US2732016A - macleod - Google Patents
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- Publication number
- US2732016A US2732016A US2732016DA US2732016A US 2732016 A US2732016 A US 2732016A US 2732016D A US2732016D A US 2732016DA US 2732016 A US2732016 A US 2732016A
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- United States
- Prior art keywords
- chamber
- well
- explosive
- pulsations
- bell
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Lifetime
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- 239000002360 explosive Substances 0.000 description 104
- 239000012530 fluid Substances 0.000 description 42
- 239000000446 fuel Substances 0.000 description 40
- 239000000203 mixture Substances 0.000 description 36
- 239000000126 substance Substances 0.000 description 36
- 239000007788 liquid Substances 0.000 description 30
- 230000000694 effects Effects 0.000 description 16
- 239000007789 gas Substances 0.000 description 16
- 239000007800 oxidant agent Substances 0.000 description 14
- 238000004880 explosion Methods 0.000 description 12
- 239000004020 conductor Substances 0.000 description 8
- 239000001301 oxygen Substances 0.000 description 8
- 229910052760 oxygen Inorganic materials 0.000 description 8
- MYMOFIZGZYHOMD-UHFFFAOYSA-N oxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 8
- LYGJENNIWJXYER-UHFFFAOYSA-N Nitromethane Chemical compound C[N+]([O-])=O LYGJENNIWJXYER-UHFFFAOYSA-N 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 6
- 238000002485 combustion reaction Methods 0.000 description 6
- 238000005755 formation reaction Methods 0.000 description 6
- 230000005484 gravity Effects 0.000 description 6
- 210000001736 Capillaries Anatomy 0.000 description 4
- 206010016754 Flashback Diseases 0.000 description 4
- 238000009835 boiling Methods 0.000 description 4
- 238000005474 detonation Methods 0.000 description 4
- 238000002309 gasification Methods 0.000 description 4
- 150000002430 hydrocarbons Chemical class 0.000 description 4
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 4
- 239000001294 propane Substances 0.000 description 4
- 230000004936 stimulating Effects 0.000 description 4
- SNIOPGDIGTZGOP-UHFFFAOYSA-N 1,2,3-propanetrioltrinitrate Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000003570 air Substances 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 2
- 239000012467 final product Substances 0.000 description 2
- 229960003711 glyceryl trinitrate Drugs 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 230000000737 periodic Effects 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000003638 reducing agent Substances 0.000 description 2
- 230000001105 regulatory Effects 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH DRILLING; MINING
- E21B—EARTH DRILLING, e.g. DEEP DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B37/00—Methods or apparatus for cleaning boreholes or wells
- E21B37/08—Methods or apparatus for cleaning boreholes or wells cleaning in situ of down-hole filters, screens, e.g. casing perforations, or gravel packs
Description
Jan. 24. 1956 N. A. M LEOD 2,732,016
APPARATUS R PRODUCING PULSATIONS TO CLEAR W CASING PERFORATIONS Filed Sept. 30, 1950 2 Sheets-Sheet l w 6 mL C ma mM A .n a m 0 N ATTORNEY Jan. 24. 1956 Filed Sept. 30, 1950 N. A. M LEOD APPARATUS FOR PRODUCING PULSATIONS TO CLEAR WELL CASING PERFORATIONS 2 Sheets-Sheet 2 INVENTOR.
Norman A. Mac Leod ATTORNEY APPARATUS FQR PRODUCING PULSATIONS TO @LEAR WELL CASlNG PERFORATIONS Norman A. MacLeod, Altadena, Calif. Application September 30, 1950, Serial No. 187,812
Claims. or. 166-623) My invention relates in general to the clearing of perforations in a well casing and in stimulating flow of fluid in the earth structure surrounding the well bore by application of explosively produced pulsations.
It is an object of my present invention to provide apparatus for feeding or moving an explosive substance or substances into a selected space and igniting the same in timed sequence so as to produce pulsations of such strength and character as to accomplish declogging of the openings of well casings and the opening of paths of flow of fluids in the surrounding strata, thereby increasing the flow of fluids into the well bore.
it is an object of the invention to provide apparatus whereby an oxidizer and a combustible substance mayv be fed into a selected space and measured quantities thereof, in substantially stoichiometrical proportions, are exploded in timed sequence so as to produce the desired pulsations. In the practice of the invention the oxidizer may consist of oxygen, air, or oxygen fortified air, and the combustible may consist of one of the hydrocarbons in gaseous form or capable of being converted to gaseous form in the selected space, for we ample, acetylene, methane, hydrogen, alcohol vapor, etc., may be employed. The fuel and the oxidizer are conveyed into the selected space through separate paths and upon being combined in this space are subjected to an ignition effect such as a spark from a sparkplug, for example, or the heat from an electrical heating element. The gases are preferably caused to flow into the selected space in stoichiometrical proportions, since this will result in an efiicient use of the fuel. The fuel substance or substances may be caused to flow into the selected space at a constant rate, periodic operation of the igniting means causingthe explosion of measured quantities of the fuel substance or substances. Also measuringmeans may be employed to feed quantities of the fuel substance or substances into the selected space, and upon the completion of the feeding operation actuation of the ignition means isefie'cted.
Where the invention is employed below the surface of a liquid in a well, the explosive fluid issubjected to pressure of a magnitude depending upon. the factors of submersion and specific gravity of the. liquid in the well. Under the conditions of pressure and confinement involved, the fuel is forcibly exploded, with an effect similar to detonation, thereby producing pulsations of great effectiveness for the cleaning of well casing and screen, and stimulating the flow of fluids in the surrounding formation. The selected space in which the explosions are produced is defined by a hollow metalbody, referred to hereinafter for simplicity asa hell.
or bell chamber having an outlet port or ports communicating with the well space. The capacity of this bell chamber is determined in accordance with the conditions of operation and desired strength of the individual pulsations. In one practice of the invention, the bell chamber is slowly moved upwardly or -downwardly in the well casing, thereby gradually changing the ponited States Patent 0 sition of the space in which the explosions occur in timed relation. The invention comprehends that in some practices of the invention it may be necessary to add small amounts of inert matter to the fuel substance or substances so as to maintain a gas volume at all times in the upper part of the bell chamber. For example, use of a fuel composition consisting of hydrogen and oxygen in stoichiometrical proportions would result in water as a final product which could interfere with the proper operation of the ignition means employed in the practice of the invention. The invention also comprehends the use of a mono-explosive such as nitromethane, instead of an oxidizer such as air, and a combustible, such as hydrocarbon.
A further object of the invention is to provide apparatus of the character herein described employing an oxidizer with a liquid fuel, and utilization of heat to produce gasification of the liquid fuel in the bell chamber or as it approaches the bell chamber. It is contemplated that the heat of explosion of previous explosions be utilized for this purpose, the liquid fuel being heated immediately prior to its entry into the bell chamber so that it will enter the bell chamber in gaseous condition. One of the advantages of this practice of the invention is that a larger quantity of fuel may be maintained in a given space, such as a fuel reservoir, disposed in a well in association with other equipment, thereby making it possible to maintain the pulsations over an extended period of time. Also, the invention contemplates the use of means for maintaining the apparatus and also fluid in the well at temperature within a desired range, so that there will be sufficient heat for gasification of fuel, and on the other hand, so that there will not be an excess of heat to cause boiling of the fluid in the well when this effect is not desired, or in some instances to produce boiling in thewell, for example, where it is desired to effect a removal of sand from a water well.
Where an open bell is employed to define the space in which the explosions are produced, whether the explosive substance or substances are fed into the upper or lower end of the bell chamber, depends upon the specific gravity of the substance or substances as compared to the specific gravity of the fluid in the well. Where mono-fuels are employed, such as nitromethane or nitroglycerine, such fuels will be fed into the bottom of the bell chamber and there exploded. Among the objects of the invention is the inclusion of a valve means and other expedients to prevent reverse flow or" the explosive effect into or through the fuel feeding system.
Further objects and advantages of the invention will be brought out in the following part of the specification wherein I have in detail described a preferred embodi nt of the invention for purpose of completely disclosing one manner in which the invention and its principles may be employed without limiting the scope of the invention defined in the appended claims.
Referring to the drawings, which are for illustrative purposes only:
Fig. 1 is a partly sectioned view showing a device employed in a preferred practice of the invention;
Fig. 2 is an enlarged fragmentary sectional view of the bell chamber situated at the lower end of the device shown in Fig. 1;
Fig. 3 is a schematic view showing a feeding mechanism which may be employed in the device disclosed.
ployed which defines a selected space or chamber 11 in which explosions are produced in timed relation. The bell has a side wall 12, an upper end member 13, and a bottom wall 14, there being laterally directed openings in the lower portion of the side wall 12, for communication of the space or chamber 11 with the interior space 16 of a well 17. The bell 10 is shown, in Fig. 1, within a perforated casing or well screen 18. The bottom wall 14 prevents downward discharge of combustion products and thereby avoids a jet action which would cause vertical movement of the bell 10 in the well. The force of the gases discharged laterally through the openings 15 is balanced.
According to the invention, an explosive substance or substances are fed into the chamber 11 and periodically exploded therein, the force of each explosion being transmitted out through openings 15, in opposite directions, into the interior 16 of the well 1.7. In accordance with the laws of hydrodynamics, the force of the explosion, after it leaves the openings 15, is transmitted in all directions. Certain of this pressure passes out through openings 19 in the casing 18. With each explosion there is an expansive efiect applied, and following each explosion there is a contractive efiect. The result of this is that a series of timed explosions produces in the space contiguous to the bell 10 a series of pulsations, or in other words, a series of cycles, each of which comprises an expansion followed by a contraction. These pulsations very rapidly and effectively produce declogging of the openings 19 of a casing or well screen 10, and likewise such pulsations, transmitted out into the surrounding formation 20 cause opening of flow channels for fluids in the surrounding formation, and so stimulate flow of fluids.
In the simple form of the invention an igniting means 21 for explosive substance in the space 11 is provided. This igniting means is shown as a spark gap such as employed in sparkplugs for internal combustion engines. The head part 13, in addition to supporting the elements of the spark gap 21, carries nozzles 22 and 23, having their jet openings 24 directed toward the spark gap 21 so that fluid jets issuing from the openings 24 will dislodge from the spark gap 21 any liquid, such as water, which may tend to close the gap and thereby interfere with proper functioning of the igniting means. The openings 24 of the nozzles 22 and 23 communicate respectively through check valves 25 and 26 with passages 27 and 28 through which an oxidizer and a combustible are conducted at such rates of flow or in such amounts that they will combine in the chamber 11 to form an explosive mixture susceptible to being ignited and exploded by the igniting means 21. The combustion of the explosive mixture produces a large volume of gas which expands and forces liquid within the well outwardly and upwardly. When the expansive force of the gas has been expended, there will be a contraction of the gas, and during this time the succeeding charge of fuel mixture is being fed into the chamber 11 from the passages 27 and 28 through the openings 24 of the nozzles 22 and 23. To hold the bell 10 substantially centralized within the well as shown in Fig. 1, bow springs 29 are secured thereto.
For cooperation with the parts just explained, with relation to Fig. 2, I provide a supply and control organization 30 which may be disposed within the well 17, relatively near the bell 10, or may be placed at or outside the upper end of the well. The organization 30 includes a supply section 31 and a control section 32. The supply section 31 is shown as having a shell or housing 33 for holding one or more containers such as schematically shown at 34 and 35. Two of these containers 34 and 35 are employed where the explosive employed in the chamber 11 consists of several fluids which are not of themselves combustible but which, upon being combined, form an explosive composition. The control section 32 is connected to the supply section 31 4 and is also connected through a slender connecting means 36 with the head 13 forming a part of the bell 10.
As shown in Fig. 3, the control section 32 has therein means for controlled feeding of fluids from the containers 34 and 35 to the nozzles 22 and 23, and also has means for actuation of the ignition means 21 in timed relation to the controlled feeding of fluids into the chamber 11. As schematically shown in Fig. 3, the control section 32 has therein double acting pumps 37 and 38. The pump 37 has a cylinder 39 in which a piston 40 is reciprocated by a rod 41. Inlet check valves 42, communicating with opposite ends of the cylinder 29, are connected through a duct 43, a pressure reducing valve 44, and duct members and 46 with the container 35.
The pump 38 has a cylinder 39' in which a piston 40 is reciprocated by a piston rod 41', the piston rods 41 and 41 being connected so that the pistons 40 and 40 will be rcciprocated in unison. Inlet check valves 42 connect the opposite ends of the cylinder 39' through a duct member 43', a pressure reducing valve 44, and duct members 45' and 46 with the container 34, Fig. 1.
In explaining the operation of the preferred form of the invention disclosed, it may be assumed that the reciprocating member 49 is moving upwardly and that the pistons 40 and 40' are being thereby moved upwardly so as to discharge through the upper discharge check valves 47 and 47' the fluid contents of the cylinders 39 and39' previously drawn into these cylinders 39 and 39 from the respective containers 35 and. 34, Fig. 1, through the upper intake check valves 42and 42. When the pistons 49 and 40' reach the upper ends of the cylinders 39 and 39, completely discharging fluid therefrom, the reciprocating member 49 will be in a position such as indicated by dotted lines 49', Figs 3. Continued upward movement of the reciprocating member 49 from the position 49 will cause it to move into the switch actuating position indicated bydotted lines 49a, closing switch 55 and actuating the electrical means 57 so that a spark will be produced across the gap of the igniting means 21 immediately following the discharge of the contents of the pumps 37 and 38 into the upper portion of the bell chamber 11. During the upward movement of the pistons 40 and 40', just described, volumes of fluid will be drawn into the lower portionsof the cylinders 39 and 39' through the lower intake valves 42 and 42, so that when the reciprocating member 49 moves downward from the raised position 49', there will be a subsequent feeding of explosive components into the chamber 11 followed by an ignition effect therein as the result of the closing of switch 56 by the member 49. The foregoing operations will be repeated as long as the motor means 48 is operated and as long as the supply of explosive components in the containers 34 and 35 lasts. Proportioning of the fluids delivered through the respective nozzles 22 and 23 may be controlled in part by differences in volume of the cylinders 39 and 39, and in part by the differences in pressure maintained in the duct members 43 and 43 by the pressure regulating valves 44 and 44, Fig. 3. The proportions of fuel and oxidizer are thus obtained for any selected mediums. For example, where propane and oxygen are employed, detonation will occur where the mixture fed into the bell chamber 11 contains between three and thirtyseven percent of propane.
Where a mono-fuel, such as nitromethane, or other liquid explosive is employed, my invention employs means such as shown in Fig. 4, for preventing flash-back of ignition efiect through ducts to the main supply tank. As indicated in Fig. 4, one or more check valves 70 and a flash-back barrier (or obturator) 71 are employed in the path of flow 72 of a liquid explosive. The barrier 71 comprises a body having a plurality of parallel capillary channels 73 whose total cross-sectional area may be greater than, but is of the same order as the cross-sectional area of the feed duct 74. In the use of an arrangement such as shown in Fig. 4, the charge of liquid explosive is forced through the duct 74, the passages 73 of the barrier 71, and through the check valve 70, by a following body of non-explosive liquid, so that after the entire quantity of liquid explosive passes through the check valve 70 it will be followed by a small amount of non-explosive liquid, which non-explosive liquid will occupy the space behind the check valve 70, the passages 73 of the barrier 71, and the duct 74. Should any explosive effect be trans mitted back through the check valve 70 when the charge of liquid explosive is fired in the space with which the valve 70 communicates, such explosive effect will be damped and extinguished by the capillary passages 73 and also by the non-explosive fluid contained in the path of flow 72 back of the check valve 70.
I claim:
1. In a device for producing pulsations in a well: means for defining in the well a chamber having communication with the interior of the well; separate container means for explosive components; means operative to consecutively feed separate quantities of said components into said chamber so as to form separate quantities of explosive mixture in said chamber; and means operative to consecutively explode said separate quantities of said explosive mixture in said chamber so as to transmit pulsations from said chamber into the well.
2. In a device for producing pulsations in a well: means for defining in the well a chamber having communication with the interior of the well; container means for explosive; walls forming at least one path of movement from said container means to said chamber; means operative to move consecutive portions of explosive from said container means through said path into said chamber; a source of electrical energy; electrical igniting means in said chamber; and means for intermittently supplying electrical energy from said source to said igniting means to fire consecutive portions of said explosives in said chamber so that pulsations will be transmitted from said chamber to the interior of the well.
3. In a device for producing pulsations in a well: means for defining in the well a chamber having communication with the interior of the well; separate container means for volatile explosive components; pump means operative to consecutively feed separate quantities of said components into said chamber so as to form separate quantities of explosive mixture in said chamber; and means operative to consecutively ignite said separate quantities of said explosive mixture in said chamber so as to transmit pulsations from said chamber into the well.
4. In a device for producing pulsations in a well: means for defining in the well a chamber having communication with the interior of the well; separate container means for volatile components; pump means operative to consecutively feed separate quantities of said components into said chamber, so as to form separate quantities of explosive mixture in said chamber; and electrical means operative in timed relation to said pump means to consecutively ignite said separate quantities of said explosive mixture in said chamber so as to transmit pulsations from said chamber into the well.
5. In a device for producing pulsations in a well: means for defining in the. well a chamber having communication with the interior of the well; separate container means for fluid explosive components; pump means operative to feed said components under high pressure into said chamber so as to form an explosive composition in said chamber; means operative to ignite consecutive portions of said explosive composition in said chamber so as to transmit pulsations from said chamber into the well; and pressure reducers for said fluid explosive components disposed between said container means and the inlet of said pump means.
6. In a device for producing pulsations in a well: means for defining in the well a chamber having only lateral communication with the interior of the well so that the issue of gases from said means will be lateral and cause minimum vertical movement of said means; separate container means for volatile explosive components; means operative to consecutively feed portions of said components into said chamber so as to form an explosive composition in said chamber; and means operative to ignite consecutive portions of said explosive composition in said chamber so as to transmit pulsations from said chamber into the well.
7. In a device for producing pulsations in a well: means 'for defining in the well a chamber having only equally distributed lateral communication with the interior of the well so that the forces of the issuing gases will be laterally directed and distributed so as to produce mimimum lateral and vertical movement of said means; container means for explosive; means operative to consecutively feed portions of said explosive into said chamber; and means operative to ignite the consecutive portions of said explosive in said chamber so as to transmit pulsations from said chamber into the well.
8. In a device for producing pulsations in a well: means for defining in the well a chamber having communication with the interior of the well; container means for explosive; walls forming at least one path of movement from said container means to said chamber; means oper ative to consecutively feed separate portions of said explosive from said container means through said path into said chamber; and means operating to fire said separate consecutively fed portions of said explosive in said chamber so that pulsations will be transmitted from said chamber to the interior of the well.
9. In a device for producing pulsations in a well; means for defining in the well a chamber having communication with the interior of the well; separate container means for explosive components; means operative to feed separate portions of said components consecutively into said chamber so as to consecutively form separate explosive compositions in said chamber; and means operative to consecutively explode said separate explosive compositions in said chamber so as to transmit pulsations from said chamber into the well.
10. In a device for producing pulsations in a Well: means for defining in the well a chamber having communication with the interior of the well; separate container means for volatile explosive components; means operative to feed separate measured quantities of said References Cited in the file of this patent UNITED STATES PATENTS 224,024 Mason Feb. 3, 1880 2,043,340 Tilbury et al. June 9, 1936 2,136,881 Johnson Nov. 15, 1938 2,331,058 Stick Oct. 5, 1943 2,362,829 Kinley Nov. 14, 1944 2,402,153 Elliott June 18, 1946 2,414,349 Alexander Jan. 14, 1947 2,421,528 Stelfen June 3, 1947 2,444,754 Stefien July 6, 1948 2,444,756 SteflFen July 6, 1948 2,450,366 Williams Sept. 28, 1948 2,506,853 Berg et al. May 9, 1950
Publications (1)
Publication Number | Publication Date |
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US2732016A true US2732016A (en) | 1956-01-24 |
Family
ID=3441750
Family Applications (1)
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US2732016D Expired - Lifetime US2732016A (en) | macleod |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3055427A (en) * | 1959-07-13 | 1962-09-25 | Phillips Petroleum Co | Self contained igniter-burner and process |
US3101117A (en) * | 1961-06-19 | 1963-08-20 | Bj Service Inc | Well treating method and apparatus |
US3101115A (en) * | 1956-10-16 | 1963-08-20 | Bj Service Inc | Well treating method and apparatus |
US3107725A (en) * | 1960-12-05 | 1963-10-22 | Pan American Petroleum Corp | Testing wells |
US3602304A (en) * | 1970-04-02 | 1971-08-31 | Amoco Prod Co | Check valve for use in gas fracturing |
US3674093A (en) * | 1970-06-24 | 1972-07-04 | Dale C Reese | Method and apparatus for stimulating the flow of oil wells |
US3680635A (en) * | 1969-12-30 | 1972-08-01 | Sun Oil Co Delaware | Method and apparatus for igniting well heaters |
US4103743A (en) * | 1976-10-29 | 1978-08-01 | Thomas L. Moran | Method and means of treating water wells |
US4823876A (en) * | 1985-09-18 | 1989-04-25 | Mohaupt Henry H | Formation stimulating tool with anti-acceleration provisions |
US4945984A (en) * | 1989-03-16 | 1990-08-07 | Price Ernest H | Igniter for detonating an explosive gas mixture within a well |
EP0620356A2 (en) * | 1993-04-14 | 1994-10-19 | DML DIESELMOTORENWERK LEIPZIG GmbH | Method and device for the cleaning of wellscreens in wells |
US20110315387A1 (en) * | 2010-06-25 | 2011-12-29 | Marat Shatikovich Gamerov | System and method for cleaning a bottom-hole formation zone of a wellbore |
Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US224024A (en) * | 1880-02-03 | Gleaning salt-wells | ||
US2043340A (en) * | 1934-05-01 | 1936-06-09 | Technicraft Engineering Corp | Well cleaner |
US2136881A (en) * | 1936-05-27 | 1938-11-15 | W J Nimmer | Well washer |
US2331058A (en) * | 1942-08-14 | 1943-10-05 | Lane Wells Co | Firing apparatus for gun perforators |
US2362829A (en) * | 1941-08-18 | 1944-11-14 | Myron M Kinley | Explosive screen cleaner |
US2402153A (en) * | 1944-03-18 | 1946-06-18 | Byron Jackson Co | Gun perforator |
US2414349A (en) * | 1941-08-25 | 1947-01-14 | Ford I Alexander | Method of and means for washing and cleaning well casing perforations and well holes by explosives |
US2421528A (en) * | 1944-07-26 | 1947-06-03 | Ralph M Steffen | Underground oil recovery |
US2444756A (en) * | 1946-01-04 | 1948-07-06 | Nat Secondary Recovery Corp | Apparatus for progressively heating oil sands surrounding oil wells |
US2444754A (en) * | 1946-01-04 | 1948-07-06 | Ralph M Steffen | Apparatus for heating oil wells and pumping oil therefrom |
US2450366A (en) * | 1944-11-24 | 1948-09-28 | Jerry D Williams | Apparatus and method for seismographic exploration shooting |
US2506853A (en) * | 1945-05-30 | 1950-05-09 | Union Oil Co | Oil well furnace |
-
0
- US US2732016D patent/US2732016A/en not_active Expired - Lifetime
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US224024A (en) * | 1880-02-03 | Gleaning salt-wells | ||
US2043340A (en) * | 1934-05-01 | 1936-06-09 | Technicraft Engineering Corp | Well cleaner |
US2136881A (en) * | 1936-05-27 | 1938-11-15 | W J Nimmer | Well washer |
US2362829A (en) * | 1941-08-18 | 1944-11-14 | Myron M Kinley | Explosive screen cleaner |
US2414349A (en) * | 1941-08-25 | 1947-01-14 | Ford I Alexander | Method of and means for washing and cleaning well casing perforations and well holes by explosives |
US2331058A (en) * | 1942-08-14 | 1943-10-05 | Lane Wells Co | Firing apparatus for gun perforators |
US2402153A (en) * | 1944-03-18 | 1946-06-18 | Byron Jackson Co | Gun perforator |
US2421528A (en) * | 1944-07-26 | 1947-06-03 | Ralph M Steffen | Underground oil recovery |
US2450366A (en) * | 1944-11-24 | 1948-09-28 | Jerry D Williams | Apparatus and method for seismographic exploration shooting |
US2506853A (en) * | 1945-05-30 | 1950-05-09 | Union Oil Co | Oil well furnace |
US2444756A (en) * | 1946-01-04 | 1948-07-06 | Nat Secondary Recovery Corp | Apparatus for progressively heating oil sands surrounding oil wells |
US2444754A (en) * | 1946-01-04 | 1948-07-06 | Ralph M Steffen | Apparatus for heating oil wells and pumping oil therefrom |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3101115A (en) * | 1956-10-16 | 1963-08-20 | Bj Service Inc | Well treating method and apparatus |
US3055427A (en) * | 1959-07-13 | 1962-09-25 | Phillips Petroleum Co | Self contained igniter-burner and process |
US3107725A (en) * | 1960-12-05 | 1963-10-22 | Pan American Petroleum Corp | Testing wells |
US3101117A (en) * | 1961-06-19 | 1963-08-20 | Bj Service Inc | Well treating method and apparatus |
US3680635A (en) * | 1969-12-30 | 1972-08-01 | Sun Oil Co Delaware | Method and apparatus for igniting well heaters |
US3602304A (en) * | 1970-04-02 | 1971-08-31 | Amoco Prod Co | Check valve for use in gas fracturing |
US3674093A (en) * | 1970-06-24 | 1972-07-04 | Dale C Reese | Method and apparatus for stimulating the flow of oil wells |
US4103743A (en) * | 1976-10-29 | 1978-08-01 | Thomas L. Moran | Method and means of treating water wells |
US4823876A (en) * | 1985-09-18 | 1989-04-25 | Mohaupt Henry H | Formation stimulating tool with anti-acceleration provisions |
US4945984A (en) * | 1989-03-16 | 1990-08-07 | Price Ernest H | Igniter for detonating an explosive gas mixture within a well |
EP0620356A2 (en) * | 1993-04-14 | 1994-10-19 | DML DIESELMOTORENWERK LEIPZIG GmbH | Method and device for the cleaning of wellscreens in wells |
EP0620356A3 (en) * | 1993-04-14 | 1995-07-19 | Leipzig Dieselmotoren Dml | Method and device for the cleaning of wellscreens in wells. |
US20110315387A1 (en) * | 2010-06-25 | 2011-12-29 | Marat Shatikovich Gamerov | System and method for cleaning a bottom-hole formation zone of a wellbore |
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