CN107152237B - A kind of large torque self-balancing low speed turbodrill - Google Patents

A kind of large torque self-balancing low speed turbodrill Download PDF

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Publication number
CN107152237B
CN107152237B CN201710554352.5A CN201710554352A CN107152237B CN 107152237 B CN107152237 B CN 107152237B CN 201710554352 A CN201710554352 A CN 201710554352A CN 107152237 B CN107152237 B CN 107152237B
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China
Prior art keywords
drill bit
screwed connection
interior
circle
mandrel
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Expired - Fee Related
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CN201710554352.5A
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Chinese (zh)
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CN107152237A (en
Inventor
李陵
叶哲伟
陈波
张海波
钟梦颖
程成
赵勇
黄凯
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Southwest Petroleum University
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Southwest Petroleum University
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Publication of CN107152237B publication Critical patent/CN107152237B/en
Expired - Fee Related legal-status Critical Current
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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
    • 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
    • E21B10/00Drill bits
    • E21B10/42Rotary drag type drill bits with teeth, blades or like cutting elements, e.g. fork-type bits, fish tail bits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B13/00Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
    • F03B13/02Adaptations for drilling wells

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  • Engineering & Computer Science (AREA)
  • Geology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Mechanical Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Earth Drilling (AREA)
  • Processing Of Stones Or Stones Resemblance Materials (AREA)

Abstract

The present invention relates to a kind of large torque self-balancing low speed turbodrills of unconventional tight stratum drillng operation.It meets the process requirements of unconventional tight stratum drillng operation.Its technical characteristic is: interior turbo blade group trap is on mandrel outer circle upper step axis, nut and the screwed connection of mandrel upper end;Outer turbo blade combination merging inner cylinder intracoelomic cavity, inner cylinder upper end and the screwed connection of top chock lower end, inner cylinder lower end and the screwed connection of step upper end;Transmission shaft upper end and the screwed connection of mandrel lower end, transmission shaft lower end and interior bit upper end screwed connection;Transmission cylinder upper end and the screwed connection of step lower end, transmission cylinder lower end and outer bit upper end screwed connection;Three gear shafts are separately mounted in the middle part of transmission cylinder in three through-holes, and three governor gears are separately mounted on three gear shafts.Interior drill bit of the invention and outer drill bit reversely cut rock stratum, the broken rock torque of autobalance both sides, the absolute drilling speed reduction of interior drill bit and outer drill bit, output torque increase relatively.

Description

A kind of large torque self-balancing low speed turbodrill
Technical field
The present invention relates to a kind of large torque self-balancing low speed turbodrills of unconventional tight stratum drillng operation.
Background technique
As the contradiction between ever-increasing world energy sources demand and existing traditional resource abatement is increasingly sharpened, the whole nation is right The demand of unconventional petroleum resources is also increasingly urgent to.Compared to traditional petroleum resources, the type and preservation of unconventional petroleum resources Form is more various, and distribution is more extensive, and potential resources is much larger than conventional gas and oil resource.Unconventional oil and gas reservoir properties are poor, Porosity, permeability are low, and especially unconventional tight stratum hardness is high, intensity is big, and drillability is poor.The mainstream used both at home and abroad at present The main helicoid hydraulic motor of mud motor, turbodrill and electronic down-hole equipment.Well of electrician's down-hole equipment due to high temperature and pressure Lower bad working environments and electric drill pole technology it is immature, it is limited to lead application at present.Helicoid hydraulic motor is widely used, but due to elastomer stator Property is extremely unstable under high temperature environment, therefore for ultradeep well helicoid hydraulic motor application critical constraints, and the output of helicoid hydraulic motor Drilling speed is lower, for scleroid unconventional tight stratum using unsatisfactory.And turbodrill has requested rubber material Limitation, has obtained fabulous application, and possess high output drilling speed and extremely low vibratility under ultradeep well hot environment, Scleroid unconventional tight stratum drilling well is very suitable to use.
However turbodrill conventional at present also has its own limitation, it is excessively high that turbodrill exports drilling speed, and exports Torque is very small, results in that its drilling efficiency is low, thus match turbodrill drilling speed and torque it is extremely important.It is current simultaneously Mud motor all have the defects that one it is common, be exactly its export drilling torque while, drilling tool shell can also bear phase The reaction torque answered, the reaction torque directly act on upper drilling string by drilling tool shell, directly result in drill string and twist deformation, especially Its reaction torque in build-up process usually makes the offset of drilling tool face generation certain angle, so that drilling tool face centering is non- It is often difficult, deflecting difficulty is substantially increased, the time of drillng operation is extended, causes a degree of economic loss.
Based on above-mentioned technical background, the present invention provides a kind of large torque self-balancing low speed turbodrill, guarantee that turbine bores While tool exports reasonable drilling speed and torque, conventional turbine drilling tool shell is overcome to bear the defect of reaction torque effect.
Summary of the invention
The purpose of the present invention is: the process requirements in order to meet unconventional tight stratum drillng operation provide a kind of big Torque self-balancing low speed turbodrill.
In order to achieve the above object, the invention adopts the following technical scheme: a kind of large torque self-balancing low speed turbodrill, Be combined by outer housing, self-aligning bearing a, nut, top chock, outer turbo blade, inner cylinder, the combination of interior turbo blade, mandrel, Step, self-aligning bearing b, transmission cylinder, governor gear, gear shaft, self-aligning bearing c, thrust bearing a, anti-lost end cap, thrust axis B, transmission shaft, wearing bush, interior drill bit and outer drill bit is held to constitute;Its structure feature is: outer housing upper end and upper drilling string screw thread connect It connects;Mandrel outer circle top is set as Step Shaft, and mandrel lower part is circumferentially uniformly arranged cavity space inside and outside three through-hole connection mandrels;It is interior Turbo blade group trap is on mandrel outer circle upper step axis, nut and the screwed connection of mandrel upper end, turbine leaf in nut compressing Piece combination;Outer turbo blade, which combines, is placed in inner cylinder intracoelomic cavity, inner cylinder upper end and the screwed connection of top chock lower end, under inner cylinder End and the screwed connection of step upper end, top chock and step compress outer turbo blade combination;Self-aligning bearing a is mounted on On top chock outer circle step surface, self-aligning bearing b is mounted on step inner hole step surface;Transmission shaft upper end and mandrel lower end Screwed connection, transmission shaft lower end and interior bit upper end screwed connection;Gear is set as in the middle part of transmission shaft outer circle;Transmission cylinder upper end and The screwed connection of step lower end, transmission cylinder lower end and outer bit upper end screwed connection;It is driven in the middle part of tube inner chamber and a ring is set Step surface, week in the middle part of transmission cylinder are enclosed in connected in star, one circle step surface of transmission tube inner chamber top setting, transmission cylinder outer circle lower part setting one Inner cavity upper stage terraces and outer circle lower stage terrace are connected to three through-holes are uniformly arranged;Three gear shafts are separately mounted to be driven In three through-holes in cylinder middle part, three governor gears are separately mounted on three gear shafts, and three governor gears are in transmission cylinder In annular groove in the middle part of chamber;Self-aligning bearing c is mounted on transmission cylinder outer circle lower stage terrace;Anti-lost end cover lumen upper end setting One circle raised step, anti-lost end cap and the screwed connection of outer housing lower end;One circle step surface of setting, outer drill bit in the middle part of outer drill bit inner cavity One circle step surface of outer circle top setting, outer drill bit outer circle lower part and lower end surface are inlaid with cutting tooth;Thrust bearing a is mounted on outer brill On head outer circle upper stage terrace, thrust bearing b is mounted on outer drill bit inner cavity middle bench face;Interior drill bit lower part is provided with jet stream Hole connection inner hole and lower end surface, interior drill bit lower end surface are inlaid with cutting tooth, and interior drill bit outer circle is set as Step Shaft;Wearing bush installation On interior drill bit outer circle Step Shaft, wearing bush is made of wear-resistant material.
It is installed hand, the gear in the middle part of transmission shaft outer circle is intermeshed with three governor gears respectively.
The beneficial effects of the present invention are: (1) interior drill bit of the invention and outer drill bit reversely cut rock stratum, autobalance relatively The broken rock torque of both sides avoids the harm of traditional mud motor reaction torque effect;(2) present invention utilizes gear-driven The high drilling speed that conventional turbine drilling tool rotor exports is decomposed into two relatively reversed drilling speeds of interior drill bit and outer drill bit, made by principle The absolute drilling speed of interior drill bit and outer drill bit reduces, and output torque increases, and is suitable for unconventional fine and close rock high speed and creeps into;(3) this hair The bright use for avoiding rubber structure part is suitable for Temperature Deep hyperbaric environment;(4) structure of the invention is compact, adapts to underground ring Border.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of large torque self-balancing low speed turbodrill of the present invention;
Fig. 2 is Figure 1A-A cross-sectional view;
In figure: 1. outer housings, 2. self-aligning bearing a, 3. nuts, 4. top chocks, 5. outer turbo blade combinations, 6. inner cylinders Body, turbo blade combination, 8. mandrels, 9. steps, 10. self-aligning bearing b, 11. transmission cylinders, 12. governor gears, 13. in 7. Gear shaft, 14. self-aligning bearing c, 15. thrust bearing a, 16. anti-lost end caps, 17. thrust bearing b, 18. transmission shafts, 19. abrasionproofs It covers, drill bit, 21. outer drill bits in 20..
Specific embodiment
As shown in Figure 1, a kind of large torque self-balancing low speed turbodrill of the present invention, be by outer housing 1, self-aligning bearing a2, Nut 3, top chock 4, outer turbo blade combination 5, inner cylinder 6, interior turbo blade combine 7, mandrel 8, step 9, aligning Bearing b10, transmission cylinder 11, governor gear 12, gear shaft 13, self-aligning bearing c14, thrust bearing a15, anti-lost end cap 16, thrust Bearing b17, transmission shaft 18, wearing bush 19, interior drill bit 20 and outer drill bit 21 are constituted;Its structure feature is: 1 upper end of outer housing and upper Portion's drill string screwed connection;8 outer circle top of mandrel is set as Step Shaft, and 8 lower part of mandrel is circumferentially uniformly arranged three through-hole connection cores Cavity space inside and outside axis 8;Interior turbo blade combines 7 sets on 8 outer circle upper step axis of mandrel, and nut 3 and 8 upper end screw thread of mandrel connect It connects, nut 3 compresses interior turbo blade combination 7;Outer 5 merging 6 inner cavity of inner cylinder of turbo blade combination, 6 upper end of inner cylinder and upper axis 4 lower end screwed connection of seat, the 9 upper end screwed connection of 6 lower end of inner cylinder and step are held, top chock 4 and step 9 compress Outer turbo blade combination 5;Self-aligning bearing a2 is mounted on 4 outer circle step surface of top chock, and self-aligning bearing b10 is mounted on lower bearing On 9 inner hole step surfaces of seat;The 8 lower end screwed connection of 18 upper end of transmission shaft and mandrel, terminal filament on 18 lower end of transmission shaft and interior drill bit 20 Button connection;Gear is set as in the middle part of 18 outer circle of transmission shaft;The 9 lower end screwed connection of 11 upper end of transmission cylinder and step, transmission cylinder The 21 upper end screwed connection of 11 lower ends and outer drill bit;One ring annular groove is set in the middle part of 11 inner cavity of transmission cylinder, on 11 inner cavity of transmission cylinder One circle step surface of portion's setting, 11 outer circle lower part of transmission cylinder setting, one circle step surface, 11 middle part of transmission cylinder is circumferential to be uniformly arranged three Through-hole is connected to inner cavity upper stage terrace and outer circle lower stage terrace;Three gear shafts 13 are separately mounted to 11 three, middle part of transmission cylinder In through-hole, three governor gears 12 are separately mounted on three gear shafts 13, and three governor gears 12 are in 11 inner cavity of transmission cylinder In the annular groove at middle part;Self-aligning bearing c14 is mounted on 11 outer circle lower stage terrace of transmission cylinder;Anti-lost 16 inner cavity upper end of end cap One circle raised step of setting, the 1 lower end screwed connection of anti-lost end cap 16 and outer housing;One circle step of setting in the middle part of outer 21 inner cavity of drill bit Face, outer 21 outer circle top of drill bit setting, one circle step surface, outer 21 outer circle lower part of drill bit and lower end surface are inlaid with cutting tooth;Thrust axis It holds a15 to be mounted on outer 21 outer circle upper stage terrace of drill bit, thrust bearing b17 is mounted on outer 21 inner cavity middle bench face of drill bit On;Interior 20 lower part of drill bit is provided with jet hole connection inner hole and lower end surface, interior 20 lower end surface of drill bit are inlaid with cutting tooth, interior drill bit 20 outer circles are set as Step Shaft;Wearing bush 19 is mounted on interior 20 outer circle Step Shaft of drill bit, and wearing bush 19 is made of wear-resistant material.
As shown in Fig. 2, the gear in the middle part of 18 outer circle of transmission shaft is intermeshed with three governor gears 12 respectively.
A kind of working principle of large torque self-balancing low speed turbodrill of the present invention is: the tripping in present invention to shaft bottom, turn on pump Circulating fluid, outer turbo blade combination 5 and interior turbo blade combination 7 are acted on by opposite torque, outer turbo blade combination 5 Inner cylinder 6, step 9, transmission cylinder 11, outer drill bit 21 is driven to rotate, interior turbo blade combination 7 driving mandrel 8, transmission shaft 18, interior drill bit 20 rotates;Under the action of governor gear 12, interior drill bit 20 and outer drill bit 21 are reversely revolved according to fixed transmission ratio Turn, interior drill bit 20 and the reversed rock for cutting wellbore center and periphery, and cutting moment of torque autobalance respectively of outer drill bit 21.

Claims (2)

1. a kind of large torque self-balancing low speed turbodrill is by outer housing (1), self-aligning bearing a (2), nut (3), upper bearing (metal) Seat (4), outer turbo blade combination (5), inner cylinder (6), interior turbo blade combine (7), mandrel (8), step (9), aligning It is bearing b (10), transmission cylinder (11), governor gear (12), gear shaft (13), self-aligning bearing c (14), thrust bearing a (15), anti-lost End cap (16), thrust bearing b (17), transmission shaft (18), wearing bush (19), interior drill bit (20) and outer drill bit (21) are constituted;It is special Sign is: outer housing (1) upper end and upper drilling string screwed connection;Mandrel (8) outer circle top is set as Step Shaft, under mandrel (8) Portion is circumferentially uniformly arranged cavity space inside and outside three through-hole connections mandrel (8);Interior turbo blade combination (7) covers in mandrel (8) outer circle On upper step axis, nut (3) and mandrel (8) upper end screwed connection, nut (3) compress interior turbo blade combination (7);Outer turbine Blade combines (5) and is placed in inner cylinder (6) inner cavity, inner cylinder (6) upper end and top chock (4) lower end screwed connection, inner cylinder (6) Lower end and step (9) upper end screwed connection, top chock (4) and step (9) compress outer turbo blade combination (5); Self-aligning bearing a (2) is mounted on top chock (4) outer circle step surface, and self-aligning bearing b (10) is mounted on step (9) inner hole On step surface;Transmission shaft (18) upper end and mandrel (8) lower end screwed connection, terminal filament on transmission shaft (18) lower end and interior drill bit (20) Button connection;Gear is set as in the middle part of transmission shaft (18) outer circle;Transmission cylinder (11) upper end and step (9) lower end screwed connection, Transmission cylinder (11) lower end and outer drill bit (21) upper end screwed connection;One ring annular groove is set in the middle part of transmission cylinder (11) inner cavity, is passed Dynamic one circle step surface of cylinder (11) inner cavity top setting, one circle step surface of transmission cylinder (11) outer circle lower part setting, in transmission cylinder (11) Portion is circumferentially uniformly arranged three through-hole connection inner cavity upper stage terraces and outer circle lower stage terrace;Three gear shafts (13) are pacified respectively In three through-holes in the middle part of transmission cylinder (11), three governor gears (12) are separately mounted on three gear shafts (13), and three Governor gear (12) is in the annular groove in the middle part of transmission cylinder (11) inner cavity;Self-aligning bearing c (14) is mounted on transmission cylinder (11) On outer circle lower stage terrace;Anti-lost one circle raised step of end cap (16) inner cavity upper end setting, anti-lost end cap (16) and outer housing (1) Lower end screwed connection;One circle step surface of setting in the middle part of outer drill bit (21) inner cavity, outer one circle step of drill bit (21) outer circle top setting Face, outer drill bit (21) outer circle lower part and lower end surface are inlaid with cutting tooth;Thrust bearing a (15) is mounted in outer drill bit (21) outer circle On portion's step surface, thrust bearing b (17) is mounted on outer drill bit (21) inner cavity middle bench face;Interior drill bit (20) lower part is provided with Jet hole connection inner hole and lower end surface, interior drill bit (20) lower end surface are inlaid with cutting tooth, and interior drill bit (20) outer circle is set as step Axis;Wearing bush (19) is mounted on interior drill bit (20) outer circle Step Shaft, and wearing bush (19) is made of wear-resistant material.
2. large torque self-balancing low speed turbodrill according to claim 1, it is characterized in that: the transmission shaft (18) outer circle The gear at middle part is intermeshed with three governor gears (12) respectively.
CN201710554352.5A 2017-07-10 2017-07-10 A kind of large torque self-balancing low speed turbodrill Expired - Fee Related CN107152237B (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108266161B (en) * 2018-01-05 2020-11-06 马鞍山铭成科技信息咨询有限公司 Intelligent drilling device with automatic regulating function and high working efficiency
CN108278078B (en) * 2018-02-05 2020-01-24 中国石油大学(北京) Ultrasonic high-frequency impact drilling device
CN108194044A (en) * 2018-02-23 2018-06-22 中国石油天然气股份有限公司 Grind shoe
CN111997518A (en) * 2019-05-27 2020-11-27 奥瑞拓能源科技股份有限公司 Drilling tool with drill rod not subjected to force spinning
CN111364917B (en) * 2020-04-03 2021-05-25 西南石油大学 Drill bit for realizing axial impact function by utilizing turbine and gear

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2148857Y (en) * 1993-03-04 1993-12-08 石油大学(华东) Speed variator with single screw arbor
CN2202793Y (en) * 1994-05-10 1995-07-05 江汉石油学院 Closing type less gear difference speed reducer under well
US6110877A (en) * 1997-02-27 2000-08-29 Roberts; John W. Non-halogenated extreme pressure, antiwear lubricant additive
US6488103B1 (en) * 2001-01-03 2002-12-03 Gas Research Institute Drilling tool and method of using same

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