The present invention relates to a rock drilling element for percussive rock drilling, a drill string and a method of transferring impact energy in a drill string according to the preambles of the independent claims.
Drilling straight holes to locate the explosives at the right place with good spacing and burden has always been considered as a must in the industry of drilling. It is quite easy to drill a straight hole with a down-the-hole machine whose percussion piston is located immediately on top of the drill bit. It is more difficult to ensure a straight hole with a top hammer machine where the percussion piston hits a drill string, including from 1 to 10 rods.
When there are particularly high safety demands on blasting, owing to the proximity of buildings, utility services or other installations, it is crucial for the blast holes to be drilled with the greatest possible precision. Indeed, high drilling precision is one of the most fundamental ingredients of a safe and accurate blasting result.
Drill rods are somewhat flexible, which basic specification allows them to drill through difficult rock at an acceptable deviation, but also with reasonable low fatigue stresses in the body and the connecting ends. This feature allows the drill rods to achieve a good service life and grants to the top hammer drilling a low cost per drilled meter.
The difficulty starts when the commonly achieved deviations are no longer tolerated. A better location of the explosives inside the rock body becomes compulsory. A better location of the explosives will also allow decrease of the amount of explosives per ton of blasted rock and can lead to substantial savings in explosives and in secondary breaking.
Many means to improve the hole straightness with top hammer drilling have been developed over the years. The two most common means are: guide bits and guide tubes. Guide bits are provided with up to 6 or 8 splines on the external part of the skirt. The splines are the means to improve the guiding inside the drilled hole, but they inevitably wear out, by far earlier than the carbide buttons crushing the rock into cuttings. After some while, the drill bit is still able to drill, but the guiding means have vanished. Guide tubes, such as disclosed in U.S. Pat. No. 6,681,875, have external diameters close to the drill bit diameter. The very high rigidity of the guide tube tends to keep the drill bit straight in line. Unfortunately, the penetration rate slows down by 10 to 20%. In addition, a guide tube does not withstand the percussion power over a long period of time and inevitably breaks at the connection to the drill bit, or forces the upper rod connected to it to break. The resulting drilling costs are usually considered as excessive, and guide tubes are not well accepted in the field.
Other common guide systems have short splines that wear out quickly, and the expected improvement in guiding the drill bit becomes very quickly ineffective.
One object of the present invention is to provide a drill string having an efficient and long lasting guide means.
Another object of the present invention is to provide a rock drilling element that avoids over-stressing of the thread joint connecting to the drill string.
Still another object of the present invention is to provide a rock drilling element designed with a relatively low linear weight for a high efficiency of the shock wave transmission.
These and other objects have been achieved by a rock drilling element, a drill string and a method of transferring impact energy in a drill string such as defined in the subsequent claims with reference to the drawings.
The basic idea for the guide rod or rock drilling element 10 according to the present invention is to avoid at best any stress concentration at a thread joint, which inevitably occurs with the heavy guide tubes as experienced in prior art solutions such as U.S. Pat. No. 6,681,875. The stress concentration in a conventional guide tube is depicted in
Regarding compressive shock waves: The heavier linear mass of the guide tube 2, at least 105-250% of the linear mass of the drill string itself, reflects part of the incident shock wave 4A energy back to the drill string and to the drilling machine, as a result of the so-called anvil effect. Therefore, the first rod 1 connected to the guide tube 2, and more specifically its male threaded spigot, suffers from a local increase of the compressive stress level. This phenomenon will be described further in detail below, with reference to
Regarding rotation mean torque and torsional waves: The lower inertia of the drill string versus the higher inertia of the tube section of the guide tube 3 is sensitive to the constant mean torque and the torsional waves traveling along the drill string. The drill rod 1, and more specifically the male thread of the drill rod, develops high torsional stresses at each impact, when carbide buttons of the drill bit impact on the rock formation.
Regarding static bending stresses: For a given angular deviation of the hole, not shown, the bending stresses can be smoothened out on both sides of a thread joint between two adjacent somewhat flexible rods. The case is fundamentally different when one part is a rigid guide tube 3. Because of the rigid guide tube, it can be assumed that the bending stresses induced in the male spigot of the rod 1 directly connected to a guide tube can almost be doubled relative to stresses developed in a rod-to-rod thread joint.
All the above-mentioned stresses (percussion, rotation, bending) are combined into a resulting stress distribution, which local excessive value will initiate fatigue failures and will result in full breakage.
At time t=−1, the shock wave 4A, shown in its entire length, which means twice the length of the impact piston, travels along the rod 1 towards the right-hand side of
At time t=0, the incident shock wave abuts on the heavier tube section 2.
At time t=1, because of the heavier linear mass, the incident shock wave 4A is split into a transmitted wave 4C traveling through the tube 2 and a reflected wave 4B of same length traveling back towards the drilling machine. The more or less dense hatching reflects the stress amplitude in both transmitted 4C and reflected 4B waves.
The shock wave is defined by its stress level and the pulse length. A high stress level (typically 200 MPa) is shown with a dense hatching at time t=−1 before the wave abuts on the heavier tube 2. The stress level is slightly lower, and thus the hatching is less dense after the wave travels into the tube section. The reflected wave 4B is depicted by a very loose hatching, inclined in another direction as a symbol of a wave traveling towards the left-hand side in
At time t=2, the first half (50%) of the incident shock wave 4A is transmitted and reflected.
At time t=3, the incident shock wave 4A travels to the right and the length of the rod subjected to high stress level is shorter than before. For sake of simplicity and in order to minimize the number of figures, the transmitted wave 4C traveling to the drill bit now abuts on the rock. The reactions at the drill bit 3 are very variable, depending on the drill bit weight and rock hardness. It is assumed that the drill bit of same linear mass as the tube section is used, and that the rock to be hard enough to withstand the drill bit motion and bit pressure. A second reflected compressive shock wave will then be initiated.
At time t=4, the incident shock wave 4A is fully transmitted into the tube section, and therefore, the creation of the stress wave 4B comes to an end.
At time t=5, the reflected wave 4B is completed and travels to the left-hand side towards the drilling machine.
The most unfavorable time for the thread joint 5 is from time about t=0 to about t=4, when incident 4A and reflected 4B stress waves are superimposed.
For example, if an incident shock wave is 200 MPa, and the reflected shock wave 4B is 40 MPa (only 20%) resulting from the higher tube impedance, then the resulting stress level is 240 MPa. As a matter of comparison, the 240 MPa stress level would develop in a regular rod-to-rod thread joint not shown, at a drilling machine with a 44% higher energy per impact (E), as a result of the formula:
E=∫σ2.dt
where σ is the compressive stress.
The conventional drill string cannot withstand a 44% increase in energy per impact. The thread joint between drill rod and guide tube, subjected to a 44% higher stress, has proven to be the weak point of the drill string. The fatigue cracks usually develop in the thread joint 5, and more precisely in the male thread, limiting the life of the two components to the range of 800 to 2500 drilled meters. It should be noted that a standard rod-to-rod thread joint is able to drill from 10 000 to 20 000 drilled meters. Such rod and guide tube lives are commonly recorded on jobsites.
The object of the present invention is to avoid the higher stress level that currently occurs in any thread joint between the drill rod and the guide rod.
An embodiment of a drill string according to the present invention for percussive rock drilling comprising a guide rod 10 according to the present invention is described hereinafter with reference foremost to
A flushing channel which is generally depicted 19 extends internally of the guide rod 10, through which a flush medium, usually air or water, is transferred. The through-going flush channel 19 is provided to lead flush medium to the rock drill bit 3 for percussive top hammer drilling. This channel is suitably centrally positioned in the guide rod.
The slender portion 10A and the guide portion 10B are preferably essentially cylindrical. A first shoulder 25 and a second shoulder 26 border the cylindrical part of the slender portion 10A at respective axial ends thereof. The first shoulder 25 is provided in the vicinity of the female thread 16.
At time t=−1, t=0 and t=1, the thread joint 5 is subjected to the incident shock wave 4A, similar to any thread joint between two standard rods.
At time t=2, the incident shock wave 4A has already ended and the stress level is close to zero. This feature occurs before the reflected shock wave 4B reaches the thread joint 5 in opposite direction.
At time t=3, t=4 and t=5, a harmless reflected wave 4B travels across the thread joint 5, having no noticeable Influence on the guide rod 10 life.
The basic idea for the guide rod 10 according to the present invention is to keep the end part or the part of the guide rod facing away from the drill bit 3 as identical as possible to the drill rod 1 connected to it, and therefore to avoid the negative influence of a 105% to 150% heavier linear mass of the conventional guide tube, enhancing locally compressive, rotation and bending stresses. In order to avoid any increase of the compressive stresses resulting from the impact pulses in the thread joint 5, which is the most sensitive portion, this slender portion 10A of the guide rod 10 should have a length equal to or preferably longer than the impact piston, which means the length of the slender portion 10A should be at least 500 mm. This slender portion 10A simultaneously smoothens the torque pulses and the bending stresses before those are conveyed towards the thread joint 5 and conveyed into the very sensitive male thread of the rod 1 connected to it.
The guide portion 10B of the guide rod is a tubular section acting as a bearing in contact with the hole wall to improve the guidance of the drill bit 3. The major reason for defining a tubular section instead of for example six long splines is deducted from field experience, that is guide tubes are considered to be less aggressive in overburden drilling and in soft rock drilling, while six splines may deteriorate the wall and drive the hole to collapse. This second portion 10B is preferably carburized or heat-treated, to withstand high wear because of heavy friction against abrasive rock, to a surface hardness between 48 HRC and 62 HRC. The second portion 10B may comprise external shallow splines in order to increase the flushing area and simultaneously decrease the clearance between splines and hole wall, for an improved guidance.
The method according to the present invention for transferring impact energy from a top hammer unit to a drill bit can be summarized as follows. The top hammer unit has a piston that provides shock waves 4A. Each shock wave has a length 2L. The method comprises the steps of:
providing a drill string comprising one or more extension rods 1 or extension tubes, a rock drilling element 10 as defined above, and a drill bit 3 or one or more guide tubes connected to a drill bit 3,
connecting an end 11 of said rock drilling element 10, 10′ facing towards the piston via a thread joint 5 to an extension rod 1 or an extension tube,
accelerating the piston,
impacting an end of the drill string to create the shock wave 4A,
allowing more than half of the shock wave 4A to pass the thread joint 5 before any reflected wave 4B is allowed to be created, and
rotating and impacting said drill bit against a rock material for making a hole therein.
The second portion 10B can in addition be altered in length, in order to optimize the shock wave transmission to the drill bit and to the rock. An alternative guide rod 10′ according to the present invention is shown in
In light of the description related to
In a computer simulation test, the efficiency of shock wave transmission has improved from 0.7245 (with a conventional full length guide tube) to 0.7677 (with optimized guide portion 10B′ length), which is almost a 6% improvement of energy transfer.
It should be noted that optimizing the shock wave transmission is not compulsory. A somewhat or even a much longer guide portion for improved guiding inside the hole (but not optimized with regard to energy transfer) can be designed to solve different drilling situations. For example, when the straightness of the hole is of a higher priority than the penetration rate. Such a guide rod would still take advantage of the lower compression stresses, more even rotation stresses and more even bending stresses in the thread joint 5 that will highly benefit the drill string life.
Such a guide rod 10 and 10′ is designed to accept conventional drill bits with a skirt and a female thread. The drill bit 3 can have either a standard skirt or a guide skirt. The above-mentioned embodiments of a guide rod according to the present invention preferably has a peripheral contact (also called shoulder contact) between the guide rod 10, 10′ and the drill bit 3. The major reason for having the shoulder contact around a large thread is to provide the shock energy precisely where it is going to be useful at the peripheral buttons of the drill bit.
The drill bit 3 can alternatively be designed with a male threaded spigot to be inserted inside the guide rod having a corresponding female thread. A carburized guide portion able to withstand high wear can in this context be the sole means for guiding inside the hole, such that the drill bit 3 needs no integral guiding devices.
The guide rod has been shown up to now with a bit directly connected to it. It is also possible to use the guide rod as an intermediate element connecting together two drill string sections of different cross-sectional area (in mm2) or linear mass (in kg/m). For example, a 60 mm drill rod delivers the impact pulses to the guide rod, which in turn is connected to one or more guide tubes with heavier linear mass. The drill bit 3 is finally connected to the last guide tube.
The drill string of rods could alternatively be a string of drill tubes wherein the guide rod 10, 10′ then is replaced by a guide tube of similar geometry but with greater dimensions. Such a guide tube should be essentially identical to the drill tubes in its upper end, and have a larger and heavier tube at its lower end to suit the drill bit diameter.
The present invention proposes a guide rod where the thread joint is moved away from the unfavorable reflection area. Thereby, several advantages are obtained, namely an efficient and long lasting guide means that avoids over-stressing of the thread joint connecting to the drill string and a high efficiency of the shock wave transmission.
Although the present invention has been described in connection with preferred embodiments thereof, it will be appreciated by those skilled in the art that additions, deletions, modifications, and substitutions not specifically described may be made without departing from the scope of the invention as defined in the appended claims.
Number | Date | Country | Kind |
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0501054-1 | May 2005 | SE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/SE2006/000536 | 5/3/2006 | WO | 00 | 5/30/2008 |