FIELD: oil and gas production, particularly, devices for completion of oil and gas wells. SUBSTANCE: perforator has combustion chamber, chemical fuel, eroding component, additional chemical reagent and nozzle unit. The latter is located on side surface of combustion chamber. Eroding component is made in form of solid blocks or powdery and located in its own vessel and separated in space from chemical fuel and additional chemical reagent. Nozzle unit is multichannel. It may move in direction perpendicular to perforator axis and side surface of casing pipe by former for possible variation of gap between end face of nozzle unit body and casing pipe. Region of action of gas flow on perforating object is connected with perforator combustion chamber, with region accommodating eroding component, and with region housing additional chemical reagent by channels of nozzle unit. EFFECT: higher efficiency of process of casing pipe perforation due to acceleration of perforation process and increased perforating ability of perforator. 5 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
DRIVE GAS-TURBINE PLANT AT AIR DELIVERY TO COMBUSTION CHAMBER HOUSING THROUGH AIR DUCT SYSTEM | 1999 |
|
RU2175096C2 |
FIRE-HEAT-SHIELDING COATING AND INSTALLATION FOR PRODUCING SUCH SHIELDING | 2008 |
|
RU2366745C1 |
METHOD OF CASED WELL PERFORATION WITH HIGH-TEMPERATURE SUPERSONIC GAS JET AND DEVICE FOR METHOD EMBODIMENT | 1999 |
|
RU2194847C2 |
METHOD OF INCREASE OF RANGE CAPABILITY OF PROJECTILE (VERSIONS) AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2462686C2 |
METHOD FOR THERMODYNAMIC PERFORATION OF THE CASED WELL AND DEVICE FOR IMPLEMENTING THE SAME | 1993 |
|
RU2077660C1 |
SOLID PROPELLANT ROCKET ENGINE NOZZLE FLOW CONTROL UNIT | 2005 |
|
RU2293867C1 |
DEVICE TO INCREASE PROJECTILE FLIGHT DISTANCE | 2011 |
|
RU2465541C1 |
GEAR TO PERFORATE HOLES | 1993 |
|
RU2057910C1 |
GYRATING ROCKET STAGE WITH COMBINED POWER PLANT AND METHOD OF CONTROLLING ROCKET FLIGHT | 2010 |
|
RU2427507C1 |
FLOW REGULATOR OF SOLID-PROPELLANT ROCKET ENGINE NOZZLE | 1999 |
|
RU2156876C1 |
Authors
Dates
2003-06-20—Published
2001-05-28—Filed