WATER JET CONFERENCE - Waterjet Technology Association

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Results of Trial Tests As part of machine verification and trial tests, a complete series of tests were run with the rotary cutting machine. The rock sample used was a fabricated sample consisting of various size boulders of soft and hard rock cast in a concrete matrix. The purpose of using such rock sample was to simulate mixed face tunneling conditions in order to verify the proper operation of all machine controls and data monitoring systems under most adverse cutting conditions. Various cutter forces were measured and recorded during trial tests. Tests were run at various machine thrust loads and cutter head rotational speeds. The analysis of test results showed a wide degree of cutter force fluctuations over the cutter head. In particular, very high peak loads were encountered on gage cutters, confirming the hypothesis that gage cutters are subject to more force fluctuations and higher shock loads than the center and inner cutters. By combining the load histories of instrumented cutters, a three-dimensional plot of cutter force distributions over the cutter head for one specific period of cutting was generated (Figure 4). Such a "fingerprint" of the tunnel face is useful in determining the hard inclusions in the face and the resultant force distributions over the cutter head. LABORATORY DRILLING FIXTURE Description and Capabilities An overall view of the laboratory drill rig is shown in Figure 5. The basic machine frame consists of a heavy I-beam weldment which serves to maintain all thrust and torque reactions within the system. The frame is bolted to the concrete foundation to provide stability during drilling. The condensed specifications of this equipment are listed in Table 2. The machine drive system consists of a Dresser Model-800 raise bore drive unit which features two pinions driving into a common gear. The drive unit includes four guide shoes which slide on structural guide columns. The columns are bolted to the base frame and further secured with a series of L-shaped steel plates, as can be seen in Figure 5. The cutterhead rotation is provided by a variable volume hydraulic motor. A 150 hp AC motor driving a variable volume hydrostatic pump delivers the necessary oil to the drive motor. Due to the hydraulic drive feature, the rotational speed of the drill bit is infinitely variable from O to 50 rpm. The torque generating capability is 25,000 ft-lbs at 20 rpm. Beyond this speed, torque decreases with constant horsepower input. A double-acting hydraulic actuator is used to provide forward thrust to the bit. The maximum thrust capability currently available is 100,000 lbs. The machine is designed to withstand higher thrust loads which can be generated by adding a second actuator to the hydraulic thrusting mechanism. Power to the thrust actuator is supplied by a 20 hp AC motor driving a 10.9 gpm variable volume pump. The maximum forward stroke of the drill rig is 54 inches. 361
The drilling fixture is designed to permit testing of bits of up to 3 ft. in diameter. The drill pipe is fitted with an adapter plate onto which various types of drill bits can be mounted. Presently, the machine is fitted with a 28-inch diameter roadheader cutting head dressed with conical bits (Figure 6). Controls and Data Monitoring System The laboratory drilling fixture is equipped with various types of transducers to monitor and measure machine operative parameters. Presently, instrumentation is available for measuring thrust, torque, rpm, penetration rate, water-jet pressure and flow. Provisions have been made for expanding the number of data channels that can be measured as need arises. Machine thrust is measured with a pressure transducer installed on the thrust actuator hydraulic line. A similar type pressure transducer is also used for measuring the torque pressure supplied to the drive motor. Penetration rate measurement is accomplished with a 10-turn potentiometer mounted on one of the guide shoes. This potentiometer is calibrated to produce a certain voltage output for a given linear movement of the drive assembly with respect to the fixed base frame. A DC-generator type transducer is used to measure the rotational speed of the cutterhead. The drilling fixture is currently operated with manual hydraulic controls. A control panel located behind the machine in an elevated position contains all necessary controls and meters for the manual operation of the equipment. Data from all transducers is routed to a multi-channel light-beam recorder which features high frequency response and a wide selection of chart speeds. Future plans for the drill rig call for its totally automated operation using the commuter system that is currently available with the rotary cutting machine. This will permit electronic servo-control of drill rig operative parameters and enable high speed acquisition and analysis of data generated from testing. Thus, the main computer control system described earlier will incorporate the capability of running either one of the two machines. Design work is also underway for installing a 6-channel wireless telemetry unit on the drill rig. The system will be mounted on the center rotating tube which passes through the drive head. Selected bits on the cutterhead will be instrumented and data telemetered to recording devices in order to measure bit forces during rock cutting. Test Plans As noted previously, the drill rig is currently fitted with a 28 inch diameter roadheader cutting head equipped with conical bits. The system is being used as part of a research program sponsored by the Department of Energy to evaluate various cutting techniques for the mechanical mining of oil shale. This effort will primarily concentrate on conducting a series of tests to assess the applicability of roadheader type machines to cutting of oil shale. Included in the investigation will be the evaluation of obtainable 362
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Proceedings of the Second U.S. WATE
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Visualization of the Central Core o
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A Status Report on the Conceptual D
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SESSION 7 - CIVIL & INDUSTRIAL Chai
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Cutting Hard Rock With Abrasive-Ent
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frictional and piping component rel
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R = a1 ⋅ A1 A2 a2 I = 2H o Q o
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attenuation of the output. The tran
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Figure 1. Branch System Modulator F
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Figure 5. Modulation Response for B
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Figure 9. Modulation response for s
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can be used for any form of input.
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with a cylindrical shape to the jet
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m/s. The range of power found from
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Figure 3. Power vs nozzle diameter
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Figure 5. Frequency vs length of th
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NAME: Gerald Zink COMPANY: StoneAge
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modulatornozzle assembly. The ordin
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DISCUSSION OF FLUID MECHANICS The i
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This process serves to protect the
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For test purposes, these concrete b
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REFERENCES CITED 1. Barker, C. R.,
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FIGURE 4. INNER CORE OF PERCUSSIVE
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FIGURE 9. EXAMPLE OF HIGH-PRESSURE
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NAME: John E. Wolgamott COMPANY: St
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THE FOCUSED SHOCK TECHNlQUE FORPROD
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The reflected wave is thus also cyl
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neglected. The introduction of a co
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DISCUSSION NAME: George Savanick CO
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H’ mean shape factor Hj theoretic
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Required streamline curvature at th
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2 x 2 ≅ ( e − 2 p + w)/k2 (2-8)
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eliminating 2 n r 2 from equations
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approximation to the actual flow si
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skin friction coefficient but are c
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where: (H) = A1H 3 + A2H 2 + A3H +
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effect (< 0.5%) on coefficients of
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TABLE 5 Rei x 10 5 β 3 4 5 6 Po Po
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TABLE 6 D(mm) d o(mm) L t(mm) L f(m
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expanding rather than contracting a
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25. Weber, H.E., 1978, Boundary lay
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Figure 5. Wall velocity distributio
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Figure 9. Effect of nozzle design o
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Figure 12. CA+T Design Philosophy.
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Figure 16. Effect of inlet b 1 cond
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Figure 20. Relaminarization at nozz
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Figure 24. Pressure decay data. 88
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VISUALIZATION OF THE CENTRAL CORE O
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DISCUSSION Although employing the i
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5. Lambert, J. H., 1760, Photometri
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Figure 6. Spectral sensitivity curv
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NAME: W.C. Cooley COMPANY: Terraspa
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INTRODUCTION Pulsed liquid jets sho
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y=X ∨ P A dy = p p A p 2 (L c y=0
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Using equation (15), the value of X
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Thus about the first 10% of the dri
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Many design cases, including those
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surface spall occurred, resulting i
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Figure 3. Chamber pressure at pisto
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Figure 7. Effect of nozzle area rat
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Figure 11. Extrusion device schemat
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Figure 15. Typical chamber pressure
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DISCUSSION NAME: W. C. Cooley COMPA
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material which are, in turn, affect
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the water jet. This method was not
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where h is the depth of penetration
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obtained during this phase of the i
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observed that the smallest depth of
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Figure 2. Idealized Relationships b
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Figure 6. Penetration as a Function
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DEVELOPMENT OF VARIABLE DELIVERY TR
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THE STRUCTURE AND FUNCTION OF THE P
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The injection pressure can be contr
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ACKNOWLEDGEMENTS The authors gratef
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Figure 4. Theoretical required powe
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Figure 9. Variation of efficiency w
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THE "SKIPJACK" SEWER CLEANING NOZZL
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HYDRO-BLASTING SAFETY C.W. Adaway,
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Remember, your Hydro-Blasting work
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horizontal, sometimes vertical, and
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Figure 2. Safety Gear Figure 3. Tub
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DEVELOPMENTS IN CLEANING COKE OVEN
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causing chain breakages and the scr
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was encountered, then the rotation
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(C) Capital Expenditure: Material i
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Figure 9. Swivel coupling Figure 10
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OPTIMIZING JET CUTTING POWER FOR TU
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PRESSURE DROP (psi) ELEMENT Cv @10
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power output. Undersized nozzles re
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Subscripts n - Nozzle p - Pump t -
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Figure 1. Cutting effect as a funct
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CONSIDERATIONS IN THE COMPARISON OF
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pressure can be lowered to perhaps
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Figure 2: Fan jet issuing from a no
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DISCUSSION NAME: John Griffiths COM
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where Q = Flow rate - gpm D = Jet O
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Again, not limited to Newtonian flu
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REFERENCES 1. Brown, R.W. and Loper
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Table 2. Jet Cleaning Speeds and ot
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ANSWER: The utilization of the stat
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complexity and short component life
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Figure 4, for ap values ranging fro
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Decontamination Methods for rapidly
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a. “PULSER” b.”ORGAN-PIPE”
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Figure 5 - Removal rate for various
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DISCUSSION NAME: David A. Summers C
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DRILLING BORE HOLES IN COAL MINES U
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pile could not be judged as represe
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DISCUSSION NAME: David Summers COMP
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HYDRAULIC MINING EXPERIMENTS IN AN
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The monitor was fed pressurized wat
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The IH rig was considered to be sup
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REFERENCES 1. Okhrimenki, V. A., A.
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Figure 2. Jet cutting sandstone at
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Figure 5. Schematic plan view of In
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Figure 7. Suction Box. 226
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USE OF HIGH PRESSURE WATER JETS FOR
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flame torch to cut this block, redu
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the order of 360 rpm. Under these c
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Figure 3. Slot cut by jet at 11 o s
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JET-MINER SURFACE AND IN-SEAM TRIAL
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The hydraulic drive of the haulage
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The surface trials had have the obj
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Figure 2. Experimental version. Fig
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Figure. 7 Jet-Miner prototype Figur
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SOME PATTERNS OF TECHNOLOGY TRANSFE
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Development of High Pressure_Techno
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configurations, the design of an op
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and public sectors. After a haitus
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Souder, W.E. and Evans, R.J., "The
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Figure 5. Technological achievement
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Table 3. Perceived disadvantages of
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already been, or is being applied w
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Using the requirements profile and
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ant hose combination, a guiding sys
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HYDRAULIC MINING TESTS Site selecti
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SAFETY All operations were carried
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TABLE V. Categories of Jet Mining D
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Figure 2. Generalized geologic prof
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SECONDARY FRAGMENTATION WITH WATER
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do possess a maximum point (Fig. 8)
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Figure 4. Rossin-Rammler plot. Figu
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Figure 8. Non-dimensional plot for
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HYDRAULIC COAL MINING SYSTEM Typica
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Figure 4. (From ref. 1) DISCUSSION
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INTRODUCTION Developing an unique t
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The coefficients "b " in Eq. (1) ca
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By the end of 1982, a total of more
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Figure 4. Cutting ability of swing-
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Figure 10. An operating performance
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for an abrasive, the abrasive parti
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the particles, while at slower spee
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to break away the remaining segment
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Table 1. Concrete saw technology. T
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NAME: Tom Brunsing COMPANY: Foster-
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FEASIBILITY STUDY OF CUTTING SOME M
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hydraulic power required to cut thr
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pressure was varied from 103 to 310
Page 318 and 319: 2.1 Heading and gutting fresh cod f
Page 320 and 321: Figure 5. The cuts surface of a blo
Page 322 and 323: Figure 17. Cuts made across the cla
Page 324 and 325: JET NOTCHING USED IN THE CONSTRUCTI
Page 326 and 327: Bottom notch diameter was determine
Page 328 and 329: σ H = in-situ stress in the horizo
Page 330 and 331: Figure 3. Final block displacement.
Page 332 and 333: Figure 8. Comparison of Slurry Pump
Page 334 and 335: THE FURTHER DEVELOPMENT OF AN UNDER
Page 336 and 337: use taps or hydrants. To achieve th
Page 338 and 339: supply line. It was determined that
Page 340 and 341: The rotating head requires major mo
Page 342 and 343: Figure 4. System field test set-up
Page 344 and 345: Figure 10. Bentonite drilled clay s
Page 346 and 347: MECHANICAL TOOLS Cutting Tool Energ
Page 348 and 349: Ψ = cos −1 ⎧ ⎪ ⎪ ⎨ ⎪
Page 350 and 351: mode also contributes to chip flush
Page 352 and 353: NAME: Simon Johnson COMPANY: Newcas
Page 354 and 355: ROLLER TOOLS COMBINED WITH HIGH-PRE
Page 356 and 357: Various designs and applications ar
Page 358 and 359: Figure 1. Full-face tunneling machi
Page 360 and 361: Figure 11. roadway profile cutting
Page 362 and 363: Figure 19. High-pressure water jet
Page 364 and 365: DESIGN AND OPERATION OF TWO LARGE-S
Page 366 and 367: The hydraulic system for the thrust
Page 370 and 371: cutting rates, degree of bit wear,
Page 372 and 373: Overall approximate Weight: Basic M
Page 374 and 375: Figure 5. 3 ft. diameter laboratory
Page 376 and 377: nozzle diameter and cutting speed w
Page 378 and 379: 2. Cutting Speed The influence of c
Page 380 and 381: energy it effects an increase in me
Page 382 and 383: Tip angle (degrees) 87 Off-set angl
Page 384 and 385: Figure 5. Figure 6. Figure 7 Figure
Page 386 and 387: Figure 17. Figure 18. Figure 19. Fi
Page 388 and 389: SCHEMES OF COAL MASSIF BREAKAGE BY
Page 390 and 391: out thoroughly an efficient scheme
Page 392 and 393: Research analysis has proved that t
Page 394 and 395: DEPENDENCE OF POWER INDICES OF COMB
Page 396 and 397: The experiments have shown how the
Page 398 and 399: K Ay = coefficient correcting for f
Page 400 and 401: Figure 1. Schemes of combined break
Page 402 and 403: Figure 5. Dependence of specific en
Page 404 and 405: Figure 12. Percentage of grade R -6
Page 406 and 407: Figure 1. Particle size analysis. T
Page 408 and 409: NAME: Dr. Henkel COMPANY: Bergbau-F
Page 410 and 411: presented. This study, of course, i
Page 412 and 413: identifying a general trend for the
Page 414 and 415: Effect of Abrasive Hardness, Shape
Page 416 and 417: In some situations, especially in c
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Figure 1. Abrasive waterjet nozzles
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Figure 8. Effect of standoff distan
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Figure 13. Abrasive waterjet cuts i
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CUTTING WITH ABRASIVE WATERJETS M.
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3.3 Abrasive Feed Systems For abras
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Because of the large number of infl
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due to wear. Although actual operat
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from this new technology. Table 2 l
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Table 1. materials cut by abrasive
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Figure 1. Abrasive waterjet nozzles
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a) kerfs in mild steel b) S.S. 15.5
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a) circle cutting in glass b) lamin
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DISCUSSION NAME: Andrew F. Conn COM
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CUTTING HARD ROCK WITH ABRASIVE-ENT
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slurry nozzle. Testing at water pre
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DISCUSSION OF TEST RESULTS Jet Conf
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materials. The flexibility in nozzl
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pressure can be wiped out if diffic
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9. Maurer, W.C., and Heilheckler, J
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Figure 5. Effect of abrasive feed r
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Figure 9. Accumulated depth of mult
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Figure 13. Close-up view of quartzi
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ABRASIVE INJECTION USAGE IN THE UNI
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sudden changes in the feed rate eff
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or the abrasive must be manually to
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clog; there not being sufficient ar
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CODE OF PRACTICE FOR THE USE OF ABR
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Figure 5. Water abrasive cleaning h
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Figure 15. 360 0 abrasive pipe clea
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ECONOMIC CONSIDERATIONS IN WATER JE
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Other criteria to be considered in
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3 MANUAL METHODS OF JET CLEANING &
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contractor with old, unsafe, equipm
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Figure 1. Showing the increased cos
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Figure 8. Automatic tube bundle cle
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ackground to the subsequent coopera
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The molecules of SUPER-WATER posses
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shaken just before use. SUPERWATER
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26. Bednarz, L.P., "Effects of Poly
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