Hindawi Publishing Corporation Mathematical Problems in Engineering Volume 2015, Article ID 153648, 34 pages http://dx.doi.org/10.1155/2015/153648 Research Article Research on the Hard-Rock Breaking Mechanism of Hydraulic Drilling Impact Tunneling RishengLong,1,2ShaoniSun,3andZishengLian1,2 1CollegeofMechanicalEngineering,TaiyuanUniversityofTechnology,Taiyuan,Shanxi030024,China 2ShanxiKeyLaboratoryofFullyMechanizedCoalMiningEquipment,Taiyuan,Shanxi030024,China 3SchoolofMechanicalEngineeringandAutomation,NortheasternUniversity,Shenyang,Liaoning110004,China CorrespondenceshouldbeaddressedtoRishengLong;[email protected] Received19May2015;Revised21July2015;Accepted26July2015 AcademicEditor:FrancescoFranco Copyright©2015RishengLongetal.ThisisanopenaccessarticledistributedundertheCreativeCommonsAttributionLicense, whichpermitsunrestricteduse,distribution,andreproductioninanymedium,providedtheoriginalworkisproperlycited. Inordertorealizetherapidhard-rocktunnelinginasafe,highlyeffective,andeconomicmanner,thehydraulicdrillingimpact hard-rocktunneling(HDIHT)technologyandmethodwereintroducedbasedonthetheoriesofrockmechanicsandhydraulic impact.Thekeyparameters,includingdrillingradiusandimpactdistance,wereresearchedtorevealthestressbehaviorduring HDIHTprocess.TheVonMisesequivalentstressanditsprincipalstresscomponentswereanalyzed,andthebreakingmechanism ofHDIHTwasalsodiscussed.Thesimulationresultsshowthat,toensuretheeffectivenessof“secondarybreaking”causedby drillingholefreesurfaces,theimpactdistanceshouldnotexceed200mm,andtheoptimaldrillingradiuswasabout35mm. 1.Introduction on the theories of rock mechanics, when hammer impacts hard rock directly, its impact energy will be converted into Hard-rock rapid tunneling, especially for the rock whose the compressive wave in the depths of rock at the impact hardnessexceedsf10(rockPlattsruggednesscoefficient),isa moment,andabrokenpitisformedinstantly.Ifsomeholes worldwidetechnicalissue,whetherforundergroundtunnel- existedinworkingface,thecompressiveimpactwavewillbe ing or construction. So far, drill and blast tunneling (DBT) transformedintothetensilestressafterthereflectionatfree and heavy-duty roadheader are still the main methods for surfaces. Owing to the fact that the tensile strength of rock hard-rocktunnelingincoalmine.However,lotsofauxiliary is only three to five percent of its compressive strength, the equipmentandpersonsneededatworkingface,greatdamage rockneartheholesmaybebrokenagainunderthesecondary tothesurroundingrocks,andovertunnelingandinsufficient breaking effect of “compression-tension” transformation [1, tunneling of final sections are the major problems of DBT 2].Thus,intheproposedHDIHTprocess,manyholesshould method. Heavy-duty roadheader also has its disadvantages bedrilledinadvancetoincreasefreesurfacearea,andthen whichareasfollows:lowereconomiccuttinghardness(≤f8), a hydraulic breaker with large impact energy was used to nethermoretunnelingefficiency,highercutterconsumption impactandcrushhardrockdirectly. rate, and so forth. Although the hard-rock tunnels (≥f10) Manynumericalsimulationmethods,includingmechan- are not more than 5 percent of the general amount of ics of continuous medium (MCM), mechanics of noncon- annualtunneling,itisstillacrucialrestrictionfactorforthe tinuous medium (MNCM), and coupling analysis of con- highly efficient production and management of coal mine. tinuous discrete (CACD), have been conducted to reveal Therefore,itisurgenttoseekanovel,safe,andhighlyeffective the breaking and failure behavior of brittle rock. In 1995, approach(includingtheories,technology,andequipment)for Munjiza et al. [3, 4] introduced the damage mechanics and thehard-rockrapidtunneling,withnoexplosion. fracture mechanics into the finite element method (FEM) Hydraulicdrillingimpacthard-rocktunneling(HDIHT) andproposedthecombinedfinite-discreteelementmethod maybe just thepotentialmethodwe arelookingfor. Based (CF/DEM)tosimulatethebrittlefractureandfailure.Based 2 MathematicalProblemsinEngineering P 2𝜃 h i h i+1 𝜓 L 𝜃 T 𝜓 R N Figure1:Sketchoftherockintrusionprocessofwedgeshapedblade. a mechanism of HDIHT method and technology have never ) 3 −m beenreportedyet. ·mc In this work, based on the relevant rock mechanics ·g theories and “element birth and death” technique, the key k k ( parameters, including drilling radius (dr) and impact dis- or w tance (di), were researched to explore the hard-rock stress c SZ fi behavior during HDIHT process through APDL program- ci pe a ming. The Von Mises equivalent stress and its principal g s 0 stresscomponentswereanalyzedindetail,andthebreaking elin TZ CZ mechanismofHDIHTwasalsodiscussed. his C 0 A0 Ac A Impact energy (kg·m) 2.TheoreticalAnalysisandCalculation Figure2:𝛼-𝐴curveduringimpactbreakingprocess. Onthebasisoftherelevanttheoriesofrockstaticintrusion [1, 2], Paul simplified the rock intrusion of wedge shaped blade into the sketch shown in Figure1. Suppose 𝑅 was the stress component of load 𝑃 along the vertical edge-surface on the MCM approach and deep understanding of rock’s direction; it could be decomposed into the shear force (𝑇) heterogeneity, Tang and his team [5–7] proposed a realistic failureprocessanalysismodel(RFPA2D,RFPA3D),whichhad andnormalforce(𝑁)ontheshearfracturesurface.Basedon Mohr-Coulombfailuretheory,whenshearstress𝜏exceeded beenwidelyusedaroundtheworld.Jingetal.[8]presented cohesion 𝐶 and internal friction 𝜇𝜎, shear-breaking would a numerical model for coupled hydromechanical processes occur.Thefailureconditionwasgivenby infracturedhardrocksusingthediscontinuousdeformation analysis (DDA) method, but their emphasis was placed on the physical behaviour of the coupled stress/deformation 𝜏−𝜇𝜎=𝐶. (1) and fluid flow interaction in rock fractures. Zhang et al. [9]usedamodifieddiscontinuousdeformationalgorithmto simulate the failure behavior of jointed rock. Using particle Assuming the load of the 𝑖th impact was 𝑃∗, the pene- 𝑖 simulationmethod,XiaandZhou[10]investigatedthefailure tration depth of the 𝑖th impact was 𝐻∗, and the edge angle 𝑖 process of brittle rock under triaxial compression through was 2𝜃 (see Figure1), there must be a relationship between bothexperimentalandnumericalapproaches.Basedonthe the(𝑖+1)thloadanditsstress: statisticalcontinuumdamagemechanicstheoryandthefinite element method (FEM), Li et al. [11] developed a statistical 𝑃∗ meso-damagemechanicalmethod(SMDMM)tomodelthe 𝑅= 𝑖+1 , transscale progressive failure process of rock. Furthermore, 2sin𝜃 many simulations were also carried out by Min and other ℎ∗ (2) researchers to study the failure process of brittle rock [12– 𝐿= 𝑖+1 , 18]. However, the researches about the hard-rock breaking sin𝜓 MathematicalProblemsinEngineering 3 Impact rod of hammer (length:1200mm) Rock (granite) 400mm 500mm 400mm di Symmetry planes Figure3:SketchofFEmodelusedinthesimulations. where 𝐿 was the length of shear plane and 𝜓 was the shear Equation(5)couldbefurtherwrittenas planeangle.Usingedgelengthastheunit,𝜏and𝜎couldbe 𝑃∗ 1 givenby 𝜏−𝜇𝜎= 𝑖+1 ⋅ [sin𝜓cos(𝜓+𝜃)cos𝜙 ℎ∗ 2sin𝜃cos𝜙 𝑖+1 𝑃∗ 𝜏= 𝑇 = 𝑅cos(𝜓+𝜃), (3) −sin𝜓sin(𝜓+𝜃)sin𝜙]= 2ℎ𝑖+∗1 (7) 𝐿 𝐿 𝑖+1 𝑁 𝑅 sin𝜓cos(𝜓+𝜃+𝜙) 𝜎= = sin(𝜓+𝜃). (4) ⋅ , 𝐿 𝐿 sin𝜃cos𝜙 where𝜏−𝜇𝜎wasafunctionof𝜓.Settingthefirstderivative Substituting (3) and (4) into (1), then (1) could be of(7)equalszero,itwaseasytobefoundthatwhen rewrittenas 𝜋 𝜃+𝜙 𝜓= − . (8) 4 2 𝑃∗ The value of 𝜏 − 𝜇𝜎 reached its maximum. Therefore, the 𝜏−𝜇𝜎= 𝑖+1 [sin𝜓cos(𝜓+𝜃) ℎ∗ 2sin𝜃 shear-breakingsurfacewouldfirstappearintheplaneofthe 𝑖+1 (5) slopeof𝜓.When𝜃+Φ < 90∘,shear-breakingmightoccur; −𝜇sin𝜓sin(𝜓+𝜃)]. while𝜃+Φ > 90∘,therockwasinafullycompressedstate; theleap-forwardinvasionwouldnothappen.Substituting(8) into(7),(7)couldbefinallywrittenas The internal friction angle 𝜙 was used to represent the 𝜏−𝜇𝜎 internalfrictioncoefficient;thatis, 𝑃∗ sin(𝜋/4−(𝜃+𝜙)/2)cos(𝜋/4+(𝜃+𝜙)/2) = 𝑖+1 (9) ℎ∗ 2sin𝜃cos𝜙 sin𝜙 𝑖+1 𝜇=𝑡𝑔𝜙= . (6) cos𝜙 =𝐶. 4 MathematicalProblemsinEngineering (a) (b) (a) dr=20mm,di=200mm (b) dr=20mm,di=250mm (c) (d) (c) dr=20mm,di=150mm (d) dr=35mm,di=200mm (e) (e) dr=50mm,di=200mm Figure4:ComparisonofdifferentFEmodels. Solvingtheaboveformula,theratioof𝑃∗ toℎ∗ could That is, the ratio of each impact’s load to its invasion 𝑖+1 𝑖+1 begivenby depthwasaconstant.Inaddition,accordingtothecorrelation 𝑃𝑖∗+1 = 4𝐶⋅sin𝜃⋅(1−sin𝜙) =𝐾. (10) btheetw𝛼e-e𝐴ncimurpvaectoefnimerpgyacatnbdrechakisienlginpgrsopceecsisficcowuoldrkb(eCdSiWvi,d𝛼e)d, ℎ𝑖∗+1 1−sin(𝜃+𝜙) into three zones, that is, scaring zone (SZ), transient zone MathematicalProblemsinEngineering 5 28 7 6 .. 27 . 3 2 26 1516 25 14 24 17 18 19 23 22 21 20 1 8 9 ···1213 Figure5:SketchofnodedistributioninFEmodel. m/s) 8.57 y ( cit ··· ··· o Vel 0 0.3 3 100 T (ms) Figure6:Velocity-timeloadingcurveofimpactrodinthesimulations. (TZ),andcrushedzone(CZ).Whenimpactenergywasquite 26kg⋅m⋅cm−3, the crushed granite volume of each impact small, the 𝛼-𝐴 curve would fallinto its left side, which was couldbecalculatedasfollows: SaZb.roInketnhipsitr,eagniodnt,htehderiompppaecdtrpoockweprowwdasertowoassmvearlylfitonefo,rfomr 𝑉 = 𝐴 = 7500(N⋅m) = 7500 m3 theCSWwasquitelarge.Theshadedregionin𝛼-𝐴curvewas break 𝛼 26(kg⋅m/cm3) 26×10/10−6 (12) TZ. In this domain, the impact breaking data and behavior =2.885×10−5m3. wereunpredictable.Asimpactenergywaslargerthan𝐴𝑐,the 𝛼-𝐴 curve would eventually enter a relatively stable region, Based on the crushed granite volume of each impact, if CZ. hammerimpactedafixedpointrepeatedly,thefinalradiusof Withregardtotherelationshipbetweenbrokenrockvol- brokenpit(𝑟pit)shouldmeetthefollowing: ume(𝑉break)andimpactenergy(𝐴),thefollowingempirical ℎ formulawaswidelyusedandexpressedasfollows[1]: 𝜋𝑟 2⋅ =2.885×10−5×𝑛 , pit 3 imp 𝑟 (13) 𝑉break =𝐶1(𝐴−𝐴0)𝑎, (11) ℎpit =0.375, pit where𝐴0 =0,𝑎=1,𝐶1 =1/𝛼,inunitsofkg−1⋅m−1⋅cm3. wdehpetrheo𝑛fimbprwokaesnthpeiti,mapnadct0t.3im75eswaatsaaficxoendsptaonint,t,dℎepciitdwedasatnhde Supposing the impact energy of hydraulic impact ham- given by the end-shape of impact rod. Therefore, in theory, meris7500J,roddiameter,150mm,andtheCSWofgranite, hydraulicimpacttunnelingwasfeasible. 6 MathematicalProblemsinEngineering 0 0.250E+07 0.750E+07 0.125E+08 a) P 0.175E+08g) ( v a 0.225E+08V ( Q 0.275E+08SE 0.325E+08 0.375E+08 0.400E+08 (a) The0.003ths (b) The0.203ths (c) The0.403ths 0 0.250E+07 0.750E+07 0.125E+08 a) P 0.175E+08g) ( v a 0.225E+08V ( Q 0.275E+08SE 0.325E+08 0.375E+08 0.400E+08 (d) The0.603ths (e) The0.803ths Figure7:TheVonMisesequivalentstresscontoursofmodelAatdifferenttime. 3.FiniteElementModelingandConfiguration and the “element birth and death” technique was realizedthroughAPDLprogramming. Takingthegranite,whosePlattsruggednesscoefficientvaried from f10 to f15, as the research object, the mechanical and (3)The compressive and shear strength were used as physicalpropertiesparameterswerelistedasfollows:elastic the failure criterion of granite elements. Program modulus,3.58×104MPa;Poisson’sratio,0.28;ratiooftensile could automatically calculates the stress status of each cell after one load step or substep. For the strengthtocompressivestrength,0.03.Foralmostallcrushed cells,whoseVonMisesequivalentstressexceededthe granite was powdery detritus in actual impact breaking compressiveorshearstrengthofgranite,theywould process,andtheobjectiveofthisworkwasmainlyfocusedon be deemed invalid and would be removed from the thestressvariationbehaviorofbrokenpit,drillingholes,and model immediately. In the meantime, system would theirsurroundingarea,thecrackgenerationandpropagation also automatically redefine the contact relationship ofgraniteduringHDIHTprocesswouldnotbeconsidered. betweenrod-endandbrokenpit. Thus,thefollowingassumptionscouldbemade: (4)Toconsidertheeffectofsurroundingrocksinactual (1)Basedonthecontinuoushomogeneousmediumthe- impactbreakingprocess,thesideandbottomsurfaces ory and the characteristics of granite, the isotropic ofFEmodelwereallsetastheunlimitedboundaries. bilinear kinematics hardening model was used. But thejointdevelopmentandtectonicchangesofgranite Themainparametersofhydraulichammerwerelistedin wasnottakenintoaccountinthesimulations. Table1. In order to reduce the computational workload, as (2)InvirtueofANSYS/LS-DYNAmodule,the“surfaceto depictedinFigure3,FEmodelwiththerocksizeof400mm× surface”contacttypeofESTSalgorithmwaschosen, 400mm × 500mm (length × width × thickness) was only MathematicalProblemsinEngineering 7 Time=0.002s 0 (a) (b) (c) 0.125E+07 0.250E+07 a) 0.375E+07 P 0.500E+07 vg) ( a 0.625E+07 V ( Q E 0.750E+07 S 0.875E+07 0.100E+08 Time=0.002s 0 (d) (e) 0.125E+07 0.250E+07 a) 0.375E+07 P 0.500E+07 vg) ( a 0.625E+07 V ( Q E 0.750E+07 S 0.875E+07 0.100E+08 Figure8:TheVonMisesequivalentstresstop-viewcontoursofdifferentmodelsatthe0.002ths. 1.0E+06 1.0E+06 1.0E+06 8.0E+05 8.0E+05 8.0E+05 6.0E+05 6.0E+05 6.0E+05 a) 4.0E+05 a) 4.0E+05 a) 4.0E+05 P P P ( 2.0E+05 ( 2.0E+05 ( 2.0E+05 0.0E+00 0.0E+00 0.0E+00 −2.0E+05 A −2.0E+05 B −2.0E+05 C 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 T (s) T (s) T (s) (a) TheVonMisesequivalentstresscurves 1.0E+06 1.0E+06 1.0E+06 5.0E+05 5.0E+05 5.0E+05 a) 0.0E+00 a) 0.0E+00 a) 0.0E+00 P P P ( ( ( −5.0E+05 −5.0E+05 −5.0E+05 −1.0E+06 A −1.0E+06 B −1.0E+06 C 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 T (s) T (s) T (s) (b) The1stprincipalstresscurves 1.0E+06 1.0E+06 1.0E+06 5.0E+05 5.0E+05 5.0E+05 0.0E+00 0.0E+00 0.0E+00 a) a) a) P −5.0E+05 P −5.0E+05 P −5.0E+05 ( ( ( −1.0E+06 −1.0E+06 −1.0E+06 −1.5E+06 A −1.5E+06 B −1.5E+06 C 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 T (s) T (s) T (s) (c) The3rdprincipalstresscurves Figure9:StressvariationcurvesofbottomnodeinmodelsA,B,andC. 8 MathematicalProblemsinEngineering 1.0E+06 1.0E+06 1.0E+06 8.0E+05 8.0E+05 8.0E+05 6.0E+05 6.0E+05 6.0E+05 a) 4.0E+05 a) 4.0E+05 a) 4.0E+05 P P P ( 2.0E+05 ( 2.0E+05 ( 2.0E+05 0.0E+00 0.0E+00 0.0E+00 −2.0E+05 A −2.0E+05 D −2.0E+05 E 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 T (s) T (s) T (s) (a) TheVonMisesequivalentstresscurves 1.0E+06 1.0E+06 1.0E+06 5.0E+05 5.0E+05 5.0E+05 Pa) 0.0E+00 Pa) 0.0E+00 Pa) 0.0E+00 ( ( ( −5.0E+05 −5.0E+05 −5.0E+05 −1.0E+06 A −1.0E+06 D −1.0E+06 E 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 T (s) T (s) T (s) (b) The1stprincipalstresscurves 1.0E+06 1.0E+06 1.0E+06 5.0E+05 5.0E+05 5.0E+05 0.0E+00 0.0E+00 0.0E+00 a) a) a) P −5.0E+05 P −5.0E+05 P −5.0E+05 ( ( ( −1.0E+06 −1.0E+06 −1.0E+06 −1.5E+06 A −1.5E+06 D −1.5E+06 E 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 0 0.2 0.4 0.6 0.8 T (s) T (s) T (s) (c) The3rdprincipalstresscurves Figure10:StressvariationcurvesofbottomnodeinmodelsA,D,andE. Table1:Mainparametersofhydraulichammerwithlargeimpact Figure4), including model A (dr = 20mm, di = 200mm), energy. modelB(dr=20mm,di=250mm),modelC(dr=20mm,di =150mm),modelD(dr=35mm,di=200mm),andmodel Parametername Value E (dr = 50mm, di = 200mm). As shown in Figure5, there Impactenergy 7500J were 28 typical nodes researched in each model, including Pistonweightofhammer 200kg bottom node (node 1), nodes along the diagonal (nodes 20 Roddiameter 150mm to28),nodesarounddrillinghole(nodes14to19),andnodes Pistonenergytransferefficiency 98% alongsideline(nodes8to13). Elasticmodulusofrodmaterial 1.02𝐸11Pa The impact frequency of rod was 10Hz, and its loading Densityofrodmaterial 7800kg⋅m−3 curvewasdemonstratedinFigure6,whichlastedonesecond. In accordance with the impact energy and energy transfer Impactfrequency 10Hz Rodweight 200kg efficiency𝜂𝑆 (betweenthepistonofhammerandrod)listed RRooddtleipngdtihameter 122000mmmm i2n00Ta×bleVr1o,dt2h/e2v;enloacmiteylyo,frVorodd(V=ro8d).5s7hmou⋅sld−1m. Feeutr7th5e0r0m×o9r8e%, t=o ensure the efficiency of HDIHT method, a pressing force Rodtiplength 200mm wouldbeappliedontherodtooffsetitsreboundaftereach Poisson’sratioofrodmaterial 0.3 impactandkeepitincontactwithbrokenpitallthetime.The valueofpressingforcecouldbecalculatedby[1] a quarter of the actual one and the symmetry boundary 𝐹=2𝑓𝑀𝑉𝑃 =0.015𝑁𝑓√𝐺𝐴, (14) conditionswereappliedonitssymmetryplanes. There were five different models developed to explore where 𝑁𝑓 was the impact frequency of hammer (BPM), 𝐺 the stress variation behavior during HDIHT process (see wastheweightofhammer’spiston(kg),and𝐴wastheimpact MathematicalProblemsinEngineering 9 3.0E+06 3.0E+06 2.0E+06 2.0E+06 a) a) P P ( 1.0E+06 ( 1.0E+06 0.0E+00 0.0E+00 0.1 0.3 0.5 0.7 0.9 0.1 0.3 0.5 0.7 0.9 T (s) T (s) A A B B C C (a) Node28 (b) Node27 3.0E+06 3.0E+06 a) 2.0E+06 2.0E+06 (P Pa) 1.0E+06 ( 1.0E+06 0.0E+00 0.0E+00 0.1 0.3 0.5 0.7 0.9 0.1 0.3 0.5 0.7 0.9 T (s) T (s) A A B B C C (c) Node26 (d) Node25 3.0E+06 3.0E+06 2.0E+06 2.0E+06 (Pa) 1.0E+06 (Pa) 1.0E+06 0.0E+00 0.0E+00 0.1 0.3 0.5 0.7 0.9 0.1 0.3 0.5 0.7 0.9 T (s) T (s) A A B B C C (e) Node24 (f) Node23 5.0E+06 5.0E+06 4.0E+06 4.0E+06 3.0E+06 3.0E+06 Pa) Pa) ( 2.0E+06 ( 2.0E+06 1.0E+06 1.0E+06 0.0E+00 0.0E+00 0.1 0.3 0.5 0.7 0.9 0.1 0.3 0.5 0.7 0.9 T (s) T (s) A A B B C C (g) Node22 (h) Node21 Figure11:Continued. 10 MathematicalProblemsinEngineering 4.0E+07 3.2E+07 2.4E+07 a) P ( 1.6E+07 8.0E+06 0.0E+00 0.1 0.3 0.5 0.7 0.9 T (s) A B C (i) Node20 Figure11:TheVonMisesequivalentstresspeak-curvesofnodesalongthediagonalinmodelsA,B,andC. energy(kg⋅m).Thus,thefinalpressingforceshouldnotbeless pointofHDIHTprocess;(2)whendikeptconstant,withthe than increaseofdrillingradius,theVonMisesstressofhole-nodes 𝐹=0.015×600×√200×750×10=34850𝑁. (15) wouldascendsimultaneously.Thatis,thebiggerthedrilling radiuswas,thelargerthemaximumVonMisesstressofhole- nodeswas. 4.SimulationResultsandDiscussion 4.1. Von Mises Equivalent Stress Contours. Figure7 showed 4.2. Stress Behavior of Bottom Node (Node 1). In terms of the Von Mises equivalent stress contours of model A at thethreeprincipalcomponentsoftheVonMisesequivalent differenttime.Obviously,therodcouldbepenetrateddeep stress, because of the symmetry of FE model, only the 1st intothegranitegradually.Inthemeantime,theelementsin principalstressandthe3rdprincipalstresswerediscussedin brokenpitwere“killed”andremoved,fortheirstresseshad thesimulations.Thelocationofbottomnode(seeFigure5) exceededthecompressiveorshearstrengthofgranite.Itwas wasjustbelowthedrillrodandcoulddirectlyreflectthestress consistentwiththeconclusionoftheoreticalcalculation. behavior of the rock under impact rod. Figure9 revealed Figure8depictedtheVonMisesstresstop-viewcontours the stress variation curves of bottom node in models A, ofdifferentmodelsatthe0.002ths.Asdemonstratedinthe B, and C, including the Von Mises equivalent stress, the figure, when dr was fixed (20mm), there was a significant 1st principal stress, and the 3rd principal stress. Obviously, stressconcentrationphenomenonaroundtheholeinmodel whendrwasfixed(20mm),amongthosethreemodels,the A, and the maximum Von Mises stress of hole-nodes (14 stressofbottomnodeinmodelCwasthelargest,whilethat to 19; see Figure5) in model A was 2.69MPa. Instead, as in model B was the smallest, whether for the Von Mises di was larger or less than 200mm, the stress concentration equivalent,the1stprincipalstress,orthe3rdprincipalstress. phenomena around the holes both were weakened and Likewise,Figure10demonstratedthestressvariationcurves became no longer obvious. In this case, the maximum Von of bottom node in models A, D, and E. It was evident that Misesstressesofhole-nodesinmodelsBandCwere1.72MPa whendikeptconstant(200mm),amongthosethreemodels, and 2.29MPa, respectively. Likewise, for models A, D, and theVonMisesequivalentstressofbottomnodeinmodelE E, when di was constant (200mm), there were significant wasthesmallest,whilethatinmodelDwasthelargest.The stressconcentrationphenomenaaroundtheholeforallthree 1stprincipalstressofbottomnodeinmodelEwasrelatively models. The maximum Von Mises stress of hole-nodes in large,butits3rdprincipalstresswasquitesmall. model D was 3.14MPa and that of hole-nodes in model E Comparing Figure9 with Figure10, the following was was3.24MPa.Oncethestressreachedorexceededthetensile evident.(1)Forthe1stprincipalstressandthe3rdprincipal strength of granite, which was only three to five percent of stressofbottomnode,therewereobvious“compress-tensile its compressive strength, it might result in the secondary stress”transformationphenomena,whichcouldbeattributed crushingoftherocknearthehole. to the existence of drilling hole free surface. (2) When dr Therefore,thefollowingresultscouldbegained:(1)inthis remainedunchanged,thestressesofbottomnodeinmodelC work, the impact distance of 200mm might be the critical weredistinctlylargerthanthoseinmodelsAandB,regardless
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