conditions using techniques which are known in the art.
  • An initiator 126 is loaded into the cartridge, preferably on site.
  • Control wires 128 lead from the initiator to a control unit 130 which is located at a remote and safe position.
  • Stemming 132 is placed into the hole from the rock face 114 and covers the cartridge to a desired extent.
  • the stemming is consolidated by being tamped in position.
  • the base 118 of the cartridge is in close contact with a bottom 134 of the hole.
  • the intention in this regard is that the stemming should confine the cartridge on one side while the surrounding surface of the rock 112 should confine the cartridge on its remaining sides.
  • a shaped member 140 is placed in the hole over the stemming 132.
  • the member is made from a plastics material and includes a downwardly facing recessed formation 142 which, in this example, is substantially conical.
  • a propellant charge 144 is loaded into the formation 142, preferably under factory conditions.
  • An initiator or igniter 146 is engaged with the member 140 and control wires 148 lead from the initiator to the control unit 130.
  • additional stemming 150 is placed into the hole over the member 140 and is consolidated by being tamped downwardly.
  • Ignition of the propellant 124 by the initiator 126 causes the release of high pressure jet material which is substantially in gaseous form.
  • the cartridge 116 is designed to contain the expanding high pressure material and for this reason is allowed to deform outwardly, without initially rupturing, so that the wall 120 of the cartridge is forced into close contact with an opposing surface of the wall of the hole.
  • the cartridge does not fracture during this process for it is fabricated from a plastically deformable material.
  • the function of the cartridge in this respect, is to confine the high pressure gas for a limited period.
  • the function of the stemming on the other hand is to contain, to the maximum extent possible, the high pressure jet material which is released when the cartridge fractures.
  • the force which is generated by the high pressure jet material and which is applied to the stemming 132 is substantial and can cause the stemming 132 to be displaced to a significant extent in the hole 110. If movement of the stemming can be restricted then the pressure which is generated in the cartridge 124 can be contained so that the resulting force exerted by the high pressure jet material is increased.
  • the propellant 144 is ignited at a precisely determined time relatively to the time at which the propellant 124 is ignited. This is done by applying a suitable control signal, generated by the control unit 130, through the control wires 148 to the initiator 146.
  • the deflagrating propellant 144 directs a pressure wave into the stemming 132 which is timed and which is of a magnitude such that this pressure wave substantially counter-balances the pressure wave which is exerted on the stemming by the propellant 124.
  • the result is that the stemming 132 is effectively held stationary and maximum energy is extracted from the propellant 124 and applied to the surrounding rock 112 in order to crack the rock in an effective manner.
  • the member 140 helps to direct the pressure wave generated by the propellant 144 into the stemming 132 and the stemming 150, in turn, helps to confine the member in the hole.
  • the control mechanism is connected to the control unit 130 shown in Figure 4 by means of the control leads 128 and 148.
  • the control mechanism includes a capacitor 162 which is charged, beforehand, by means of a suitable charging voltage which is applied via the leads 148 to the capacitor.
  • the mechanism further includes a timer 164 which is turned on, to start a timing interval of a predetermined duration, by means of a control signal applied via the wires 148 from the control unit. At the end of the timing interval a switch 166 in the timer is closed and the capacitor is caused to discharge through the closed switch and direct the discharged energy into the initiator 146 which is associated with the propellant 142.
  • the control signal which is used to start the timer can also be used to fire the initiator 126.
  • the igniter 146 will be fired a short interval after the initiator 126 is fired. It is possible however to reverse the sequence of operations in that the igniter can be ignited before the initiator 126.
  • the sequence of operations in this regard is determined by the aforementioned requirement in that, as noted, the two pressure waves must be generated in such a way that they effectively meet and counteract each other within the mass of the stemming 132.

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Mining & Mineral Resources (AREA)
  • Geology (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Selective Calling Equipment (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Finger-Pressure Massage (AREA)
  • Catching Or Destruction (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

La présente invention se rapporte à un appareil de bourrage comportant un élément, une charge propulsive et un amorceur conçu pour mettre à feu la charge propulsive. La matière de bourrage (32) est placée dans le trou (10) à partir de la surface de la roche (14) recouvrant la cartouche sur une étendue souhaitée. La matière de bourrage est consolidée par bourrage sur place. Un élément (34), qui est composé d'une matière plastique telle que le polypropylène, est ensuite placé au-dessus de la matière de bourrage (32). Cet élément présente une extrémité avant conique (36) qui est tournée vers le bas à l'intérieur de ladite matière de bourrage et qui, dans cet exemple, présente une extrémité arrière sensiblement plane (38) qui est tournée vers le haut. Le diamètre maximum de l'élément (34) est légèrement inférieur au diamètre nominal du trou (10). Une charge propulsive (40) est placée sur l'élément ou, de préférence, est intégrée à cet élément en usine. Un amorceur ou allumeur (42) est amené au contact de la charge propulsive. Des fils conducteurs de commande (44) raccordent l'amorceur à l'unité de commande qui est utilisée pour déclencher l'amorceur (28).
PCT/ZA2002/000209 2002-01-03 2002-12-17 Dispositif de bourrage active WO2003060290A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US10/500,356 US20060169162A1 (en) 2002-01-03 2002-12-17 Activated stemming device
DE60214041T DE60214041D1 (de) 2002-01-03 2002-12-17 Aktivierte verdämmungsvorrichtung
CA002472533A CA2472533A1 (fr) 2002-01-03 2002-12-17 Dispositif de bourrage active
EP02796156A EP1463871B1 (fr) 2002-01-03 2002-12-17 Dispositif de bourrage active
AU2002360867A AU2002360867B2 (en) 2002-01-03 2002-12-17 Activated stemming device

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
ZA2001/5469 2002-01-03
ZA2001/5470 2002-01-03
ZA200105469 2002-01-03
ZA200105470 2002-01-03

Publications (2)

Publication Number Publication Date
WO2003060290A1 true WO2003060290A1 (fr) 2003-07-24
WO2003060290B1 WO2003060290B1 (fr) 2004-05-27

Family

ID=27145585

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ZA2002/000209 WO2003060290A1 (fr) 2002-01-03 2002-12-17 Dispositif de bourrage active

Country Status (7)

Country Link
US (1) US20060169162A1 (fr)
EP (1) EP1463871B1 (fr)
AT (1) ATE336640T1 (fr)
AU (1) AU2002360867B2 (fr)
CA (1) CA2472533A1 (fr)
DE (1) DE60214041D1 (fr)
WO (1) WO2003060290A1 (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005033474A1 (fr) * 2003-10-03 2005-04-14 International Technologies, Llc Procede de sautage et accessoire de sautage
WO2007033387A1 (fr) * 2005-05-27 2007-03-22 Marianna Suzanne Van Rensburg Dispositif de centrage de tube a chocs
RU2451264C1 (ru) * 2010-11-22 2012-05-20 Государственное образовательное учреждение высшего профессионального образования "Санкт-Петербургский государственный горный институт имени Г.В. Плеханова (технический университет)" Скважинная забойка
WO2014180101A1 (fr) * 2013-05-10 2014-11-13 武汉大学 Procédé de tir coussin combinant une limitation des dégâts de fond de trou et une excavation rapide
WO2015198282A1 (fr) * 2014-06-26 2015-12-30 Fourie Heinrich Johann Dispositif de support
RU2704694C1 (ru) * 2019-05-29 2019-10-30 Акционерное общество "Новосибирский механический завод "Искра" Подвесная скважинная забойка
CN116007462A (zh) * 2023-02-15 2023-04-25 武汉大学 一种用于水下爆破的孔底缓冲消能方法

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2005207543A1 (en) * 2004-01-26 2005-08-04 Nxco International Limited Rock breaking cartridge and use thereof
RU2526950C1 (ru) * 2013-02-26 2014-08-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Тихоокеанский государственный университет" Засыпная забойка взрывных скважин с элементами каменного материала
EP3465073A1 (fr) * 2016-05-26 2019-04-10 Master Blaster Proprietary Limited Procédé de dynamitage de trou de mine à ciel ouvert
CN109506533B (zh) * 2018-11-21 2024-01-23 中国电建集团成都勘测设计研究院有限公司 用于深孔爆破装药的空气间隔装置

Citations (5)

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Publication number Priority date Publication date Assignee Title
US4167139A (en) * 1977-05-23 1979-09-11 Austin Powder Company Time delay primer and method of using same
US5247886A (en) * 1992-10-14 1993-09-28 The Curators Of The University Of Missouri Blast plug and stemming construction for blast holes
RU2112207C1 (ru) * 1994-12-30 1998-05-27 Восточный научно-исследовательский горнорудный институт Способ формирования скважинного заряда
WO2001065199A1 (fr) * 2000-02-29 2001-09-07 Rocktek Ltd Douille de cartouche et cartouche pour trous de mine et procede d'utilisation
WO2002042711A1 (fr) * 2000-11-21 2002-05-30 International Technologies, Llc Dynamitage par trous de mine

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US3713386A (en) * 1970-06-22 1973-01-30 Colt Ind Operating Corp Range limited projectile system
US3706278A (en) * 1971-02-25 1972-12-19 Us Army Distributed propulsion for guns
JPH10500745A (ja) * 1994-04-14 1998-01-20 サンバースト エクスカベイション インコーポレイテッド 発破穴の穴尻加圧による硬質岩石の制御破砕

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4167139A (en) * 1977-05-23 1979-09-11 Austin Powder Company Time delay primer and method of using same
US5247886A (en) * 1992-10-14 1993-09-28 The Curators Of The University Of Missouri Blast plug and stemming construction for blast holes
RU2112207C1 (ru) * 1994-12-30 1998-05-27 Восточный научно-исследовательский горнорудный институт Способ формирования скважинного заряда
WO2001065199A1 (fr) * 2000-02-29 2001-09-07 Rocktek Ltd Douille de cartouche et cartouche pour trous de mine et procede d'utilisation
WO2002042711A1 (fr) * 2000-11-21 2002-05-30 International Technologies, Llc Dynamitage par trous de mine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
DATABASE WPI Section PQ Week 199851, 27 May 1998 Derwent World Patents Index; Class Q79, AN 1998-608316, XP002241423, KARAPETYAN YU M. ET AL.: "Blasting hole charge for use in open=cast ore mining - has additional air gap beneath closing charge of height related to closing charge" *

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005033474A1 (fr) * 2003-10-03 2005-04-14 International Technologies, Llc Procede de sautage et accessoire de sautage
US7387071B2 (en) 2003-10-03 2008-06-17 International Technologies, Llc Blasting method and blasting accessory
WO2007033387A1 (fr) * 2005-05-27 2007-03-22 Marianna Suzanne Van Rensburg Dispositif de centrage de tube a chocs
RU2451264C1 (ru) * 2010-11-22 2012-05-20 Государственное образовательное учреждение высшего профессионального образования "Санкт-Петербургский государственный горный институт имени Г.В. Плеханова (технический университет)" Скважинная забойка
WO2014180101A1 (fr) * 2013-05-10 2014-11-13 武汉大学 Procédé de tir coussin combinant une limitation des dégâts de fond de trou et une excavation rapide
WO2015198282A1 (fr) * 2014-06-26 2015-12-30 Fourie Heinrich Johann Dispositif de support
RU2704694C1 (ru) * 2019-05-29 2019-10-30 Акционерное общество "Новосибирский механический завод "Искра" Подвесная скважинная забойка
CN116007462A (zh) * 2023-02-15 2023-04-25 武汉大学 一种用于水下爆破的孔底缓冲消能方法

Also Published As

Publication number Publication date
ATE336640T1 (de) 2006-09-15
US20060169162A1 (en) 2006-08-03
WO2003060290B1 (fr) 2004-05-27
EP1463871B1 (fr) 2006-08-16
AU2002360867A1 (en) 2003-07-30
AU2002360867B2 (en) 2007-02-15
DE60214041D1 (de) 2006-09-28
CA2472533A1 (fr) 2003-07-24
EP1463871A1 (fr) 2004-10-06

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