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RU2008150559A - METHODS FOR HYDRAULIC RIGGING OF THE FORMATION AND PRODUCTION OF A HYDROCARBON FLUID FROM THE LAYER - Google Patents

METHODS FOR HYDRAULIC RIGGING OF THE FORMATION AND PRODUCTION OF A HYDROCARBON FLUID FROM THE LAYER Download PDF

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Publication number
RU2008150559A
RU2008150559A RU2008150559/03A RU2008150559A RU2008150559A RU 2008150559 A RU2008150559 A RU 2008150559A RU 2008150559/03 A RU2008150559/03 A RU 2008150559/03A RU 2008150559 A RU2008150559 A RU 2008150559A RU 2008150559 A RU2008150559 A RU 2008150559A
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Russia
Prior art keywords
formation
propellant
cavity
wellbore
rocket fuel
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RU2008150559/03A
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Russian (ru)
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RU2432460C2 (en
Inventor
Лоран ПРУВО (GB)
Лоран ПРУВО
Бернар МОНТАРОН (FR)
Бернар Монтарон
Клод ВЕРКАМЕР (FR)
Клод ВЕРКАМЕР
Original Assignee
Шлюмбергер Текнолоджи Б.В. (Nl)
Шлюмбергер Текнолоджи Б.В.
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Publication of RU2008150559A publication Critical patent/RU2008150559A/en
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Publication of RU2432460C2 publication Critical patent/RU2432460C2/en

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    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B43/00Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
    • E21B43/25Methods for stimulating production
    • E21B43/26Methods for stimulating production by forming crevices or fractures
    • E21B43/263Methods for stimulating production by forming crevices or fractures using explosives

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  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Geology (AREA)
  • Mining & Mineral Resources (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

1. Способ гидравлического разрыва пласта, при котором через ствол скважины, проходящий через пласт породы, размещают компоненты ракетного топлива в полости, расположенной на радиальном расстоянии от ствола скважины и воспламеняют их для создания давления, достаточного для осуществления гидравлического разрыва пласта. ! 2. Способ по п.1, в котором пласт включает в себя карбонатную породу, являющуюся нефтеносной. ! 3. Способ по п.1, в котором ракетное топливо имеет время увеличения давления, составляющее по меньшей мере 0,4 мс. ! 4. Способ по п.1, в котором ствол скважины выполнен с возможностью доступа с поверхности для каротажного инструмента. ! 5. Способ по п.1, в котором полость является перфорационным каналом. ! 6. Способ по п.1, в котором полость является разрывом пласта. ! 7. Способ по п.1, в котором полость является микростволом скважины. ! 8. Способ по п.7, в котором микроствол скважины имеет диаметр, составляющий 13 см (4 дюйма) или менее. ! 9. Способ по п.7, в котором микроствол скважины имеет диаметр, составляющий 7 см (2 дюйма) или менее. ! 10. Способ по п.1, в котором ракетное топливо воспламеняют с использованием сигнала с поверхности. ! 11. Способ по п.1, в котором ракетное топливо воспламеняют с использованием механизма замедленного высвобождения энергии воспламенения, размещаемого вместе с ракетным топливом. ! 12. Способ по п.1, в котором ракетное топливо является твердым, гелеобразным или жидким. ! 13. Способ по п.1, в котором воспламеняют компоненты ракетного топлива для образования дополнительных полостей в пласте для повторных размещений дополнительных компонентов ракетного топлива. ! 14. Способ для подачи углеводородной тек� 1. A hydraulic fracturing method in which, through a wellbore passing through a rock formation, propellant components are placed in a cavity located at a radial distance from the wellbore and ignited to create a pressure sufficient to hydraulically fracture the formation. ! 2. The method of claim 1 wherein the formation includes a carbonate rock that is oil bearing. ! 3. The method of claim 1, wherein the propellant has a pressurization time of at least 0.4 ms. ! 4. The method of claim 1, wherein the wellbore is accessible from the surface for a logging tool. ! 5. The method of claim 1 wherein the cavity is a perforation. ! 6. The method of claim 1 wherein the cavity is a fracture. ! 7. The method of claim 1, wherein the cavity is a microborehole. ! 8. The method of claim 7, wherein the microborehole has a diameter of 13 cm (4 inches) or less. ! 9. The method of claim 7, wherein the microborehole has a diameter of 7 cm (2 inches) or less. ! 10. The method of claim 1 wherein the propellant is ignited using a signal from the surface. ! 11. The method of claim 1 wherein the propellant is ignited using a delayed ignition energy release mechanism provided with the propellant. ! 12. The method of claim 1, wherein the propellant is solid, gel, or liquid. ! 13. The method of claim 1, wherein propellant components are ignited to form additional cavities in the formation for re-accommodating additional propellant components. ! 14. Method for supplying hydrocarbon stream

Claims (14)

1. Способ гидравлического разрыва пласта, при котором через ствол скважины, проходящий через пласт породы, размещают компоненты ракетного топлива в полости, расположенной на радиальном расстоянии от ствола скважины и воспламеняют их для создания давления, достаточного для осуществления гидравлического разрыва пласта.1. A method of hydraulic fracturing, in which rocket fuel components are placed through a wellbore passing through a rock formation in a cavity located at a radial distance from the wellbore and ignited to create sufficient pressure to effect hydraulic fracturing. 2. Способ по п.1, в котором пласт включает в себя карбонатную породу, являющуюся нефтеносной.2. The method according to claim 1, in which the reservoir includes carbonate rock, which is oil-bearing. 3. Способ по п.1, в котором ракетное топливо имеет время увеличения давления, составляющее по меньшей мере 0,4 мс.3. The method according to claim 1, in which the rocket fuel has a pressure increase time of at least 0.4 ms. 4. Способ по п.1, в котором ствол скважины выполнен с возможностью доступа с поверхности для каротажного инструмента.4. The method according to claim 1, in which the wellbore is configured to access from the surface for a logging tool. 5. Способ по п.1, в котором полость является перфорационным каналом.5. The method according to claim 1, in which the cavity is a perforation channel. 6. Способ по п.1, в котором полость является разрывом пласта.6. The method according to claim 1, in which the cavity is a fracturing. 7. Способ по п.1, в котором полость является микростволом скважины.7. The method according to claim 1, in which the cavity is a microbore of the well. 8. Способ по п.7, в котором микроствол скважины имеет диаметр, составляющий 13 см (4 дюйма) или менее.8. The method of claim 7, wherein the microbore of the well has a diameter of 13 cm (4 inches) or less. 9. Способ по п.7, в котором микроствол скважины имеет диаметр, составляющий 7 см (2 дюйма) или менее.9. The method of claim 7, wherein the microbore of the well has a diameter of 7 cm (2 inches) or less. 10. Способ по п.1, в котором ракетное топливо воспламеняют с использованием сигнала с поверхности.10. The method according to claim 1, in which rocket fuel is ignited using a signal from the surface. 11. Способ по п.1, в котором ракетное топливо воспламеняют с использованием механизма замедленного высвобождения энергии воспламенения, размещаемого вместе с ракетным топливом.11. The method according to claim 1, in which the rocket fuel is ignited using a mechanism for the sustained release of ignition energy, placed together with the rocket fuel. 12. Способ по п.1, в котором ракетное топливо является твердым, гелеобразным или жидким.12. The method according to claim 1, in which the propellant is solid, gel or liquid. 13. Способ по п.1, в котором воспламеняют компоненты ракетного топлива для образования дополнительных полостей в пласте для повторных размещений дополнительных компонентов ракетного топлива.13. The method according to claim 1, in which ignite the components of rocket fuel to form additional cavities in the reservoir for re-placement of additional components of rocket fuel. 14. Способ для подачи углеводородной текучей среды из пласта с сетью разрывов, при котором направляют нагретую текучую среду в пласт через сеть разрывов, увеличивают подвижность углеводородных текучих сред в нагретой текучей среде и перемещают углеводородные текучие среды на поверхность, при этом обеспечивают доступность сети разрывов пласта путем помещения через ствол скважины, проходящий через пласт, компонентов ракетного топлива в полость, расположенную на радиальном расстоянии от упомянутого ствола скважины, и воспламеняют их для создания давления, достаточного для гидравлического разрыва пласта, тем самым обеспечивая увеличенный доступ к сети разрывов пласта. 14. A method for delivering a hydrocarbon fluid from a formation with a fracture network, in which a heated fluid is directed into the formation through a fracture network, increasing the mobility of hydrocarbon fluids in the heated fluid and moving hydrocarbon fluids to the surface, while ensuring the availability of the fracture network by placing, through the wellbore passing through the formation, rocket fuel components into a cavity located at a radial distance from said wellbore, and igniting them for Creating a pressure sufficient to fracture, thus providing increased access to the network fracturing.
RU2008150559/03A 2007-12-21 2008-12-19 Procedures for formation fracturing and extraction of hydrocarbon fluid medium from formation RU2432460C2 (en)

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US11/962,885 US20090159286A1 (en) 2007-12-21 2007-12-21 Method of treating subterranean reservoirs
US11/962,885 2007-12-21

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RU2432460C2 RU2432460C2 (en) 2011-10-27

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RU2432460C2 (en) 2011-10-27
CA2646168A1 (en) 2009-06-21
US20090159286A1 (en) 2009-06-25

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