AU637472B2 - Fracturing method and apparatus employing destructive resonance - Google Patents

Description

637472 COMMONWEALTH OF AUSTRALIA PATENTS ACT 1952-69 COMPLETE SPECIFICATION

(ORIGINAL)

Form Class Int. Class Application Number: Lodged: 73993/91 28th March 1991 Complete Specification Lodged: Accepted: Published: Priority Related Art:

OS*

aS 0 S Name of Applicant *a

S..

Address of Applicant S Actual Inventor: *'Address for Service JOHN G. SELLAR 6045 W. Evans Place, Lakewood, Colorado 80227, United States of America JOHN G. SELLAR WATERMARK PATENT TRADEMARK ATTORNEYS.

LOCKED BAG NO. 5, HAWTHORN, VICTORIA 3122, AUSTRALIA Complete Specification for the invention entitled: METHOD AND APPARATUS FOR EMPLOYING DESTRUCTIVE RESONANCE The fowing statement is a full description of this invention, including the best method of performing it known to me The following statement is a full description of this invention, including the best method of performing it known to me "METHOD AND APPARATUS FOR EMPL.OYING DESTRUCTIVE RESONANCE" The present invention relates generally to the field of resonance measuring and testing, and more particularly to the use of measured resonance as an Input to a resonance producing apparatus for destructive purposes.

s* 0 00 0 0000 2 040* Background Art As can be seen by reference to the following U.S.

Patent Nos. 4,539,845; 4,283,956; 4,307,610; 4,446,733; and 4,389,891, the prior art Is replete with myriad and diverse resonance measuring and testing apparatus, Molimar, U.S. Patent No. 4,539,845, describes the mechanical sensing of the natural frequency of an object under fatigue testing, electrically coupling the sensed frequency to a mechanical input device so that the object is kept at resonance but controlling amplitudes to fixed values, thereby reducing the testing time and forces required for fatigue testing compared with the other methods, wherein the amplitude of vibration of the tested object engine and motor components) is kept to a predetermined set point value.

Okubo, U.S. Patent No. 4,446,733, like Molimar, uses a combination of mechanical sensing, electric coupling, and mechanical input to measure and maintain resonance in structural materials for the purposes of stress relieving, fatigue testing and non-destructive load testing.

Fournler, U.S. Patent No. 4,389,891, in a manner similar to Molimar and Okubo, also uses a combination of mechanical sensing, electric coupling, and mechanical Input to measure the natural frequencies in turbine and compressor *o 25 vanes and propeller blades.

In addition, Leupp, U.S. Patent No. 4,307,610, uses a combination of mechanical sensing, electric coupling, and mechanical Input to maintain resonance in order to measure crack propagation In samples for assessing the fatigue behavior of a material or a component; and Lechner, U.S.

Patent No. 4.283.956 induces resonance to detect and indicate the onset of cracking in articles subjected to dynamic loading.

While all of the aforementioned prior art patents are more than adequate for the basic purpose and function for which they have been specifically designed, these prior art methods and apparatus have overlooked the fact that even though resonance can be a highly destructive orce, that destructiveness can be used for useful purposes.

Resonance is an extremely powerful phenomena. Major man-made structures, designed to be indestructible, have been destroyed by relatively insignificant forces, which by chance have been applied at resonant frequencies. All objects and structures have resonant frequencies, some of which can be sufficiently "damped" to be almost undetectable.

The destructive power of resonance is witness to the 0.0e well known Army instruction "break step on bridges" and is evidenced by that most famous bridge failure at Tacoma.

Washington. captured on film in 1940, wherein a 2.800 foot span of two lane bridge literally "blew down" in a 40 mph wind.

While the body of knowledge on resonance is extremely large, there have been very few attempts to use the 25 destructive power of resonance for useful work in the mining industry.

The work that has been done appears to have concentrated on the ultrasonic frequency range, above 20,000 cycles/second, whereas, experimental field data on -3three rock types indicates that lower frequencies, under 4.000 Hz. are more applicable.

Resonant frequencies are those that a solid body naturally assumes during relaxation from an energized state to an unenergized state. The lowest frequency at which a body freely vibrates Is called the primary frequency. Other resonant frequencies are called harmonics. When bodies are excited, deliberately or by accident, at their resonant frequencies, very small forces can display seemingly disproportionate and devastating effeqts.

The application of energy to excite resonant frequencies is restricted by basic underlying principles.

Vibration can be represented by a simple pendulum, such as a ball suspended from a string. To Initiate the pendulum motion, the ball is displaced to one side of the quiescent position of the pendulum. Once the ball is released, the most effective phase of the pendulum swing to apply energy to increase amplitude occurs between the release of the ball and the arrival of the ball at the quiescent position. As the ball passes through the quiescent position, the positive force of the ball diminishes to the point where the ball stops and swings back towards the release position wherein 'ee the reverse travel of the ball is always acting against the Initial direction of the swing.

25 Applying this example to the principles of resonance, It is the amplitude of vibration exceeding the elasticity constant which breaks solid objects,, The objective In applying resonance for destruction is therefor to maximize 4 C the swing. It can be seen that the most effective time to apply energy to the pendulum is the first one-fourth of one cycle. To maximize amplitude, under no circumstance can the energy pulse be greater than one-half of one cycle. This Is the first of two basic principles. Pulse time must be less than 1/2f (Ideally, I/4f) where f primary frequency, in cycles per second.

Again, using the pendulum, It is apparent that the energy pulse can be applied every swing (cycle) every second swing, or every third swing etc., It cannot be applied twice per swing. This is the second principle. The frequency of the pulse is either f or f divided by an Integer. It cannot exceed f.

While these two principles are simple, maintaining their Integrity In practice is not. Indications are that the applicable frequency range Is between 200 and 5,000 cycles **15 each second. Physically pulsing energy at these high cyclical rates is difficult enough and Is compounded by the requirement for absolute accuracy. If the pulse frequency Is out by even one cycle per second, then for half of every second the pulses act against resonance.

Unlike the simple sine-wave type motion of a swing, rock present a much more complex phenomena. The apparent resonant frequency of a particular rock may be expected to

S

be effected by at least the following: the mass of the rock, the rock material the circumstances of the rock free 25 standing, partially embedded, etc.), discontinuities Joints and fractures, the point of measurement, and, the point of excitation, However, provided that: the points of excitation and measurement do not change, the Input force frequency exactly matches the measured frequency or the measured frequency divided by an integer, the input force waves are supportive In phase, and the amplitude of vibration does not return to zero between pulses, then the rock will be in resonance.

If the amplitude is Increased to the point where the measured resonant frequency is changed, then destructive work has been accomplished. This of course may not break the rock it may merely have altered the circumstances of a fracture or Joint plane. To effectively achieve breakage, not only must the amplitude of the resonant vibration be sufficient, but any change in measured output frequency must Immediately be reflected in the input frequency.

*3* 3* *0 3 0 3 Disclosure of the Invention Briefly stated, the present invention involves the use of resonance to effectively utilize a destructive power to produce a beneficial result in a mining and/or comminution environment wherein low electrical power outputs are used to produce disproportionate results compared to conventional techniques.

In essence, the present Invention comprises a method and apparatus for sensing the resonance of a mass such as rock, or rock particles or the bonding between rock particles and applying a resonant pulse to the same to Induce fractures.

In addition, the method of this invention uses resonant frequencies below the ultrasonic frequency of 20,000 cycles per second to accomplish the destructive fracturing of a mass.

As will be explained in greater detail further on, means are used to measure the exact or approximate fundamental resonant frequency or frequencies of solids or 000 solid particles or the bonding between solid particles In their Individual circumstances and electronically couple the measured frequency or frequencies divided by an Integer, to

C

an Input device such as a laser, wherein, the vibration of the mass is sensed by a remote vibration detector whose 25 output is used to determine the change in resonant frequency produced by the partial fracturing of the rock, whereupon, the frequency producing means is varied to the new frequency o.

to continue the fracturing process occuring within the rock 0.000:

C

mass.

If energy is applied scientifically at resonance, It Is reasonable to assume that the energy level required will be much less than either the laboratory measured crushing energy level or the brutal non-scientific battering delivered by a rock breaker. Looking at these different breaking techniquest crushing, single blow, and resonance; if an energy relationship can be established between crushing and single blow, and then between single blow and resonance, it should be possible to estimate the relationship between resonance and crushing.

Firstly, scientific laboratory information is available on crushing energy levels and single blow energy levels to achieve rock breakage. By comparing the two, an order of magnitude saving can be estimated between the slow application of energy (crushing) as opposed to the fast application (single blow).

For example: Crushing: Laboratory tests on Hematite samples show crushing eneryy levels of 15-30 Joules per kg.

to*** 0O

S

*s 0

S

.5 Single blow: Laboratory tests Indicate that single blow energy levels required for breakage are approximately 2 x weight (tonnes) Joules per kg.

25 Therefore: Cruh!InqEnerm 25 to Blow Energy W W where W is expressed in tonnes.

This gives wide ranging orders of magnitude depending on weight. For minus 200 mm Hematite (primary crusher undersize), the ratio is 250 500 times. For 1 metre cubed primary crusher feed, the ratio is 2 4 times.

Determining the relationship l,-tween single blow energy levels and resonance energy levels for breaking rock Is obviously impossible breaking rock using resonance has not yet been achieved. However, using scientific laboratory test results on other materials, the likely magnitude of the resonant to off resonant (single blow) ratio can be established.

Laboratory testwork on metal plates, Indicates that power levels at resonance to achieve a given deflection are between 7 and 50 times less than the off resonant single blow power. Published pile driving information comparing single blow piles with resonant piles, Indicates that speed increases between 30 and 130 times have been achieved. Using these results. It can be assumed that the ratio of 15 non-resonant (single blow) to resonant energy is likely to *b a: be in the range of 10 to 100.

9 Combining the two ranges indicates that energy e requirements at resonance may be 20 to 50,000 times less than energy levels required for crushing. Table 1 reproduced below.

Testwork on rock types have been restricted to Hematite, B.I.F. (Banded Iron Formation) and Shale. Rock sizes have varied from 10 cm cubes up to 25 cubic metre 0 o boulders. This testwork has Indicated a rough correlation between primary resonant frequencies and volume where: F= k ffe 0 F Hz (cycles/sec) V Volume Additional testwork has indicated that resonant freauencies of rocks larger than 200 mm cubed (primary crusher undersize) are less than 4.000 H z Rocks over 0.5m 3 (a cube with 0.8 m sides) have frequencies under 1.000.

These two figures are important.

Firstly, a mechanical device currently exists which can deliver accurate pulsed energy of 11 kW up to 1.000 cycles/second. In theory, this machine can break rocks up to tonnes using resonance, by delivering in 5 seconds. more than the calculated crushing energy at 30 Joulesk'a.

Below 0.5m 3 sizes frequencies above 1.000 cycles/sec.), the frequency is such that electronic devices are required to control the accuracy of energy pulses.

Lasers are an obvious choice. Pulsing lasers up to 25.000 ilz are commercially available and a 55 watt (average power) unit while only ab! to deliver sufficient power to theoretically break a minus 100 mm rock, this rock size aces up to 200 mm usina a resonance "leveraae" factor of 10. to 270 mm using 30; to 470 mm using 100 and to 1 metre using 1.000.

The attached eneray and power tables compare four S different sources. Impact Breakers (Rammer). High Pressure *~co Pulsing Pumps. .22 Calibre Bullets and a 55 watt Pulsing Laser. This odd assortment of power sources is chosen for 25 the following reasons: The Rammer 2000 breaks all Hematite and B.I.F. rocks: the Rammer 1600 breaks most of them. It is believed to be possible to accurately generate controlled

SC

pressure pulses in a water jet. Reliable high pressure pumps are available and as the calculations show. high speed water "sluas" look very powerful. A 2000 round-a-minute (33Hz) .22 calibre rifle is commercially available. The rifle is more destructive than it should be according to its manufacturers. It "carves up" bullet proof vests which easily stop single heavier calibre bullets. Calculations involving a single round, nevertheless, show the projectile as a powerful energy source. The bullet has a very brief Impulse time. Laser calculations refer to a 55 watt (average power) laser.

The column "Peak Power" Is a laser terminology. It is a calculation of the energy delivered by one pulse, over the time of that pulse, then multiplied up as if that power was delivered continually over 1 second.

Of particular interest in the first two tables are the following: The Rammer 1600 is more "powerful" than the **15 Rammer 2000, but it delivers less energy per blow and less om,, energy per blow per unit area. Energy delivered per unit area is physically limited by the strength of breaker tools.

High pressure pumps are capable of delivering high energy

S

levels per unit area. The apparently low powered laser watts) can deliver a heavy punch per unit area when the beam is focused down to 1/2 mm and below (similar to stilleto heeled shoes).

4 0

S

-11-

CRUSHING

Hematite/B.I .F.

TABLE 1 ENERGY REQUIREMENT ENERGY c.w. RESONIANT ENERkY Density 3.5t/m 3 Energy Requirement Reduced A Factor of Cube Dimension (m) 0.2 0.27 0.37 0.47 0.53 0.58 15 0.67 0,795 1 .145 1.26 1.355 1.44 1,59 2.15 Crushing Energy 9a 100 (3) 0* J.

I

S

SOUU

9u Ut, I U I U. I 90

U

b I

C,.

S

p&~

U

9 Wk) 42 1.05 2,62 5.25 7.87 12,25 15.7 26.25 52.5 78.7 105 131 157 210 525 42 105 262 525 787 1225 1575 2625 5250 7870 10500 13100 15700 21000 52500 14 35 87 175 262 408 525 875 1750 2620 3500 4370 5230 7000 17500 4.2 10.5 26.2 52.5 79 123 158 263 E25 787 1050 1310 1570 2100 5250 500 1000 (3) .84 .4 2. 1 1.11 5.2 2.6 10.5 5.3 15.7 7.9 24.5 12.2 31.5 15.8 52.5 26.2 1 05 52 158 79 210 105 262 131 315 157 420 210 1050 525 3000 .88 1.7 2.6 4 9 17 26 44 52 175 a as 8 Dashed area Is within 55W power range.

oil 0 1 1 9 b S -12- TABLE 2 ENERGY INPUT Per Blow Rammer 2000 Rammer 1600 High Pressure Pump 15,000 psi: f 35 Hz 10.000 psi; f 750 Hz .22 calibre bullet (Jou I es) 8200 6010 270 3.2 11.5 Per Sq Cm per Blow (JoulIes) 35.5 30.3 1280 Liser Focus f= 10,000 Hz f 5,000 Hz f 1,000 Hz 200~ .005 .011 .055 0 .5 mm 3 5 27 0.25 mm 11 22 110 SS~4

S

a 9* S

S

~S

S d S

C

OOMU 55

S

-13- TABLE 3 POWER INPUT Peak Power Peak Power Per Sq Cm kW kW Rammer 2000 Impulse Time (sec) 0.01 820 0.004 2050 8.9 0.002 4090 17.8 Rammer 1600 Impulse Time (sec) 0.01 840O 4.2 0.004 2100 10.6 0.002 4200 21,2 Hig-h Pressure Pump *15,000 psi: f 35 Hz 37.8 178 10,000 psi: f 750 Hz 9.6 135 .22 calibre bullet 410 1450 20 Laser Focus mm '0,25 mm f 10,000 Hz f =5,000 Hz 40 20x10 3 B0X10 3 f =1,000 Hz -14- Brief-DELscri1pt on of the DraJk~i.g These and other objects. advantages and novel features of the Invention will become apparent from the detailed description of the best mode for carryino out the preferred embodiment of the drawinas which follows, particularly when considered in conjunction with the accompanying drawings.

wherein: Fig. I Is a schematic view of the apparatus that Is used to carry out the method of this inventiont Fia. 2 is a schematic view of a mechanical energy input device and a fixed transducer: and Fla. 3 Is an Isolated view of the preferred eneroy pulsing member of this Invention.

0* 0* 00 -Is Best Mode for Carrving Out the Invention As can be seen by reference to the drawings, and In particular to Fig. 1, the apparatus that is employed In this invention is designated generally by reference numeral The apparatus (10) comprises In general a transducer unit an energy generating unit a vibration monitor unit an analyser unit a frequency control unit and a power control unit which are used to fracture a rock mass (100). These units will now be described in seriatim fashion.

As can best be seen by reference to Fig. 1, the transducer unit (11) comprises a fixed acoustic transducer member (17) that is operatively associated with the rock mass (100) to sense the vibration of the rock mass (100) over a small portion of the surface area of the mass (100).

The energy generating unit (12) of the preferred embodiment comprises a low powered pulsing laser member (18) wherein the power requirements of the laser member (18) is 1 9 approximately equal to 55 watts and, the laser beam <19) is 20 focused down to 1/2 mm or less.

The vibration monitor unit (13) comprises a remote vibration monitor member (20) such as the 55x Laser Doppler Vibrometer System manufactured by DISA Electronik of Denmark, wherein the output of the remote vibratioh monitor member (20) is transmitted by an electrical lead (50) to al9b analyzer unit Either the vibration monitor unit (13) is used in the circuit or the fixed transducer unit (11).

S.1. The analyzer unit (14) comprises an output frequency and amplitude analyzer member (21) which is connected by 6 electrical leads (50) to either the remote vibration monitor -16member (20) or the fixed transducer member (17) to measure the frequency and amplitude of vibration of the rock mass (100). In addition, the frequency and amplitude analyzer member (21) is operatively coupled as at (22) to the frequency control unit The frequency control unit (15) comprises an input frequency controller member (23) having a manual override wherein the Input frequency controller member (23) Is attached by electrical leads to a power control unit (16) in the form of a conventional power control member (25) and thence to the energy generator unit (12).

In the operation of the apparatus the operator would either employ the manual override (24) to vary the output of the energy controller member (23) relative to the frequency generator unit (12) until such time that 4 visual (201) or audio (202) Indications, such as sparks or cracking sounds were detected from the rock mass (100), or the output from the fixed transducer member (17) or the

S

remote vibration monitor member (20) are used to 20 automatically determine a change in the resonant frequency a of the rock mass (100) and the input frequency controller member (23) then adjusts the output of the energy generator unit (12) to match the new resonant frequency of the rock mass (100) to continue the rracturing process.

0' 25 Having thereby described the subject matter of this *0 Invention, It should be apparent that many substitutions, modifications, and variations of the Invention are possible In light of the above teachings. It Is therefore to be

S.

t t understood that the Invention as taught and described herein -17- Is only to be limited to the extent of the bceadth and scope of the appended claims.

OVO

0 -18-

Claims (7)

1. A method of fracturing a mass of material such as rock sing resonant frequencies wherein the method comprises the steps of: determining the resonant frequency of a mass of material: applying the determined value of the resonant frequency to a portion of the mass of material by a sub-ultrasonic frequency generating device to cause fracturing of the mass of material in the vicinity of the applied frequency: monitoring the mass of material for changes in resonant frequency; and applying the value of the applied frequency such that the applied frequency will coincide exactly with the sensed values of the new resonant frequency of the fractured a t mass of material. S

2. The method of Claim 1 wherein to achieve resonance a excitation of the mass of material, the pulse time in 20 seconds of the frequency generating device is limited to a maximum of 1 divided 2f, where f is the measured resonant frequency In cycles per second.

3. A method of Claim 2 wherein to achieve resonance S" excitation of the mass of material, the pulse frequ'ency of the energy generating device is lmlted to the measured resonant frequency,

4. The method of Claim 2 wherein to achieve resonance S excitation of the mass of material, the pulse frequency of S the energy generating device Is limited to the measured 0 resonant frequency divided by an Integer. 30 resonant frequency divided by an Integer. -19- I U An apparatus for fracturing a mass of material such as rock, using resonant frequencies wherein, the apparatus comprises: means for determining the resonant frequency for a given mass of material; non-contacting sub-ultrasonic frequency generating means for generating frequencies in the sub-ultrasonic range; means for monitoring changes in the resonant frequency of the mass of material as fracturing takes place; energy generating means; and, control means operatively associated with the means for monitoring or the non-contacting sub-ultrasonic frequency generating means for varying the output of the energy generating means in response to the input of the means for monitoring changes in the resonant frequency of the mass such that fracturing of the mass of material will continue.

6. The apparatus as in Claim 5 wherein the non-contacting sub-ultrasonic energy generating means comprises a laser.

7. The apparatus as in Claim 6 wherein the means for monitoring changes in the resonant frequency of the mass of material as fracturing takes place includes a remote vibration monitor and a transducer operatively associated with the said mass of material.

8. The apparatus as In Claim 7 wherein the control means comprises an output frequency and amplitude analyser operatively coupled to an input frequency controller, wherein the output frequency and amplitude analyser is responsive to the output from the remote vibration monitor or the transducer operatively associated with the mass of material and wherein the Input frequency controller varies the frequency of the non- contacting energy generating means. o Dated this 16th day of March, 1993. JOHN G. SELLAR WATERMARK PATENT TRADEMARK ATTORNEYS "THE ATRIUM', 290 BURWOOD ROAD, 55 HAWTHORN, VICTORIA 3122. S eo•• AU7399391.WPC DO0029