CN107299825B - A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit - Google Patents
A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit Download PDFInfo
- Publication number
- CN107299825B CN107299825B CN201710558964.1A CN201710558964A CN107299825B CN 107299825 B CN107299825 B CN 107299825B CN 201710558964 A CN201710558964 A CN 201710558964A CN 107299825 B CN107299825 B CN 107299825B
- Authority
- CN
- China
- Prior art keywords
- planet carrier
- output shaft
- sun gear
- face
- input shaft
- 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.)
- Active
Links
- 238000005553 drilling Methods 0.000 title claims abstract description 66
- 230000006698 induction Effects 0.000 title abstract description 6
- 230000002093 peripheral effect Effects 0.000 claims abstract description 37
- 244000309464 bull Species 0.000 claims description 31
- 230000007704 transition Effects 0.000 claims description 5
- 230000001939 inductive effect Effects 0.000 claims 7
- 238000005265 energy consumption Methods 0.000 abstract description 6
- 238000005520 cutting process Methods 0.000 description 13
- 238000000034 method Methods 0.000 description 11
- 238000005516 engineering process Methods 0.000 description 9
- 230000035939 shock Effects 0.000 description 9
- 230000033001 locomotion Effects 0.000 description 8
- 230000004044 response Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 7
- 238000013461 design Methods 0.000 description 6
- 239000012530 fluid Substances 0.000 description 6
- 239000011435 rock Substances 0.000 description 6
- 230000001360 synchronised effect Effects 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 3
- 239000003208 petroleum Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 241001074085 Scophthalmus aquosus Species 0.000 description 2
- 239000000872 buffer Substances 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000005381 potential energy Methods 0.000 description 2
- 238000003908 quality control method Methods 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 238000007514 turning Methods 0.000 description 2
- DNWOICFXGDPWDH-UDNLFYBJSA-N (4R,7S,10S,13S,16S,19S,22R,25S,28S,31S,34S,37R)-37-[[2-[[(2S)-2-[[(2S)-6-amino-2-[[(2S)-2-[[(2S)-2-[[(2S)-2-[[(2S)-1-[(2S)-2-[[(2S)-2-[[(2S)-2-[[(2S)-1-[(2S)-4-amino-2-[[(2S)-2-[[(2S)-4-amino-2-[[(2S)-2-[[(2S)-2-amino-3-hydroxypropanoyl]amino]propanoyl]amino]-4-oxobutanoyl]amino]-3-hydroxypropanoyl]amino]-4-oxobutanoyl]pyrrolidine-2-carbonyl]amino]propanoyl]amino]-4-methylpentanoyl]amino]propanoyl]pyrrolidine-2-carbonyl]amino]-5-carbamimidamidopentanoyl]amino]-4-carboxybutanoyl]amino]-5-carbamimidamidopentanoyl]amino]hexanoyl]amino]propanoyl]amino]acetyl]amino]-19,34-bis(4-aminobutyl)-31-(2-amino-2-oxoethyl)-25,28-dibenzyl-10,16-bis[(1R)-1-hydroxyethyl]-13-[(4-hydroxy-3-(125I)iodanylphenyl)methyl]-7-(hydroxymethyl)-22-(1H-indol-3-ylmethyl)-6,9,12,15,18,21,24,27,30,33,36-undecaoxo-1,2-dithia-5,8,11,14,17,20,23,26,29,32,35-undecazacyclooctatriacontane-4-carboxylic acid Chemical compound CC(C)C[C@H](NC(=O)[C@H](C)NC(=O)[C@@H]1CCCN1C(=O)[C@H](CC(N)=O)NC(=O)[C@H](CO)NC(=O)[C@H](CC(N)=O)NC(=O)[C@H](C)NC(=O)[C@@H](N)CO)C(=O)N[C@@H](C)C(=O)N1CCC[C@H]1C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H](CCC(O)=O)C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](C)C(=O)NCC(=O)N[C@H]1CSSC[C@H](NC(=O)[C@H](CO)NC(=O)[C@@H](NC(=O)[C@H](Cc2ccc(O)c([125I])c2)NC(=O)[C@@H](NC(=O)[C@H](CCCCN)NC(=O)[C@@H](Cc2c[nH]c3ccccc23)NC(=O)[C@H](Cc2ccccc2)NC(=O)[C@H](Cc2ccccc2)NC(=O)[C@H](CC(N)=O)NC(=O)[C@H](CCCCN)NC1=O)[C@@H](C)O)[C@@H](C)O)C(O)=O DNWOICFXGDPWDH-UDNLFYBJSA-N 0.000 description 1
- 108700014798 Leu(8)-Trp(22)-iodo-Tyr(25)- somatostatin 28 Proteins 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000001970 hydrokinetic effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 239000003129 oil well Substances 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000003442 weekly effect Effects 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B17/00—Drilling rods or pipes; Flexible drill strings; Kellies; Drill collars; Sucker rods; Cables; Casings; Tubings
- E21B17/02—Couplings; joints
- E21B17/04—Couplings; joints between rod or the like and bit or between rod and rod or the like
- E21B17/07—Telescoping joints for varying drill string lengths; Shock absorbers
- E21B17/076—Telescoping joints for varying drill string lengths; Shock absorbers between rod or pipe and drill bit
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B4/00—Drives for drilling, used in the borehole
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B4/00—Drives for drilling, used in the borehole
- E21B4/006—Mechanical motion converting means, e.g. reduction gearings
Landscapes
- 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)
- Retarders (AREA)
Abstract
A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit, planet carrier are sleeved on the external peripheral surface of sun gear input shaft, and small sliding bearing bush is sleeved on the circumferential surface of the sun gear input shaft;4 planetary gear shafts are evenly arranged on the surface of the planet carrier;8 planetary gears are divided into 2 groups, and make what 2 groups of planetary gears axially arranged to be sleeved in each planetary gear shaft, wherein first group of planetary gear inputs axis connection drill collar end close to the sun gear;First group of planetary gear end face is bonded with the inner face of sun gear input shaft one end step by end force bearing.Planet carrier output shaft is sleeved on the external peripheral surface of the sun gear input shaft, and is bonded the inner face of the planet carrier output shaft and the outer end face of the planet carrier.The present invention is completed in planet wheel decelerator structure basis, is had impact stable and continuous, durability guarantee, is guaranteed the characteristics of drilling eyelet quality and low energy consumption.
Description
Technical field
The present invention relates to field of oil drilling, a kind of equipment suitable for petroleum PDC drill bit drilling well.
Background technique
The stratum for meeting anisotropy or hard inclusions is often bored in Process of Oil Well Drilling, often causes the viscous of drilling system
Sliding, de- pressure, collapses phenomena such as tooth and breaking at bouncing of drilling tool, has seriously affected drilling progress, quality control.As modern industry automates
Deeply, the contradiction of drilling progress, the technical requirements of quality control and cost control becomes increasingly conspicuous, and there is an urgent need to one kind for technology development
Reliable, steady, efficient drilling technology equipment can be realized under harsh environments.
Application No. is a kind of shock absorbing type high frequency torsion impact device is disclosed in the innovation and creation of CN201610099208.2.It should
Impactor is mainly used in petroleum drilling technology field, in particular to a kind of shock absorbing type high frequency torsion impact device.Invention impact
The more other drilling tools of frequency at least promote 1 times, and the disc spring group for being installed in drilling tool bottom from drill string axial vibrations absorbs, Quan Mianbao
Protect the cutting tooth of PDC drill bit.
Application No. is a kind of gas drilling of gas drive liquid self-loopa is disclosed in the innovation and creation of CN201511028393.8
Helicoid hydraulic motor.The drilling tool is a kind of for air drilling brill directional well, horizontal well and high angle hole, is followed certainly using gas drive liquid
Ring is capable of the gas drilling helicoid hydraulic motor of steady output torque;It is total including sequentially connected motor assembly, universal shaft from top to bottom
At and driving-shaft assembly.The efficiency that the invention has steady output torque, extends drilling tool service life.
It is sliding that the document report SLTIT type torsional pulse drilling speed tool of " petroleum machinery " 2013.42 eliminates PDC drill bit card
Phenomenon improves bad ground rate of penetration.The tool is used cooperatively with PDC drill bit, forms a kind of new drilling engineering speed-raising skill
Art, while shortening drilling period, additionally it is possible to stablize drilling process, extend drill tool life.Using fluid dynamic theory, 3D
The method of production that Virtual Design technology is combined with experimental study, raise speed toolroom in test life > 150H.
" oil drilling technology " 2015.1 document reports three kinds of speed-raising technologies of current domestic and international application: hydraulic rotary-percussion respectively
Speed-raising tool, screw rod or turbine motor drilling tool and air drilling.
Above-mentioned drilling tool patented technology all has the application effect of preferable drilling speed, but needs slush pump or gas pump
Power is supported, and one side energy consumption is larger;On the other hand it is not applicable drilling unable to do what one wishes or without fluid circulation to be crept into for deep-well.
Above-mentioned data in literature retrieval, has not seen the document report for not depending on hydrokinetic inertial confinement drilling apparatus.
Summary of the invention
To overcome dependence fluid circulation power existing in the prior art and the biggish deficiency of energy consumption, the invention proposes
A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit.
The present invention includes sun gear input shaft, inertia duplex gear ring, planetary gear, end force bearing, planet carrier output
Axis, planet carrier, planetary gear shaft, small sliding bearing bush and bull torsionspring.Wherein: the planet carrier is sleeved on the sun gear
The external peripheral surface of input shaft, small sliding bearing bush are sleeved on the circumferential surface of the sun gear input shaft;4 planetary gear shafts are uniformly distributed
On the surface of the planet carrier;8 planetary gears are divided into 2 groups, and being sleeved on of making that 2 groups of planetary gears axially arrange is described
In each planetary gear shaft, wherein first group of planetary gear inputs axis connection drill collar end close to the sun gear;First group of row
The end face of star gear is bonded with the inner face of sun gear input shaft one end step by end force bearing.
The planet carrier output shaft is sleeved on the external peripheral surface of the sun gear input shaft, and makes the planet carrier output shaft
Inner face be bonded with the outer end face of the planet carrier.
One end of the inertia duplex gear ring is sleeved on the external peripheral surface of sun gear input axis connection drill collar one end,
The other end of the inertia duplex gear ring is sleeved on the external peripheral surface of the planet carrier output shaft, and makes in the inertia duplex gear ring
It is engaged between the inner surface in portion and the planetary gear external peripheral surface;The inner surface and sun gear of the inertia duplex gear ring
Intracavitary Zhou You great sliding bearing bush between the outer surface of input shaft.
The bull torsionspring is the bull torsionspring that elasticity involves constraint, which is sleeved on described
The external peripheral surface of planet carrier output shaft is stated, and makes the inner face of the bull torsionspring and the outer end of the inertia duplex gear ring
Face is chimeric, and the end face of the outer end of the bull torsionspring is solid by the outer end end face of fixing bolt and the planet carrier output shaft
Tightly.
The external peripheral surface of one end of the sun gear input shaft is isometrical section, and the external peripheral surface of the other end is multistage
Step-like, the circumferential surface of first order step therein is first group of planetary gear matching surface, the circumference of second level step
Surface is the mounting surface of end force bearing, and the circumferential surface of third level step is the mounting surface of inertia duplex gear ring, and
The circumferential surface of the third level step has the boss of radially protruding, the axially position for the inertia duplex gear ring.It is described too
The outer diameter that sun takes turns isometrical section of input shaft is identical as the internal diameter of planet carrier, and makes isometrical section of the sun gear input shaft and the first order
The end face of step difference becomes the axial locating surface of the planet carrier between ledge surface;The outer diameter and the row of the third level step
The maximum outside diameter of carrier output shaft is identical.
The end face of the planet carrier output shaft inner end is evenly equipped with the pin hole for installing the planet carrier.Planet carrier output
The inner surface of axis outer end is the flank for connecting drill bit.The inner surface of the planet carrier output shaft inner end is isometrical section, this etc.
The internal diameter of diameter section is identical as the outer diameter of the sun gear input shaft, and the planet carrier output shaft and the sun gear is made to input shaft clearance
Cooperation.The internal diameter in planet carrier output shaft inner surface middle section is identical as the assembly outer diameter of nut, exports the planet carrier
Axis and the assembly nut clearance fit.The outer surface diameter in the planet carrier middle section is minimum, and the appearance in the middle section and both ends
Face forms the cooperation of the planet carrier output shaft outer surface Yu bull torsionspring inner surface in the middle section with chamfered transition
Gap, the deformation space as the bull torsionspring;The external peripheral surface of the planet carrier output shaft inner end is cascaded surface, is used for
The inertia duplex gear ring is installed.The bull torsionspring is sleeved on the external peripheral surface of planet carrier output shaft.
The planetary gear modulus is 1.0~5.0.
The inner circumferential surface axial alignment of the inertia duplex gear ring has 2 groups of straight-sided flanks engaged with the planetary gear.
The inner circumferential surface of described inertia duplex gear ring one end and the step surface on the excircle of sun gear input shaft one end cooperate, separately
The inner circumferential surface of one end and the step surface on planet carrier output shaft excircle cooperate.It is defeated in the inertia duplex gear ring and planet carrier
Shaft cooperates the end face of one end uniformly distributed fluted, for being fitting to connection with the end face of bull torsionspring.
It presses in the tail end of the sun gear input shaft equipped with assembly nut;The assembly nut is sleeved on the sun gear input
The external peripheral surface of axis, and in the sun gear input shaft external peripheral surface and planet carrier output shaft inner circumferential surface it
Between.
The planet carrier is hollow revolving body.Planetary gear mounting hole is evenly equipped on the shell of the planet carrier.Institute
State the uniformly distributed axis hole there are four for installing each planet carrier output shaft on the end face of planet carrier both ends;The axis hole is respectively and respectively
The both ends of the rectangular through-hole penetrate through, and keep the mutual corresponding through-hole being located on the end face of planet carrier both ends concentric.?
There is axially projecting annular convex platform at the inner edge of planet carrier one end end face, which is seam allowance.
The outer diameter of the planet carrier is less than the internal diameter of the inertia duplex gear ring, and the internal diameter of the planet carrier is more defeated than sun gear
Enter the big 3~8mm of outer diameter of axis.
The present invention is completed in planet wheel decelerator structure basis.Structure of the invention is made of five parts: first
Part is assembling planet carrier output block: eight planetary gears are fixed on planet carrier output shaft by 4 planetary gear shafts, are formed
Planet carrier output block;Second part is big sliding bearing bush to be filled on sun gear input shaft, and be set with the inertia that elasticity involves
Duplex gear ring guarantees that the inner ring end face of inertia duplex gear ring and big sliding bearing bush are in transition fit;Part III is in the sun
Small sliding bearing bush and end face bearing are installed on wheel input shaft, then load planet carrier between sun wheel shaft and inertia duplex gear ring
Output shaft assembly guarantees sun gear, planetary gear and the intermeshing of inline gear and small sliding bearing bush and carrier output shaft
The transition fit of component, and pass through the assembly nut check planet carrier output shaft component of sun gear input shaft end, also to install additional
Anti-withdrawing bolt ensures reliable lock;Part IV is the big sliding bearing bush in the carrier output shaft assembly installation other end, and outside
Portion's suit elasticity involves the bull torsionspring of constraint, so that its end involves slot and the elastic end for involving inertia duplex gear ring
Portion involves slot mutual cooperation, forms inertia torsion and involves mechanism;Part V is in bull torsionspring and planet carrier output shaft
The end of component cooperation, with the other end of 4 fixing screw constraint lock ingot bull torsionsprings, then Standard is completed.
Aiming at the problem that vibration of existing drilling system, bouncing of drilling tool and de- pressure, the present invention proposes that inertial confinement induces drilling side
Method.The present invention utilizes the impact vibration response theory of rotor dynamics inertial load, a kind of inertial confinement that repeat is realized
Induce drilling method.The principle of the invention is to discharge the freedom degree constraint of rotor inertia constraint induction, the design of replacement system statics
Method matches independent inertial confinement circumferential direction change impacts vibratory response, alleviates the drilling body that drill bit creeps into the card that is hampered
Be wave motion response, stablize drilling system basic machining condition, realize continuous-stable drilling method, for drill deeply, deep hole
Processing and high-efficient cutting provide a kind of method of completely new inertial confinement induction drilling.
Compared with prior art, the present invention has the characteristics that 5:
1) it impacts stable and continuous: alleviating drill bit and be hampered shock motion, inhibit to eliminate the vibration of drill string system from source;It is hampered
Resistance is timely responded to brokenly, drilling is avoided to be interrupted, ensures that cutting is continuous;
Drill bit, which is hampered, generates the side knock wave of torsional shear, and is communicated up torsional pulse cross by inertia planet carrier 9
Wave, and resolve into three tunnels and be communicated up.First via shock wave decomposes Partial Shear shock wave by torsionspring 12, but by turning round
Turning the flexible of spring reduces the peak value buffering of shearing impact wave;Second tunnel and third road shock wave pass through respectively planetary gear 8 and
Sun gear 1 decomposes impulsive torque by transmission ratio, and wherein most impulsive torque is transmitted in inertia duplex outer gear ring 4, only small
Part torsional impact wave is transmitted on drilling rod alleviates shock motion significantly, it is suppressed that drill string system vibratory impulse in response to belt is come
Oscillating movement, reduce drill vibration.
Simultaneously when drilling starts bit cutting, before drill bit does not reach the cutting moment of torque, the torque that sun gear 1 inputs is first
It is stored in the form of potential energy in torsionspring 12.When drill bit reaches the cutting moment of torque, apparatus of the present invention and drill bit synchronous rotary
Drilling, drilling have just begun with progress.Once drill bit is hampered in drilling process, the inertia duplex outer gear ring 4 of synchronous rotation is relied on
Inertia discharges section store potential energy, and moment is added on drill bit, accordingly provides additional broken rock torque, while its velocity of rotation
It is corresponding to reduce.Additional broken rock torque and the size of deceleration provided by the present apparatus depend on the size being hampered, and be hampered big release energy
Amount is more, slows down big, vice versa.Energy after drill bit broken rock discharges suddenly, and drill bit can show rotation and accelerate to advance by leaps and bounds;Slow down simultaneously
Inertia duplex outer gear ring 4 also synchronous require to accelerate the original drilling velocity of rotation that follows up;It as a result is exactly the energy discharged after broken rock
Amount is redistributed, and drill bit acceleration, which is advanced by leaps and bounds, to be slowed down, and inertia duplex outer gear ring 4 is synchronous with coming up.The alternate stress that such drill bit is subject to
Reduce, complete the cutting circulation of a wheel shock response, the cycle period that drill bit continuously buffers is formed, and the item of continuous cutting is formed
Part.
2) durability guarantee: structure slows down the alternate stress that drill bit is subject to, and ensures drill bit fatigue life.
It is horizontal that rock cutting needs drill bit to undertake certain loading stress, but if the fluctuation of this loading stress is excessive,
Damage drill bit will be easier by fluctuating shock loading;If drill bit bit pressure and kinetic stability are good in continuous drilling, drill bit is cut
The fluctuation for cutting mean stress is small, that is, the stress ratio of alternation fluctuating load is small.The present invention by above-mentioned buffer shock-absorbing system,
Can effectively control the stress fluctuation amplitude of alternating load, the impact of cushioned drill bit inertial oscillation, reduce the broken resistance of drill bit advance by leaps and bounds with
And the impact velocity that is hampered, realize the durability guarantee of drilling life of bit.
3) hole quality guarantees: continuous and stable Drilling bore bit is not swung, and eye diameter is secure, the smooth rule of eyelet;
Just because of above-mentioned buffering and reason, drilling rod wave motion response is small and bit cutting is continuous, and drilling rod is not easy
The kinetic stability problem of brill is now put, drill bit only has the cutting movement of rotation, and the rare revolution motion for swinging drilling then creeps into hole
The amplification degree of eye diameter is just guaranteed.The drill bit movement track stable and continuous of cutting simultaneously, so drilling eyelet relative smooth rule
Then.
4) economy: without extra power demand, no displacement requirements do not flog a dead horse, low energy consumption;
Relative to both at home and abroad using fluid displacement come the patent of invention of assisted machining, such as the Tork Buster of Atlas
The technologies such as drilling tool and screw pump combined drilling are rushed with domestic torsion, necessarily will increase well head under same mud displacement
The consumption of mud plunger pump load bring energy consumption.Apparatus of the present invention are without fluid dynamic demand, also unlike Atlas Tork
Buster active attack rock is only to be cut after being hampered by dynamic response.Apparatus of the present invention do not consume fluid dynamic, also not blindly
The power of drill string conduction is consumed, then energy consumption reduces naturally.
5) novelty: conventional static design concept, the realization technology of applied dynamics design principle are broken through.
The design principle of apparatus of the present invention is the design concept from dynamics, is related to rotation, speed, vibration, punching
It hits, frequency response, advance by leaps and bounds and the concept of time such as sluggishness.Not only theory structure is peculiar, dynamic design method and bump vibration
Concept is also novel.
Detailed description of the invention
Fig. 1 is the inertial confinement drilling apparatus structure chart with PDC drill bit, wherein 1a is main view, and 1b is the A-A of 1a
Direction view;
Fig. 2 is sun gear input shaft structure schematic diagram, wherein 2a is main view, and 2b is right view;
Fig. 3 is planet carrier output shaft structural schematic diagram, wherein 3a is left view, and 3b is main view;
Fig. 4 is planetary gear construction schematic diagram, wherein 4a is left view, and 4b is main view, and 4c is axonometric drawing;
Fig. 5 is planetary gear shaft structural schematic diagram, wherein 5a is left view, and 5b is main view;
Fig. 6 is inertia duplex gear ring structure schematic diagram, wherein 6a is main view, and 6b is right view, and 6c is axonometric drawing;
Fig. 7 is planet carrier structure schematic diagram, and 7a is main view, and 7b is right view, and 7c is axonometric drawing;
Fig. 8 is bull torsion-spring structure schematic diagram, and 8a is main view, and 8b is the cross-sectional view of 8a.In figure:
1. sun gear input shaft;2. big sliding bearing bush;3. end force bearing;4. inertia duplex gear ring;5. planetary gear;
6. planet carrier;7. planetary gear shaft;8. small sliding bearing bush;9. planet carrier output shaft;10. assembling nut;11. Anti-withdrawing bolt;12.
Bull torsionspring;13. fixing bolt.
Specific embodiment
The present embodiment is a kind of inertial confinement drilling apparatus of adjoint PDC drill bit, including sun wheel input shaft 1, inertia duplex
Gear ring 4, planetary gear 5, end force bearing 3, planet carrier output shaft 6, planetary gear shaft 7, small sliding bearing bush 8 and bull torsion
Spring 12.
Wherein: the planet carrier 6 is sleeved on the external peripheral surface of the sun gear input shaft 1, and 4 planetary gear shafts 7 are equal
Cloth is on the surface of the planet carrier;8 planetary gears 5 are divided into 2 groups, and make what 2 groups of planetary gears axially arranged to be sleeved on
In each planetary gear shaft, wherein first group of planetary gear inputs axis connection drill collar end close to the sun gear;Described first
Group planetary gear end face is bonded with the inner face of sun gear input shaft one end step by end force bearing 3.
The planet carrier output shaft 9 is sleeved on the external peripheral surface of the sun gear input shaft 1, and exports the planet carrier
The inner face of axis is bonded with the outer end face of the planet carrier.Small sliding bearing bush 1 is sleeved on the circumference table of the sun gear input shaft 1
Face;Assembly nut 10 is located at the tail end of the sun gear input shaft, is sleeved on the external peripheral surface of the sun gear input shaft, and locate
Between the external peripheral surface of the sun gear input shaft and the inner circumferential surface of planet carrier output shaft 9.The assembly nut with
The end face of sun gear input shaft 1, which is matched, is drilled with Anti-withdrawing bolt 11.
One end of the inertia duplex gear ring 4 is sleeved on the outer circle weekly form of sun gear input axis connection drill collar one end
Face, the other end of the inertia duplex gear ring are sleeved on the external peripheral surface of the planet carrier output shaft 9, and make the inertia duplex-gear
It encloses between the inner surface and the external peripheral surface of the planetary gear 5 at middle part and engages;The inner surface of the inertia duplex gear ring with
Intracavitary Zhou You great sliding bearing bush 2 between the outer surface of sun gear input shaft 1.
The bull torsionspring 12 is the bull torsionspring that elasticity involves constraint, which is sleeved on
The external peripheral surface for stating planet carrier output shaft 9, and make the inner face and the inertia duplex gear ring 4 of the bull torsionspring
Outer end face it is chimeric, the end face of the outer end of the bull torsionspring is outer by fixing bolt 13 and the planet carrier output shaft 9
End face is held to fasten.
The sun gear input shaft 1 is hollow shaft.The external peripheral surface of one end of the sun gear input shaft is isometrical section, separately
The external peripheral surface of one end is the step-like of multistage, and the circumferential surface of first order step therein is that first group of planetary gear is matched
Surface is closed, the circumferential surface of second level step is the mounting surface of end force bearing, and the circumferential surface of third level step is inertia
The mounting surface of duplex gear ring 4, and have the boss of radially protruding in the circumferential surface of the third level step, it is double for the inertia
Join the axially position of gear ring.The outer diameter of isometrical section of the sun gear input shaft is identical as the internal diameter of planet carrier 6, and makes the sun gear
The end face of step difference becomes the axial locating surface of the planet carrier 6 between isometrical section of input shaft and the first order ledge surface;Institute
The outer diameter for stating third level step is identical as the maximum outside diameter of the planet carrier output shaft 9.
The planet carrier output shaft 9 is hollow revolving body.The end face of the planet carrier output shaft inner end is evenly equipped with pin hole, is used for
The planet carrier 6 is installed.The inner surface of the planet carrier output shaft outer end is the flank for connecting drill bit.Planet carrier output
The inner surface of axis inner end is isometrical section, and isometrical section of the internal diameter is identical as the outer diameter of the sun gear input shaft 1, makes the planet carrier
Output shaft and the sun gear input shaft clearance fit.The internal diameter in the 9 inner surface middle section of planet carrier output shaft and the assembly
The outer diameter of nut 10 is identical, makes the planet carrier output shaft and the assembly nut clearance fit.The outer surface in the planet carrier middle section
Diameter is minimum, and the outer surface at the middle section and both ends forms the planet carrier output shaft in the middle section with chamfered transition
The fit clearance of outer surface and 12 inner surface of bull torsionspring, the deformation space as the bull torsionspring;The planet carrier
The external peripheral surface of output shaft inner end is cascaded surface, for installing the inertia duplex gear ring 4.The bull torsionspring suit
In the external peripheral surface of planet carrier output shaft.
The planetary gear 5 is standard spur gear.The planetary gear modulus is 1.0~5.0.In the present embodiment, the row
The modulus of star gear is 2.0.
The inertia duplex gear ring 4 is hollow revolving body.The inner circumferential surface axial alignment of the inertia duplex gear ring has 2 groups
The straight-sided flank engaged with the planetary gear.The inner circumferential surface and the sun gear input shaft of described inertia duplex gear ring one end
Step surface cooperation on 1 one end excircle, inner circumferential surface and the step surface on 9 excircle of planet carrier output shaft of the other end are matched
It closes.Cooperate the end face of one end uniformly distributed fluted in the inertia duplex gear ring and planet carrier output shaft, is used for and bull torsionspring
12 end face is fitting to connection.
The planet carrier 6 is hollow revolving body.Uniformly distributed there are four rectangular through-hole on the shell of the planet carrier, the rectangle is logical
Hole is planetary gear mounting hole.Uniformly distributed on the end face of the planet carrier both ends there are four axis holes, defeated for installing each planet carrier
Shaft 9;The axis hole is penetrated through with the both ends of each rectangular through-hole respectively, and makes to be located at planet carrier both ends end face
On mutual corresponding through-hole it is concentric.There is axially projecting annular convex platform at the inner edge of planet carrier one end end face, the boss
For seam allowance.
The outer diameter of the planet carrier is less than the internal diameter of the inertia duplex gear ring 4, and the internal diameter of the planet carrier compares sun gear
Big 3~the 8mm of the outer diameter of input shaft 1.
Claims (8)
1. a kind of inertial confinement of adjoint PDC drill bit induces drilling apparatus, which is characterized in that including sun gear input shaft, inertia
Duplex gear ring, planetary gear, end force bearing, planet carrier output shaft, planet carrier, planetary gear shaft, small sliding bearing bush and more
Head torsionspring;Wherein: the planet carrier is sleeved on the external peripheral surface of the sun gear input shaft, and small sliding bearing bush is sleeved on
The circumferential surface of the sun gear input shaft;4 planetary gear shafts are evenly arranged on the surface of the planet carrier;8 planetary gears are divided into 2
Group, and make what 2 groups of planetary gears axially arranged to be sleeved in each planetary gear shaft, wherein first group of planetary gear leans on
The nearly sun gear inputs axis connection drill collar end;First group of planetary gear end face and one end stand of sun gear input shaft
The inner face of rank is bonded by end force bearing;
The planet carrier output shaft is sleeved on the external peripheral surface of the sun gear input shaft, and makes the interior of the planet carrier output shaft
End face is bonded with the outer end face of the planet carrier;
One end of the inertia duplex gear ring is sleeved on the external peripheral surface of sun gear input axis connection drill collar one end, this is used
The other end of property duplex gear ring is sleeved on the external peripheral surface of the planet carrier output shaft, and makes in the middle part of the inertia duplex gear ring
It is engaged between inner surface and the planetary gear external peripheral surface;The inner surface and sun gear of the inertia duplex gear ring input
Intracavitary Zhou You great sliding bearing bush between the outer surface of axis;
The bull torsionspring is that elasticity involves the bull torsionspring of constraint, which, which is sleeved on, described states row
The external peripheral surface of carrier output shaft, and keep the inner face of the bull torsionspring and the outer end face of the inertia duplex gear ring embedding
It closes, the end face of the outer end of the bull torsionspring is fastened by the outer end end face of fixing bolt and the planet carrier output shaft.
2. inducing drilling apparatus with the inertial confinement of PDC drill bit as described in claim 1, which is characterized in that the sun gear
The external peripheral surface of one end of input shaft is isometrical section, the external peripheral surface of the other end be it is multistage step-like, therein first
The circumferential surface of grade step is first group of planetary gear matching surface, and the circumferential surface of second level step is end force bearing
Mounting surface, the circumferential surface of third level step is the mounting surface of inertia duplex gear ring, and in the circle of the third level step
Perimeter surface has the boss of radially protruding, the axially position for the inertia duplex gear ring;Isometrical section of the sun gear input shaft
Outer diameter is identical as the internal diameter of planet carrier, and makes step difference between isometrical section of the sun gear input shaft and the first order ledge surface
End face become the planet carrier axial locating surface;The outer diameter of the third level step and the maximum of the planet carrier output shaft are outer
Diameter is identical.
3. inducing drilling apparatus with the inertial confinement of PDC drill bit as described in claim 1, which is characterized in that the planet carrier
The end face of output shaft inner end is evenly equipped with the pin hole for installing the planet carrier;The inner surface of the planet carrier output shaft outer end is to use
In the flank of connection drill bit;The inner surface of the planet carrier output shaft inner end be isometrical section, isometrical section of the internal diameter and it is described too
The outer diameter of sun wheel input shaft is identical, makes the planet carrier output shaft and the sun gear input shaft clearance fit;The planet carrier is defeated
The internal diameter in shaft inner surface middle section is identical as the assembly outer diameter of nut, matches the planet carrier output shaft with the assembly nut gap
It closes;The outer surface diameter in the planet carrier middle section is minimum, and the outer surface at the middle section and both ends is with chamfered transition, in the middle section
The fit clearance for foring the planet carrier output shaft outer surface Yu bull torsionspring inner surface, as the bull torsionspring
Deformation space;The external peripheral surface of the planet carrier output shaft inner end is cascaded surface, for installing the inertia duplex gear ring;Institute
State the external peripheral surface that bull torsionspring is sleeved on planet carrier output shaft.
4. inducing drilling apparatus with the inertial confinement of PDC drill bit as described in claim 1, which is characterized in that the planet tooth
The modulus of wheel is 1.0~5.0.
5. inducing drilling apparatus with the inertial confinement of PDC drill bit as described in claim 1, which is characterized in that the inertia is double
The inner circumferential surface axial alignment of connection gear ring has 2 groups of straight-sided flanks engaged with the planetary gear;The inertia duplex gear ring one
Step surface on the inner circumferential surface at end and sun gear input shaft one end excircle cooperates, the inner circumferential surface of the other end with
Step surface cooperation on planet carrier output shaft excircle;Cooperate the end face of one end in the inertia duplex gear ring and planet carrier output shaft
It is uniformly distributed fluted, for being fitting to connection with the end face of bull torsionspring.
6. inducing drilling apparatus with the inertial confinement of PDC drill bit as described in claim 1, which is characterized in that in the sun
The tail end for taking turns input shaft is pressed equipped with assembly nut;The assembly nut is sleeved on the external peripheral surface of the sun gear input shaft, and
External peripheral surface in the sun gear input shaft and between the inner circumferential surface of planet carrier output shaft.
7. inducing drilling apparatus with the inertial confinement of PDC drill bit as described in claim 1, which is characterized in that the planet carrier
For hollow revolving body;Planetary gear mounting hole is evenly equipped on the shell of the planet carrier;On the end face of the planet carrier both ends
The uniformly distributed axis hole there are four for installing each planet carrier output shaft;Both ends of the axis hole respectively with each rectangular through-hole are passed through
It is logical, and keep the mutual corresponding through-hole being located on the end face of planet carrier both ends concentric;In the inner edge of planet carrier one end end face
There is axially projecting annular convex platform at place, which is seam allowance.
8. inducing drilling apparatus with the inertial confinement of PDC drill bit as claimed in claim 7, which is characterized in that the planet carrier
Outer diameter be less than the internal diameter of the inertia duplex gear ring, the internal diameter of the planet carrier is bigger than the outer diameter of sun gear input shaft by 3~
8mm。
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710558964.1A CN107299825B (en) | 2017-07-11 | 2017-07-11 | A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit |
US16/629,894 US11306537B2 (en) | 2017-07-11 | 2018-07-09 | Induced drilling method for inertia constrained implicated motion and inertial constraint induced drilling device |
PCT/CN2018/094949 WO2019011202A1 (en) | 2017-07-11 | 2018-07-09 | Method for induced drilling by means of inertial confinement motion traction, and inertial confinement induced drilling device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710558964.1A CN107299825B (en) | 2017-07-11 | 2017-07-11 | A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit |
Publications (2)
Publication Number | Publication Date |
---|---|
CN107299825A CN107299825A (en) | 2017-10-27 |
CN107299825B true CN107299825B (en) | 2019-01-04 |
Family
ID=60132751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710558964.1A Active CN107299825B (en) | 2017-07-11 | 2017-07-11 | A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107299825B (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11306537B2 (en) | 2017-07-11 | 2022-04-19 | Xi'an Manyuan Electromechanical Equipment Co., Ltd. | Induced drilling method for inertia constrained implicated motion and inertial constraint induced drilling device |
CN109750977A (en) * | 2017-11-01 | 2019-05-14 | 陈晓新 | A kind of New well drilling torque increase square, which disappears, to quiver except vibratory tool |
CN108108779B (en) * | 2017-11-29 | 2021-03-09 | 中国石油天然气集团公司 | Data storage method, device and system for hydraulic spinning tool |
CN109931000B (en) * | 2019-04-23 | 2020-07-24 | 西南石油大学 | Adjustable jet oscillation PDC drill bit |
CN110919870B (en) * | 2019-11-11 | 2020-11-06 | 东阳市琰安建筑工程有限公司 | Device for forming arc-shaped hanging groove on end face of stone plate for architectural decoration |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001098619A2 (en) * | 2000-06-17 | 2001-12-27 | Weir Group Investments Limited | Drive system |
US7464750B2 (en) * | 2006-01-06 | 2008-12-16 | Bal Seal Engineering Co., Inc. | Rotary fluid-sealing structure using speed-reduction stages |
CN201461894U (en) * | 2009-08-14 | 2010-05-12 | 卫华集团有限公司 | Planetary gear transmission differential |
CN203925277U (en) * | 2014-06-16 | 2014-11-05 | 江苏航天鸿鹏数控机械有限公司 | A kind of adjusting microinching formula drilling well helicoid hydraulic motor |
CN205977090U (en) * | 2016-08-29 | 2017-02-22 | 盐城市荣嘉机械制造有限公司 | High -efficient anti screw rod drilling tool that dashes |
CN206035378U (en) * | 2016-08-29 | 2017-03-22 | 盐城市荣嘉机械制造有限公司 | Screw drilling tool |
-
2017
- 2017-07-11 CN CN201710558964.1A patent/CN107299825B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001098619A2 (en) * | 2000-06-17 | 2001-12-27 | Weir Group Investments Limited | Drive system |
US7464750B2 (en) * | 2006-01-06 | 2008-12-16 | Bal Seal Engineering Co., Inc. | Rotary fluid-sealing structure using speed-reduction stages |
CN201461894U (en) * | 2009-08-14 | 2010-05-12 | 卫华集团有限公司 | Planetary gear transmission differential |
CN203925277U (en) * | 2014-06-16 | 2014-11-05 | 江苏航天鸿鹏数控机械有限公司 | A kind of adjusting microinching formula drilling well helicoid hydraulic motor |
CN205977090U (en) * | 2016-08-29 | 2017-02-22 | 盐城市荣嘉机械制造有限公司 | High -efficient anti screw rod drilling tool that dashes |
CN206035378U (en) * | 2016-08-29 | 2017-03-22 | 盐城市荣嘉机械制造有限公司 | Screw drilling tool |
Non-Patent Citations (2)
Title |
---|
PDC钻头扭矩控制技术分析;韩飞等;《石油矿场机械》;20121231;第41卷(第12期);第69-71页 |
行星式PDC钻头驱动器研制;何超等;《石油钻采工艺》;20101231;第32卷;第73-75页 |
Also Published As
Publication number | Publication date |
---|---|
CN107299825A (en) | 2017-10-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN107299825B (en) | A kind of inertial confinement induction drilling apparatus of adjoint PDC drill bit | |
CN105927147B (en) | A kind of percussion drilling speed-raising tool and method | |
CN201554363U (en) | Turbine type torsion impact drilling tool for hard formation | |
CN104499941B (en) | Method of longitudinal vibration of drilling string is converted into the device of drill bit torsional pulse | |
US11306537B2 (en) | Induced drilling method for inertia constrained implicated motion and inertial constraint induced drilling device | |
CN103321569A (en) | Cam type high-frequency percussion well drilling tool | |
CN101624898B (en) | Rock-entering vibrating device for rotary drilling machine | |
CN102705140A (en) | Drilling power tool, drilling tool and drilling method for forming boreholes | |
CN101652563A (en) | A wind turbine comprising a torsional vibration absorber | |
CN103375133A (en) | Down-hole displacement percussion drilling tool | |
CN108798503A (en) | Screw circumferential direction percussion drilling tool | |
CN108625769A (en) | Torsional pulse drilling speed tool | |
CN109098654A (en) | A kind of mechanical axial-rotation percussion drilling tool based on helicoid hydraulic motor | |
CN205558849U (en) | Utilize turbine to produce downhole tool of shock oscillation | |
CN201474610U (en) | Injection rock excitation device of rotary drilling rig | |
CN202926511U (en) | Drilling power tool and novel drilling tool | |
CN202157745U (en) | Screw drilling tool transmission shaft assembly with vibration reduction function | |
CN203412971U (en) | Connecting structure between speed reducer and motor | |
CN204326969U (en) | Method of longitudinal vibration of drilling string is converted into the device of drill bit torsional pulse | |
CN101893081A (en) | Driven gear of engine balance shaft | |
CN106320984B (en) | The drilling tool of axial impact is realized using vortex-induced vibration | |
CN208669203U (en) | Screw circumferential direction percussion drilling tool | |
CN203488681U (en) | Independent vibration damping structure of gearbox | |
CN211950338U (en) | Low-energy-consumption hydraulic oscillator | |
CN204920776U (en) | Drill bit hydraulic pulse impacter |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |