US2348047A - Mud turbine and method of assembling the same - Google Patents

Mud turbine and method of assembling the same Download PDF

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Publication number
US2348047A
US2348047A US391336A US39133641A US2348047A US 2348047 A US2348047 A US 2348047A US 391336 A US391336 A US 391336A US 39133641 A US39133641 A US 39133641A US 2348047 A US2348047 A US 2348047A
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shaft
guides
runners
runner
turbine
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US391336A
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Yost Lloyd
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AO Smith Corp
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AO Smith Corp
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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
    • E21B4/00Drives for drilling, used in the borehole
    • E21B4/02Fluid rotary type drives
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making

Definitions

  • Patented May 1944 MUD TURBINE AND METHOD F ASSEM- BLING THE SAME maya you, Los Angela, cam., amm a a. o.
  • This invention relates to a mud turbine and Vmethod of assembling the same and has been venting cave in of th well.
  • the present invention is directed to the use of an adjustable runner and to a more simple assembly procedure in which the runners and guides of a multiple stage turbine are assembled with the shaft in the casing and individually secured to the shaft and casing, respectively.
  • the motive uid employed is mud which has a high viscosity as distinguished from water or vapor, and 'the utilized in the drilling of deep oil wells in which the relatively non-rotating drill casing I extends downwardly from the top of the well and is of smaller diameter than the hole 2 being drilled.
  • the turbine 3 At the lower end ofthe casing is the turbine 3, the vertical rotating shaft 4 of which extends downwardly to rotate the drill 5 at the bottom of the well.
  • 'Ihe turbine 3 is of the multiple stage type in order to develop the power necessary in the small diameter available. Usually a twenty or thirty stage turbine is employed depending somewhat upon the design of the runners and guides and the requirements.
  • the motive uid employed is mud which may be of the usual mud composition employed in drilling oil wells for cleaning the well and preventing cave in.
  • the mud is pumped down through casing I, turbine 3 and out at or near the drill 5 from whence it passes upwardly outside of casing l to the top of the well. It is then reclaimed and used over again. Normally this ilow of mud is at a very high rate.
  • runners 6 secured to the shaft 4 and guides 1 keyed to the casing I.
  • the runners 6 and guides 'l are usually from about two and one-half inches to about fou'r inches in height, and according to the invention, they are spaced apart a distance of from one to one and a half inches.
  • Figure 1 is a vertical section of a well showing the'turbine of this invention in place;
  • Fig. 2 is an enlarged vertical section of the turbine on the longitudinal center line with parts broken away;
  • Fig. 3 is a still further enlarged section of a runner and the two adjacent guides.
  • Fig. 4 is a transverse section on line 4-4 of Fig. 3.
  • the embodiment illustrated in the drawing is runners and guides, it was discovered that the thick mud employed for motive power quickly cut or wore away' the metal ofthe blades at the top and also bottom of the runners and guides. Such a turbine did not stand up for even the minimum number of hours necessary for con-'- tinuous service in a commercial operation.
  • Each runner 6 comprises the usual blades 8 radiating from a hub 9 having a frusto-conical inner surface.
  • the runner is secured to the shaft by the wedge action of an intermediate split adapter sleeve III which is tapered complementary to the taper of the inner surface of hub 9.
  • the sleeve I is tightened in place by meansvof a nut I
  • the tapered or wedge portion of sleeve III is split as at I2 to allow contraction for tightening on shaft 4 under the wedging action.
  • the sleeve III is preferably keyed to hub 9 by a suitable key I3 which prevents loosening of they nut caused by the tendency for relative rotation between the sleeve and hub.
  • runner 8 'Ihe construction of the runner 8 allows it to be secured to the smooth shaft at any adjusted position, and runners will not disturb the balance of the rotating parts as would be the case with keys or other forms of interlock with the shaft.
  • 'I'he guides 1 comprise the guide vanes I4 spaced around the circumference and held in place by an outer cylindrical web I5 and an' inner cylindrical web I6.
  • the outer web I5 has a slot I1 in its outer surface to receive a key I8 secured to the inside of casing and which holds all of the guides locked against rotation relative to each other and to the casing.
  • the inner web I6 has its inner surface substantially spaced from the shaft 4 and it has a flange .I9 at its lower edge extending inwardly toward the shaft 4.
  • a rubber or other suitable bearing is supported on the flange I9 inthe space between web I6 and shaft 4.
  • this bearing is of the fluted type to provide for self cleaning from mud and prevent excessive wear on the shaft.
  • the bearing 20 helps to keep the shaft and casing concentric at all times and prevents any misalignment of parts due to uneven side pressure: Although in some instances it might not be necessary to place a bearing at each guide, it is advisable to do so since it has been found that longer continuous service can be obtained in .this way.
  • the guides 1 are spaced apart by guide spacer sleeves 2
  • are preferably separate pieces, although they may be made integral with the webs I5 of the respective guides.
  • Suitable radial and thrust bearings 22 and 23 respectively may also be provided.
  • the bearings shown constitute the subject matter of copending applications Serial No. 391,335, filed May 1, 1941, for Ball thrust bearing for well drilling units, and 391,339 filed the same date, for Radial ball bearing, and issued to Patent No. 2,286,528 by the present inventor.
  • the lower end of the rotor shaft 4 isI supported by an adapter coupling 24 which rests on thrust bearing 23 and to which the drill shaft 25 is secured.”
  • the adapter 24 serves to direct the mud being discharged from the turbine into the center of the hollow drill shaft 25, and has two dia;- metricallyopposed circular recesses 26 in its outer surface.
  • the casing I has ⁇ threaded openings 21 corresponding to the recesses 26 and which are normally sealed by plugs 28.
  • a guide 1 is then lowered over the top end of the shaft until it rests on a stationary shelf ll provided in casing I just above the coupling 24.
  • a runner 9 is then dropped over the top end of shaft 4 and lowered until it rests on the first guide 1.
  • An appropriate tool is inserted from the top to engage the nut II and to turn it relative to the adapter sleeve I0. 'I'hreading of the nut on the adapter sleeve tends to push the runner 9 downwardly and may pull the sleeve I9 slightly upward until all parts are tight.
  • is dropped down in the casing I and a guide 1 is lowered upon it.
  • another runner 8 is applied in the same manner as that described for the first runner, and so on, until all of' the runners and guides are in place.
  • the upper guide 1 is held in place by an annular nut 3
  • a cap 32 is then secured to the upper end of the shaft to guide the mud towards ithe outer circumference of the casing where it enters the turbine blades.
  • the guides 1 are supported on casing by the sleeve 30 and the shaft 4 with its runners 9 is supported through coupling 24 on the thrust bearing 23.
  • the guides 1 are prevented from rotation by the key I8 while shaft 4 and its runners are free to rotate. 'I'he upper end of the drill shaft 25 is secured to the shaft 4 after assembly. I
  • the invention provides for the locating of each runner independently relative to its next lower guide so that all clearances are substantially alike in the finished structure.
  • Various embodiments of the invention may be employed within the scope of the accompanying claims.
  • a runner mounted on a rotary shaft and comprising a circular web carrying a series of blades, and having a frusto-conical inner surface spaced from said shaft, an adapter sleeve intermediate the web and shaft and having an outer frusta-conical surface complementary to the inner surface of the web, a nut threaded upon the thinner end of said adapter sleeve and pressing against said web to bias the two in opposite directions and wedge said sleeve in said web and upon said shaft, said sleeve being split in the thicker end to provide for its contraction upon said shaft, and a key interlocking said web and said adapter sleeve to prevent relative rotation therebetween.

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Mining & Mineral Resources (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Hydraulic Turbines (AREA)

Description

L. YOST May 2, 1944.
MUD TURBINE AND METHOD OF ASSEMBLING THE SAME Filed May l 1941 7U/ J/f d n MM i s w. 1in/7 4 ENT OR.
ATTRNEY.
Patented May 1944 MUD TURBINE AND METHOD F ASSEM- BLING THE SAME maya you, Los Angela, cam., amm a a. o.
Smith Corporation, Milwaukee, Wis., a corporation of New York IApplication May l, 1941, Serial No. 391,336
3 Claims.
This invention relates to a mud turbine and Vmethod of assembling the same and has been venting cave in of th well.
Heretofore in attempting to design and construct such turbines, it has been assumed that the blades o1' the runners and guides should be fairly close together to obtain the maximum torque values. Furthermore, the construction was such that the runners and guides had to be assembled on the shaft prior to insertion in the casing, and to do this, the guides were interlocked with outer spacer rings, and the runners were similarly interlocked with inner spacer rings. The guides were secured to the casing at the end of the structure and the runners were secured to the shaft at the ends of the structure.
The present invention is directed to the use of an adjustable runner and to a more simple assembly procedure in which the runners and guides of a multiple stage turbine are assembled with the shaft in the casing and individually secured to the shaft and casing, respectively. It takes into account that the motive uid employed is mud which has a high viscosity as distinguished from water or vapor, and 'the utilized in the drilling of deep oil wells in which the relatively non-rotating drill casing I extends downwardly from the top of the well and is of smaller diameter than the hole 2 being drilled. At the lower end ofthe casing is the turbine 3, the vertical rotating shaft 4 of which extends downwardly to rotate the drill 5 at the bottom of the well.
'Ihe turbine 3 is of the multiple stage type in order to develop the power necessary in the small diameter available. Usually a twenty or thirty stage turbine is employed depending somewhat upon the design of the runners and guides and the requirements.
The motive uid employed is mud which may be of the usual mud composition employed in drilling oil wells for cleaning the well and preventing cave in. The mud is pumped down through casing I, turbine 3 and out at or near the drill 5 from whence it passes upwardly outside of casing l to the top of the well. It is then reclaimed and used over again. Normally this ilow of mud is at a very high rate.
In the turbine illustrated there are alternate runners 6 secured to the shaft 4 and guides 1 keyed to the casing I. The runners 6 and guides 'l are usually from about two and one-half inches to about fou'r inches in height, and according to the invention, they are spaced apart a distance of from one to one and a half inches.
It was at first assumed that so great a spacing of the runners and guides would destroy the emciency of the turbine. However, in construct ing one with fairly small clearance between the and illustrated in one embodiment in the acl companying drawing. In the drawing:
Figure 1 is a vertical section of a well showing the'turbine of this invention in place;
Fig. 2 is an enlarged vertical section of the turbine on the longitudinal center line with parts broken away;
Fig. 3 is a still further enlarged section of a runner and the two adjacent guides; and
Fig. 4 is a transverse section on line 4-4 of Fig. 3.
The embodiment illustrated in the drawing is runners and guides, it was discovered that the thick mud employed for motive power quickly cut or wore away' the metal ofthe blades at the top and also bottom of the runners and guides. Such a turbine did not stand up for even the minimum number of hours necessary for con-'- tinuous service in a commercial operation.
By providing about a one and one-quarter inch clearance between runner and guide blades, the wear on the edges of the blades is kept at about the minimum without sacricing eiiciency. Thicker mud may make it possible and desirable to employ greater clearance, while a thinner motive fluid will require closer spacing to maintain the eiliciency.
Each runner 6 comprises the usual blades 8 radiating from a hub 9 having a frusto-conical inner surface. The runner is secured to the shaft by the wedge action of an intermediate split adapter sleeve III which is tapered complementary to the taper of the inner surface of hub 9.
The sleeve I is tightened in place by meansvof a nut I| disposed in a recess in the upper edge of hub 9 and threaded to the sleeve at its thinner end. Preferably, the tapered or wedge portion of sleeve III is split as at I2 to allow contraction for tightening on shaft 4 under the wedging action.
The sleeve III is preferably keyed to hub 9 by a suitable key I3 which prevents loosening of they nut caused by the tendency for relative rotation between the sleeve and hub.
'Ihe construction of the runner 8 allows it to be secured to the smooth shaft at any adjusted position, and runners will not disturb the balance of the rotating parts as would be the case with keys or other forms of interlock with the shaft.
'I'he guides 1 comprise the guide vanes I4 spaced around the circumference and held in place by an outer cylindrical web I5 and an' inner cylindrical web I6. The outer web I5 has a slot I1 in its outer surface to receive a key I8 secured to the inside of casing and which holds all of the guides locked against rotation relative to each other and to the casing. The inner web I6 has its inner surface substantially spaced from the shaft 4 and it has a flange .I9 at its lower edge extending inwardly toward the shaft 4.
A rubber or other suitable bearing is supported on the flange I9 inthe space between web I6 and shaft 4. Preferably this bearing is of the fluted type to provide for self cleaning from mud and prevent excessive wear on the shaft. The bearing 20 helps to keep the shaft and casing concentric at all times and prevents any misalignment of parts due to uneven side pressure: Although in some instances it might not be necessary to place a bearing at each guide, it is advisable to do so since it has been found that longer continuous service can be obtained in .this way.
The guides 1 are spaced apart by guide spacer sleeves 2| each of which corresponds in height to the height of a runner plus the clearance provided above and below the runner. The sleeves 2| are preferably separate pieces, although they may be made integral with the webs I5 of the respective guides.
Suitable radial and thrust bearings 22 and 23 respectively may also be provided. The bearings shown constitute the subject matter of copending applications Serial No. 391,335, filed May 1, 1941, for Ball thrust bearing for well drilling units, and 391,339 filed the same date, for Radial ball bearing, and issued to Patent No. 2,286,528 by the present inventor.
The lower end of the rotor shaft 4 isI supported by an adapter coupling 24 which rests on thrust bearing 23 and to which the drill shaft 25 is secured." The adapter 24 serves to direct the mud being discharged from the turbine into the center of the hollow drill shaft 25, and has two dia;- metricallyopposed circular recesses 26 in its outer surface. The casing I has` threaded openings 21 corresponding to the recesses 26 and which are normally sealed by plugs 28.
- 1n assembling the turbine, prior to attaching the bearings 22' and 23 and before the openings 21 are sealed, special pins 29 are inserted in the openings 21 to extend into the respective recesses 26. The shaft 4 is then lowered until the adapter coupling 24 rests on the pins 29; In practice, this Yowering will be exactly equal to the amount of clearance desired between each runner and its next adjacent lower guide.
A guide 1 is then lowered over the top end of the shaft until it rests on a stationary shelf ll provided in casing I just above the coupling 24. A runner 9 is then dropped over the top end of shaft 4 and lowered until it rests on the first guide 1. An appropriate tool is inserted from the top to engage the nut II and to turn it relative to the adapter sleeve I0. 'I'hreading of the nut on the adapter sleeve tends to push the runner 9 downwardly and may pull the sleeve I9 slightly upward until all parts are tight.
`After the first runner i is thus positioned, a guide spacer ring 2| is dropped down in the casing I and a guide 1 is lowered upon it. Then another runner 8 is applied in the same manner as that described for the first runner, and so on, until all of' the runners and guides are in place. The upper guide 1 is held in place by an annular nut 3| threaded to the casing and pressing down on the guide. A cap 32 is then secured to the upper end of the shaft to guide the mud towards ithe outer circumference of the casing where it enters the turbine blades.
The structure is then laid horizontal and the pins 29 removed from openings 21. The plugs 29- are then applied to seal openings 21 and the bearings 22 and 23 are attached to the lower end of the turbine, vthe shaft 4 being raised to normal operating position with the desired clearance be- -tween each runner and its next adjacent lower guide.l
The guides 1 are supported on casing by the sleeve 30 and the shaft 4 with its runners 9 is supported through coupling 24 on the thrust bearing 23. The guides 1 are prevented from rotation by the key I8 while shaft 4 and its runners are free to rotate. 'I'he upper end of the drill shaft 25 is secured to the shaft 4 after assembly. I
The invention provides for the locating of each runner independently relative to its next lower guide so that all clearances are substantially alike in the finished structure. Various embodiments of the invention may be employed within the scope of the accompanying claims.
The invention is claimed as follows:
1. In a turbine of the class described, a runner mounted on a rotary shaft and comprising a circular web carrying a series of blades, and having a frusto-conical inner surface spaced from said shaft, an adapter sleeve intermediate the web and shaft and having an outer frusta-conical surface complementary to the inner surface of the web, a nut threaded upon the thinner end of said adapter sleeve and pressing against said web to bias the two in opposite directions and wedge said sleeve in said web and upon said shaft, said sleeve being split in the thicker end to provide for its contraction upon said shaft, and a key interlocking said web and said adapter sleeve to prevent relative rotation therebetween.
2. In the assembly of aturbine of the class described, the method of first locating the rotor shaft below its normal operating position in the casing by a distance substantially equal to the clearance to be provided between each runner and its next adjacent lower guide, assembling the runners and guides alternately with the guides spaced apart to accommodate the runners and provide4 clearance between the runners and adjacent guides securing each runner to the rotor shaft as the same is placed against its next adjacent lower guide. thereafter moving the shaft and its attached runners upwardly relathe same apart to accommodate the runners and provide clearance between the runners and adjacent guides; securing each runner to the rotor shaft as the same is placed against its next adjacent lower guide, thereafter moving the shaft and its attached runners upwardly relative to the casing an amount equal to the clearance to be provided between the respective runners and their next adjacent lower guides, and securing the shaft for rotation. in its final operating position.
LLOYD YOST.
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Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2452581A (en) * 1944-06-07 1948-11-02 Standard Telephones Cables Ltd Turbogenerator
US2588311A (en) * 1946-10-28 1952-03-04 Engineering Dev Company Inc Oil well drilling apparatus
US2591488A (en) * 1946-11-08 1952-04-01 Smith Corp A O Balanced turbodrill
US2592519A (en) * 1948-11-08 1952-04-08 California Research Corp Turbodrill thrust balancing apparatus
US2613917A (en) * 1948-04-14 1952-10-14 California Research Corp Turbine-impact drill
US2646962A (en) * 1947-02-19 1953-07-28 Engineering Dev Company Inc Fluid motor for driving rotary tools
US2800296A (en) * 1954-10-14 1957-07-23 Borg Warner Turbine
US2983481A (en) * 1957-03-01 1961-05-09 Tiraspolsky Wladimir Motors for subterranean drilling
US2991837A (en) * 1957-05-29 1961-07-11 California Research Corp Turbo drill thrust bearings
US3018997A (en) * 1956-05-28 1962-01-30 Neyrpic Ets Turbine unit for turbodrills and turbocorers
US3039735A (en) * 1956-10-31 1962-06-19 Turbodrill Internat Corp Motor for subterranean work
US3159222A (en) * 1958-09-30 1964-12-01 Dresser Ind Turbodrill
US4340334A (en) * 1980-01-30 1982-07-20 Maurer Engineering, Inc. Turbodrill with rubber rotor bearings
US4475605A (en) * 1981-09-10 1984-10-09 Vsesojuzny Nauchnoissledovatelsky Institut Burovoi Tekhniki Turbodrill
US20090223676A1 (en) * 2006-07-08 2009-09-10 Alan Martyn Eddison Selective Agitation
US20100212912A1 (en) * 2005-01-14 2010-08-26 Alan Martyn Eddison Valve
US20100270034A1 (en) * 2007-11-20 2010-10-28 National Oilwell Varco, L.P. Wired multi-opening circulating sub
WO2012051382A1 (en) * 2010-10-13 2012-04-19 Houvener Robert C Hydrokinetic energy transfer device and method
US20130264119A1 (en) * 2012-03-26 2013-10-10 Gunther H-H. von Gynz-Rekowski Hammer Drill
US8770318B2 (en) 2010-04-01 2014-07-08 National Oilwell Varco, L.P. Drilling motor with a locking collet sleeve stabilizer
US20150060144A1 (en) * 2013-08-27 2015-03-05 Smith International, Inc. Turbine blade for turbodrills
RU2581856C1 (en) * 2015-03-23 2016-04-20 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Volumetric downhole motor
US20160312536A1 (en) * 2014-01-16 2016-10-27 China University Of Petroleum-Beijing Line projection blade turbine stator-rotor assembly and turbine motor
RU2610490C2 (en) * 2014-10-20 2017-02-13 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Turbodrill
RU2624085C1 (en) * 2016-01-18 2017-06-30 Товарищество С Ограниченной Ответственностью "Научно-Внедренческий Центр Алмас" Volumetric downhole motor
RU2698336C2 (en) * 2017-11-07 2019-08-26 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Well drilling method
EA034947B1 (en) * 2018-04-09 2020-04-09 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Volumetric downhole motor
RU2721987C1 (en) * 2019-06-24 2020-05-25 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Volumetric downhole motor
WO2022231407A1 (en) * 2021-04-27 2022-11-03 Токтамыс Нусипхулович Мендебаев Downhole positive displacement motor
RU2790647C1 (en) * 2021-12-03 2023-02-28 Товарищество С Ограниченной Ответственностью "Научно-Внедренческий Центр Алмас" Volumetric downhole motor

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2452581A (en) * 1944-06-07 1948-11-02 Standard Telephones Cables Ltd Turbogenerator
US2588311A (en) * 1946-10-28 1952-03-04 Engineering Dev Company Inc Oil well drilling apparatus
US2591488A (en) * 1946-11-08 1952-04-01 Smith Corp A O Balanced turbodrill
US2646962A (en) * 1947-02-19 1953-07-28 Engineering Dev Company Inc Fluid motor for driving rotary tools
US2613917A (en) * 1948-04-14 1952-10-14 California Research Corp Turbine-impact drill
US2592519A (en) * 1948-11-08 1952-04-08 California Research Corp Turbodrill thrust balancing apparatus
US2800296A (en) * 1954-10-14 1957-07-23 Borg Warner Turbine
US3018997A (en) * 1956-05-28 1962-01-30 Neyrpic Ets Turbine unit for turbodrills and turbocorers
US3039735A (en) * 1956-10-31 1962-06-19 Turbodrill Internat Corp Motor for subterranean work
US2983481A (en) * 1957-03-01 1961-05-09 Tiraspolsky Wladimir Motors for subterranean drilling
US2991837A (en) * 1957-05-29 1961-07-11 California Research Corp Turbo drill thrust bearings
US3159222A (en) * 1958-09-30 1964-12-01 Dresser Ind Turbodrill
US4340334A (en) * 1980-01-30 1982-07-20 Maurer Engineering, Inc. Turbodrill with rubber rotor bearings
US4475605A (en) * 1981-09-10 1984-10-09 Vsesojuzny Nauchnoissledovatelsky Institut Burovoi Tekhniki Turbodrill
US20100212912A1 (en) * 2005-01-14 2010-08-26 Alan Martyn Eddison Valve
US8069926B2 (en) 2005-01-14 2011-12-06 Andergauge Limited Method of controlling flow through a drill string using a valve positioned therein
US20090223676A1 (en) * 2006-07-08 2009-09-10 Alan Martyn Eddison Selective Agitation
US8167051B2 (en) 2006-07-08 2012-05-01 National Oilwell Varco, L.P. Selective agitation
US20100270034A1 (en) * 2007-11-20 2010-10-28 National Oilwell Varco, L.P. Wired multi-opening circulating sub
US8863852B2 (en) 2007-11-20 2014-10-21 National Oilwell Varco, L.P. Wired multi-opening circulating sub
US8770318B2 (en) 2010-04-01 2014-07-08 National Oilwell Varco, L.P. Drilling motor with a locking collet sleeve stabilizer
WO2012051382A1 (en) * 2010-10-13 2012-04-19 Houvener Robert C Hydrokinetic energy transfer device and method
US20130264119A1 (en) * 2012-03-26 2013-10-10 Gunther H-H. von Gynz-Rekowski Hammer Drill
US9488010B2 (en) * 2012-03-26 2016-11-08 Ashmin, Lc Hammer drill
US20150060144A1 (en) * 2013-08-27 2015-03-05 Smith International, Inc. Turbine blade for turbodrills
US20160312536A1 (en) * 2014-01-16 2016-10-27 China University Of Petroleum-Beijing Line projection blade turbine stator-rotor assembly and turbine motor
RU2610490C2 (en) * 2014-10-20 2017-02-13 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Turbodrill
RU2581856C1 (en) * 2015-03-23 2016-04-20 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Volumetric downhole motor
RU2624085C1 (en) * 2016-01-18 2017-06-30 Товарищество С Ограниченной Ответственностью "Научно-Внедренческий Центр Алмас" Volumetric downhole motor
RU2698336C2 (en) * 2017-11-07 2019-08-26 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Well drilling method
EA034947B1 (en) * 2018-04-09 2020-04-09 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Volumetric downhole motor
RU2721987C1 (en) * 2019-06-24 2020-05-25 Товарищество с ограниченной ответственностью "Научно-внедренческий центр "Алмас" Volumetric downhole motor
WO2022231407A1 (en) * 2021-04-27 2022-11-03 Токтамыс Нусипхулович Мендебаев Downhole positive displacement motor
RU2790647C1 (en) * 2021-12-03 2023-02-28 Товарищество С Ограниченной Ответственностью "Научно-Внедренческий Центр Алмас" Volumetric downhole motor

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