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DEM modeling of ice cuttings transportation by electromechanical auger core drills

Published online by Cambridge University Press:  26 July 2017

J. Hong
Affiliation:
Polar Research Center, Jilin University, Changchun, China E-mail: ptalalay@yahoo.com
P. Talalay
Affiliation:
Polar Research Center, Jilin University, Changchun, China E-mail: ptalalay@yahoo.com
M. Sysoev
Affiliation:
Polar Research Center, Jilin University, Changchun, China E-mail: ptalalay@yahoo.com
X. Fan
Affiliation:
Polar Research Center, Jilin University, Changchun, China E-mail: ptalalay@yahoo.com
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Abstract

Electromechanical auger core drills are widely used in shallow ice-coring practice on mountain glaciers and polar ice caps and sheets. Generally, these drills are lightweight, can be readily transported to remote drilling sites, are easily installed there and drill with relatively high rates of penetration and low power consumption. During the past few decades, dozens of electromechanical auger drills have been designed. However, the auger options were usually determined by experience, and the main parameters (auger angle and rotation speed) are varied in a wide range from drill to drill. In order to choose the optimal auger parameters, the discrete element method (DEM) is used to analyze the performance of cuttings transportation for different rotation speeds in the range 50–200 rpm and auger angles in the range 15–45°. To improve the efficiency of cuttings transportation, many factors have to be considered (e.g. particle sizes and their variability, ice temperature, material of the core barrel and jacket, and availability of needed driven motor-gears). For the conditions assumed in the present studies, the recommended rotation speed is 100 rpm at auger angles of 35–40°.

Keywords

Type
Research Article
Copyright
Copyright © International Glaciological Society 2014

Introduction

Shallow drilling in ice sheets and glaciers down to 300–350 m depth has valuable applications for glacier structure, composition and thermodynamics study and for research into current climate variability (e.g. inter-hemispheric relationships and the timing and expression of the Little Ice Age). These tasks were included in the project ‘2 k Array’ for the next decade or more of the ice-core community under the auspices of International Partnerships in Ice Core Sciences (IPICS; http://www.pages-igbp.org/ipics/). Electromechanical auger core drills are widely used in ice shallow-coring practice given their obvious advantages: (1) they are lightweight and can be readily transported by helicopter; (2) power consumption is relatively low compared with commercial rotary drill rigs and cable-suspended thermal core drills; and (3) auger drills are more environmentally friendly as they do not need to use a drilling fluid.

The main feature of electromechanical auger drills is that the rotating core barrel with helical flights on the outer surface is used to transport ice cuttings from the drill head to the imbedded chip chamber. The upper part of a typical drill includes (Fig. 1): (1) cable termination to connect the drill with the armored cable; (2) in most drills, a slip-ring device to prevent cable damage when the anti-torque fails, and a rotation sensor to detect anti-torque failure during penetration; (3) an anti-torque system to prevent spinning of the non-rotated section; (4) in some drills, a hammer to ease core breaking and retrieve a sticking drill; and (5) not always, a pressure-resistant instrumentation chamber, containing the sensors and controls.

Fig. 1. Basic structure of ice shallow drill: 1. cable; 2. cable termination; 3. anti-torque leaf springs; 4. motor with reducer; 5. clutch; 6. shaft; 7. booster; 8. rotating core barrel; 9. jacket; 10. drill head; 1 1 . cutters.

The lower part of the electromechanical auger drill includes: (1) a coring head equipped with cutters and core catchers; (2) a core barrel with spiral flights and chip chamber; (3) in most drills, a jacket; and (4) a geared motor. Torque limiters (friction clutch) were included in some drill designs. Some methods to increase friction between cuttings and the inner surface of the jacket (e.g. ribs or grooves) are provided in most of the drills.

The original concept of an electromechanical auger drill was based on the SIPRE hand auger driven by a suspended motor with an anti-torque device (Reference SuzukiSuzuki, 1994). Two such drills were built by Japanese experts in the early 1970s and tested at Mizuho station, Antarctica, in 1971 and at Ice Island T-3, Arctic Ocean, in 1973. At the same time, another auger drill was built at the University of Iceland, Reykjavík, and used in summer 1972 to drill a 415 m deep hole on Vatnajökull, Iceland (Reference Árnason, Björnsson and TheodórssonÁrnason and others, 1974). Shortly afterwards, two other drills were designed at the University of Bern, Switzerland, by H. Rufli (Reference Rufli, Stauffer, Oeschger and SplettstoesserRufli and others, 1976) and at the US Army Cold Regions Research and Engineering Laboratory (CRREL) by J. Rand (Reference Rand and SplettstoesserRand, 1976). The last two drills became for a long time excellent prototypes for electromechanical auger drills development, so this type of drill was often referred to as the ‘Rufli–Rand drill’.

Dozens of electromechanical auger drills have been designed during the past few decades, yet one of the first holes on Vatnajökull is still recognized as the deepest hole drilled by this type of drill. The borehole at Vatnajökull was filled with drained water (Reference Árnason, Björnsson and TheodórssonÁrnason and others, 1974). The details of the various internal components give each electromechanical auger drill its own unique operating capacities. However, the auger options were usually determined by experience, and the main parameters (auger angle and rotation speed) are varied in a wide range from drill to drill (Table 1).

Table 1. Main auger characteristics of shallow electromechanical drills

Inability to promptly remove the cuttings results in their being pulverized into progressively finer particle sizes, making drilling very inefficient, and in extreme cases halting the drilling process altogether, resulting in cutters icing, abnormal power consumption and high rotation torques (Reference Zacny and CooperZacny and Cooper, 2007). This paper presents research on ice auger transportation based on the discrete element method (DEM) which is able to analyze the performance of cuttings transportation depending on different operating conditions (auger angle and rotation speed) in terms of average particle velocity, average particle axial velocity, mass flow rate, average height of particle transportation, average particle unit mass, dissipated energy and energy distribution.

Model Description

The main elements of the auger conveyer are (Fig. 2):

  1. D 1: auger inner diameter (ID) equal to the outer diameter (OD) of the core barrel;

  2. D 2: auger OD or diameter of flights;

  3. α: auger angle determined by the angle between the tangent to the flight helical line and a horizontal line;

  4. p: pitch equal to the width of one complete helix turn measured parallel to the auger.

Fig. 2. Parameters of three-flight auger.

Auger angle is slightly changed from α1 estimated on the auger ID to α 2 on the OD:

(1)

where D is the diameter (m) at an arbitrary point of the flight (D 1 ≤ D ≤ D 2).

Augers are often used for transporting, elevating or mixing particles at controlled and steady rates in agriculture or food processing (Reference Owen and ClearyOwen and Cleary, 2009) and are employed in pile foundation engineering (Reference Tan, Duan, Tan and ShiTan and others, 2011). Although the structures of augers differ, the principles applied in transporting cuttings or particles are always similar. Surprisingly, calculations based on the theory of auger transportation for soils suggested by Reference Bashkatov and OlonovskyBashkatov and Olonovsky (1968) gave very small optimal auger angles (7.5–12°) for transportation of ice cuttings, contrary to field experience (Reference Hong, Talalay and SysoevHong and others, 2014). This was a reason for undertaking this research and use of the DEM method to predict the performance of ice cuttings transportation by coring auger.

DEM simulations involve following the motion of every particle (coarser than some cut-off size) and modeling each collision between the particles and between the particles and their environment (e.g. the internal surface of the stationary jacket, the surface of the rotating core barrel and the surface of the flights). The boundary geometry is built using a CAD software package imported as a triangular surface mesh into the DEM software package. This provides unlimited flexibility in specifying the three-dimensional geometries with which the particles interact (Reference Owen and ClearyOwen and Cleary, 2009).

The following considerations and parameters of the coring auger are applied to the simulation. The auger has three 5 mm wide flights at constant helix angle. The core barrel with an OD of 108 mm is modeled as a solid tube to keep cuttings in the gap between the core barrel and the jacket with ID/OD of 119/125 mm. The clearance between the auger flights and the inner surface of the jacket is 0.5 mm. A solid ring imitates the bottom of the hole to prevent falling-down of the cuttings from the flights due to gravitational force. A series of DEM simulations was carried out for different rotation speeds in the range 50–200 rpm and auger angles in the range 15–45° (Table 2). Since the processing time for each numerical experiment using a workstation based on an Intel Xeon E5-1650 processor was up to 4 months, the simulation time had to be limited to 0.4–1.0 s (the slower the rotation speed, the longer the simulation time).

Table 2. Selected and calculated auger operating parameters

The size analyses of the particles produced by the KEMS-112 electromechanical drill with air reverse circulation suggested that the ‘cold’ ice cuttings had an isometric shape that could be approximated by a ball (Reference TalalayTalalay, 2006). In these DEM simulations, it is assumed that the maximum size (diameter) of the ice particles is approximately equal to the depth of cut:

(2)

where ROP is the rate of penetration (in all simulations ROP = 20 m h−1), n is the drill head rotation speed (rpm) and m is the number of cutters (m = 3). The particle sizes follow a normal distribution.

The mass of cuttings Q (kg s−1) produced per unit time by the drill head is estimated as

(3)

where ρ is the density of drilled ice (ρ = 920 kg m−3) and d 2 and d 1 are the OD/ID of the drill head (d 2 = 0.129 m; d 1 =0.1 m).

The particle-to-particle (ice-to-ice) friction is taken as 0.1, that of particle to core-barrel (stainless steel) as 0.17, that of particle to flight (nylon) as 0.21 and that of particle to inner surface of the jacket (aluminum grooved tube) as 0.24.

Cuttings Distribution Along the Auger

Figure 3 illustrates the cuttings distribution along the coring auger during transportation. The first row shows the particle distribution at a rotation speed of 50 rpm with the angle varied from 15° to 45° in steps of 10°. The rotation speed increases from 50 rpm to 200 rpm from the first row to the last (seventh) row in steps of 25 rpm. The cuttings are colored depending on their diameter, with the smaller particles being brighter and the larger particles darker.

Fig. 3. Cuttings distribution along coring auger.

At low rotation speeds (50 and 75 rpm) the particles are aligned with the auger flights at the slight angles of 15° and 25°. If the auger angle increases (35° and 45°), a cuttings build-up is formed near the bottom of the coring auger, indicating that the lifting force between cuttings and jacket is not enough to transport particles at these operating parameters.

At a rotation speed of 100 rpm, cuttings are transported smoothly without a build-up forming; however, at the highest auger angle of 45°, particles start to fall down in the clearance between the flights and the jacket. With a further increase in rotation speed, there is little evidence that cuttings form a build-up, but the number of cuttings that drop into the clearance between the flights and jacket increases. The particle sizes as shown by Eqn (2) decrease with increasing rotation speed and are smaller than the clearance between the flights and jacket (0.5 mm) at rotation speeds higher than 125 rpm. Downfallen particles need to be re-transported and can accumulate near the bottom, causing packing, increasing power consumption and finally a halt to cuttings transportation.

The results of cuttings distribution analysis show that there are two main types of particle transportation: an ordered track generated at lower rotation speeds, and a disordered track at rotation speeds higher than 125 rpm when cuttings are in a muddle along the auger. Comparing the rows in Figure 3, it is worth noting that the efficiency of cuttings transportation increases with increasing rotation speed. Comparing columns, it may be concluded that the efficiency of cuttings transportation increases with increasing auger angle.

Results

The performance of cuttings transportation is studied in terms of the following parameters:

  1. 1. Average particle velocity (AV), which refers to the total velocity in three-dimensional space to describe how fast the cuttings move;

  2. 2. Average particle axial velocity (AAV), which refers to the velocity in the upward direction and relates to the vertical movement ability of the particles;

  3. 3. Mass flow rate (MFR), determined by recording the mass of each particle that has passed through a plane perpendicular to the axis of the screw (this plane is located halfway between the two periodic boundaries which are borders of a pitch; Reference Owen and ClearyOwen and Cleary, 2009);

  4. 4. Average particle height (AH), which refers to the transportation height of particles to calculate the auger volumetric removal efficiency and to demonstrate its capability more clearly than velocity;

  5. 5. Average particles unit mass dissipated energy (AE), which refers to the energy consumed by 1 kg of particles being transported along the coring auger;

  6. 6. Energy ratio (ER), which indicates the ratio between particle kinetic energy and potential energy (if the kinetic energy of a particle is equal to its potential energy, ER= 1).

The AV marginally increases with increasing auger angle at low rotation speed (≤75 rpm) and increases more rapidly when the rotation speed exceeds 100 rpm (Fig. 4). At high rotation speed and steep helix angle (45°), the AV decreases. The variation of the AV with auger angle is smaller than the change due to the increase in rotation speed.

Fig. 4. Average particle velocity (AV) vs auger angle.

The AAV trend is almost the same as AV (Fig. 5). The only difference is the curve shape at a rotation speed of 50 rpm in which AAV decreases more rapidly with increasing auger angle. This implies that, at low rotation speed, increasing the auger angle is an ineffective method to speed up the upward movement of the particles.

Fig. 5. Average particle axial velocity (AAV) vs auger angle.

At first, the MFR rapidly increases with increasing auger angle and then starts to decelerate (Fig. 6). The turning point depends on the rotation speed: when the auger rotates at 50 and 75 rpm, MFR stabilizes at 30°; at 100 rpm at 35°; and at 125 and 150 rpm at 40°. The MFR at rotation speed >125 rpm and auger angle of 45° increases sharply, probably because disorder in the cuttings tracks causes some particles to pass the same plane many times. The MFR at a rotation speed of 50 rpm is lower than the others, which is in agreement with the slowest AAV.

Fig. 6. Mass flow rate (MFR) of particles vs auger angle.

The AH increases at the start and then becomes almost stable at certain auger angles depending on rotation speed: when the auger rotates at 50 rpm, AH stabilizes at 25°, and at 75 rpm at 35°, while at other rotation speeds AH starts to decelerate at 40° (Fig. 7). The variation of AH with auger angle is much smaller than the change due to increasing rotation speed, and the trend is almost the same as AAV.

Fig. 7. Average height (AH) of particle transportation vs auger angle.

The AE increases monotonically with increasing auger angle and rotation speed (Fig. 8). The variation of AE with auger angle is much smaller than the change due to increasing rotation speed. With rotation speed rising, the intensity of AE growth also rises, probably because of increased disordering of the cuttings tracks, which increases the kinetic energy of the particles.

Fig. 8. Average particles unite dissipated energy (AE) vs auger angle.

The ER variations indicate that the portion of particle kinetic energy increases with increasing auger angle and rotation speed (Fig. 9). This is the main reason why AE increases with auger angle and rotation speed. The disordering of the particle tracks at large auger angle and high rotation speed consumes much more energy than regular transportation of cuttings.

Fig. 9. Energy ratio (ER) of particles vs auger angle.

Conclusions and Discussion

DEM simulation shows that the nature of cuttings transportation in a coring auger is complex and sensitive to the operating parameters. Considering the size of cuttings we can draw the following conclusions.

At low rotation speed, cuttings accumulate at the lower end of flights. At higher speed (≥100 rpm), chip transportation is more efficient.

Assuming that particle size decreases with increase in rotation speed, more and more particles fall into the clearance between the flight and the jacket, with rotation speed increasing, resulting in a need for them to be transported over again. Cuttings transportation is more efficient if the particle size is larger than the clearance between the flight and the jacket. Therefore generation of coarser cuttings should be considered when selecting the operating parameters (in the first instance, depth of cut and rotational speed) and shape of cutters. On the other hand, the clearance between the flight and the jacket has to be as small as possible. This depends on the coaxiality of the core barrel and jacket and the straightness of the tubes used to manufacture the core barrel and jacket, which is usually longer.

Maintaining an ordered track for the particles is an important factor in increasing transportation efficiency and energy saving. The reason why the cuttings tracks become disordered is probably that the clearance between the flights and jacket is larger than the diameter of the particles at high rotational speeds or that the weight of the particles is too light and the track easily becomes unstable at high rotation speed.

To choose optimal parameters for a coring auger, many factors have to be considered (e.g. particle sizes and their variability, ice temperature, material of core barrel and jacket and others, and the availability of the needed drive motor-gears). For the conditions assumed in the present study, the critical rotation speed between ordered tracking and disordered tracking is near 100 rpm at auger angles of 35–40°, and in conjunction with a comprehensive evaluation of various transportation characteristics (AV, AAV, AH, AE, ER) these values can be recommended as the optimal auger parameters.

Acknowledgements

This paper presents the results of research supported by the ‘Recruitment Program of Global Experts’ established by the organizing department of the Central Committee of the Communist Party of China and the National Science Foundation of China (grant No. 41327804). We thank Victor Zagorodnov (The Ohio State University, USA) for fruitful suggestions. We also thank George Cooper (University of California, USA) for editing.

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Figure 0

Fig. 1. Basic structure of ice shallow drill: 1. cable; 2. cable termination; 3. anti-torque leaf springs; 4. motor with reducer; 5. clutch; 6. shaft; 7. booster; 8. rotating core barrel; 9. jacket; 10. drill head; 1 1 . cutters.

Figure 1

Table 1. Main auger characteristics of shallow electromechanical drills

Figure 2

Fig. 2. Parameters of three-flight auger.

Figure 3

Table 2. Selected and calculated auger operating parameters

Figure 4

Fig. 3. Cuttings distribution along coring auger.

Figure 5

Fig. 4. Average particle velocity (AV) vs auger angle.

Figure 6

Fig. 5. Average particle axial velocity (AAV) vs auger angle.

Figure 7

Fig. 6. Mass flow rate (MFR) of particles vs auger angle.

Figure 8

Fig. 7. Average height (AH) of particle transportation vs auger angle.

Figure 9

Fig. 8. Average particles unite dissipated energy (AE) vs auger angle.

Figure 10

Fig. 9. Energy ratio (ER) of particles vs auger angle.