Fluid coupling drive system for a drill rig air compressor

Abstract

A drill rig includes a base, a drill tower coupled to and extending from the base, a drill pipe coupled to and supported by the drill tower, an air compressor coupled to the base, a prime mover coupled to the air compressor, and a fluid coupling disposed between and coupled to both the prime mover and the air compressor.

Claims

1. A drill rig comprising: a base; a drill tower coupled to and extending from the base; a drill pipe coupled to and supported by the drill tower; an air compressor coupled to the base; a prime mover coupled to the air compressor; a control system; and a fluid coupling coupled to and operated by the control system, wherein the air compressor is configured to be driven by the fluid coupling, wherein the fluid coupling is disposed between and coupled to both the prime mover and the air compressor, wherein the fluid coupling is a variable speed fluid coupling configured to have varying amounts of oil disposed therein to create variable speed control in the air compressor, wherein the prime mover is configured to operate at a constant speed regardless of the amount of oil in the fluid coupling, and wherein the control system is configured to increase and decrease the amount of oil in the fluid coupling throughout operation of the air compressor to drive the air compressor.

2. The drill rig of claim 1, wherein the fluid coupling includes an input pump and a separately spaced output turbine that both rotate about a shared axis and are separated by a gap inside the fluid coupling.

3. The drill rig of claim 2, wherein the fluid coupling is a hydrodynamic device that includes oil within the gap to transfer momentum from the input pump to the output turbine.

4. The drill rig of claim 3, wherein the prime mover is coupled to the input pump and is configured to cause the input pump to rotate, causing oil adjacent the input pump in the gap to rotate and to be pumped toward the output turbine, thereby causing the output turbine to rotate.

5. The drill rig of claim 2, wherein the air compressor includes a main rotor, and wherein the output turbine is coupled to the main rotor of the air compressor such that rotation of the output turbine causes rotation of the main rotor.

6. The drill rig of claim 2, further comprising an additional turbine disposed between the input pump and the output turbine.

7. The drill rig of claim 2, wherein the fluid coupling includes a lock-up structure that physically links and connects the input pump to the output turbine when the input pump is increasing in speed and reaches a predetermined speed threshold.

8. The drill rig of claim 7, wherein the predetermined speed threshold is 70% of a maximum operating speed of the input pump.

9. The drill rig of claim 7, wherein the lock-up structure includes a pad on at least one of the input pump and the output turbine that expands radially due to centrifugal force.

10. The drill rig of claim 7, wherein the lock-up structure eliminates slippage between the input pump and the output turbine at full operating speeds.

11. The drill rig of claim 1, wherein the air compressor is an oil flooded rotary screw air compressor having a main rotor that rotates about a first axis and a secondary rotor coupled to the main rotor that rotates about a second axis, and wherein both the main rotor and the secondary rotor are disposed within a stator housing.

12. The drill rig of claim 11, wherein the stator housing includes an air inlet port and an air outlet port, wherein the main rotor includes helical lobes and grooves along a length of the main rotor, and wherein the secondary rotor includes helical lobes and grooves along a length of the secondary rotor.

13. The drill rig of claim 1, further comprising a hydraulic pump coupled to and powered by the output turbine, wherein the hydraulic pump is separate from the fluid coupling.

14. The drill rig of claim 1, wherein the control system is configured to vary the amount of oil in the fluid coupling based on an amount of air needed for a given borehole.

15. The drill rig of claim 1, wherein the control system is configured to remove only a portion of the oil from the fluid coupling during a standby period of the air compressor, and to add oil back in to the fluid coupling after the standby period has passed, wherein the prime mover is configured to continue operating at its constant speed throughout the removal and addition of oil.

16. The drill rig of claim 1, wherein the control system is configured to increase and decrease the amount of oil in the fluid coupling throughout operation of the air compressor to drive the air compressor at varying speeds while the prime mover remains operating at its constant speed, wherein the control system is configured to increase and decrease the amount of oil in the fluid coupling to correspond to an amount of air needed for a given borehole, and wherein the control system is configured to remove at least substantially all of the oil from the fluid coupling during a standby operation of the drill pipe while the prime mover remains operating at its constant speed, and to add oil back into the fluid coupling after the standby period.

17. A method of operating an air compressor on a drill rig, the method comprising: varying an amount of oil within a fluid coupling that is coupled to both the air compressor and to a prime mover, wherein the fluid coupling drives the air compressor and the amount of oil in the fluid coupling is controlled via a control system; and while varying the amount of oil, maintaining a constant speed of the prime mover to generate slippage between an input pump in the fluid coupling and an output turbine in the fluid coupling, thereby creating variable speed control in the air compressor throughout operation of the air compressor.

18. The method of claim 17, wherein the method includes removing some of the oil from the fluid coupling when the drill rig is not drilling, thereby causing the output turbine and a main rotor in the air compressor to slow down.

19. The method of claim 18, wherein the method includes adding oil into the fluid coupling when the drill rig begins to drill, thereby causing the output turbine and the main rotor in the air compressor to speed up.

20. The method of claim 17, wherein the method includes removing all or substantially all of the oil from the fluid coupling during an extended shutdown period of the drill rig, thereby creating a disconnect between the input pump and the output turbine, and wherein during the extended shutdown period the prime mover continues to operate at the constant speed.

21. The method of claim 17, wherein the fluid coupling includes a lock-up structure that physically links and connects the input pump to the output turbine when the input pump is increasing in speed and reaches a predetermined speed threshold.

22. The method of claim 21, wherein the predetermined speed threshold is 70% of a maximum operating speed of the input pump.

23. The method of claim 21, wherein the lock-up structure eliminates slippage between the input pump and the output turbine at full operating speeds.

24. The method of claim 17, further comprising varying the amount of oil in the fluid coupling based on an amount of air needed for a given borehole.

25. The method of claim 17, further comprising removing only a portion of the oil from the fluid coupling during a standby period of the air compressor, and adding oil back in to the fluid coupling after the standby period has passed and continuing to operate the prime mover at its constant speed throughout the removal and addition of the oil.

26. The method of claim 17, further comprising: increasing and decreasing the amount of oil in the fluid coupling to correspond to an amount of air needed for a given borehole, and removing at least substantially all of the oil from the fluid coupling during a standby operation of the drill rig while the prime mover remains operating at its constant speed, and adding oil back into the fluid coupling after the standby period.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a side view of a drill rig according to one construction.

(2) FIG. 2 is a schematic view of an air compressor, prime mover, and fluid coupling of the drill rig of FIG. 1.

(3) FIG. 3 is a schematic view of the air compressor and the prime mover of FIG. 2, and a fluid coupling according to another construction.

(4) Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limited.

DETAILED DESCRIPTION

(5) With reference to FIG. 1, a blasthole drill 10 includes a drill tower 14, a base 18 (e.g., a machinery house) beneath the drill tower 14 that supports the drill tower 14, an operator's cab 22 coupled to the base 18, and crawlers 26 driven by a crawler drive 30 that drive the drill 10 along a ground surface 34. The drill tower 14 is coupled to and supports a drill pipe 38 (e.g., with a drill bit, not shown), which is configured to extend vertically downward through the ground 34 and into a borehole. In some constructions, multiple drill pipes 34 are connected together to form an elongated drill string that extends into the borehole.

(6) The drill 10 also includes leveling jacks 42 coupled to the base 18 that support the drill 10 on the surface 34, and a brace 46 coupled to both the base 18 and the drill tower 14 that supports the drill tower 14 on the machinery house 18. The drill tower 14 includes a drill head motor 50 that drives a drill head 54, and a coupling 58 that couples together the drill head 54 with an upper end of the pipe 38.

(7) With reference to FIGS. 1 and 2, the drill 10 further includes an air compressor 62 coupled to and disposed within the base 18 for flushing bit cuttings from the bottom of the borehole to the surface. In the illustrated construction, the air compressor 62 is an oil flooded rotary screw air compressor, although other constructions include different types of air compressors.

(8) As illustrated in FIG. 2, the air compressor 62 is a lubricant-injected, rotary screw compressor that includes a main rotor 66 that rotates about an axis 68 and a secondary rotor 70 that rotates about an axis 72, both the main rotor 66 and the secondary rotor 70 being disposed in a stator housing 74. The stator housing 74 includes an air inlet port 78 and an air outlet port 82. The main rotor 66 has helical lobes 86 and grooves 90 along a length of the main rotor 66, while the secondary rotor 70 has corresponding helical lobes 94 and grooves 98 along a length of the secondary rotor 70. Air flowing in through the inlet port 78 fills spaces between the helical lobes 86, 94 on each rotor 66, 70. Rotation of the rotors 66, 70 causes the air to be trapped between the lobes 86, 92 and the stator housing 74. As rotation continues, the lobes 86 on the main rotor 66 roll into the grooves 98 on the secondary rotor 70 and the lobes 94 on the secondary rotor 70 roll into the grooves 90 on the main rotor 66, thereby reducing the space occupied by the air and resulting in increased pressure. Compression continues until the inter-lobe spaces are exposed to the air outlet port 82 where the compressed air is discharged. Lubricant is injected into the stator housing 74 during the compression of the air. The lubricant lubricates the intermeshing rotors 66, 70 and associated bearings (not shown).

(9) With continued reference to FIGS. 1 and 2, the air compressor 62 is driven by a fluid coupling 102. The fluid coupling 102 includes an input pump 106 and a separately spaced output turbine 110 that both rotate about an axis 108, and are separated by a gap 112 inside the fluid coupling 102. As illustrated in FIG. 2, the output turbine 110 is coupled to the main rotor 66 of the air compressor 62, and the input pump 106 is coupled to a prime mover 114 (e.g., the flywheel of a diesel engine in the drill 10). In the illustrated construction, the fluid coupling 102 is a hydrodynamic device that uses oil within the gap 112 to transfer momentum from the input pump 106 to the output turbine 110. For example, when the prime mover 114 is activated, the prime mover 114 causes the input pump 106 to rotate, which causes oil adjacent the input pump 106 in the gap 112 to rotate and to be pumped toward the output turbine 110, thereby causing the output turbine 110 to also rotate. Rotation of the output turbine 110 causes rotation of the main rotor 66 in the air compressor 62.

(10) With continued reference to FIGS. 1 and 2, the fluid coupling 102 is optimally controlled with a control system 118. The control system 118 varies the amount of oil in the fluid coupling 102, while keeping the prime mover 114 operating at constant speed. Controlling the amount of oil in the fluid coupling 102 generates varying slippage between the input pump 106 and the output turbine 110, thereby creating variable speed control in the air compressor 62.

(11) The variable speed control of the fluid coupling 102 provides fuel and energy savings for the prime mover 114. For example, when a standby period occurs (i.e., when there is no drilling), the control system 118 removes some of the oil from within the fluid coupling 102, which generates greater slippage between the input pump 106 and the output turbine 110, and causes the output turbine 110 (and the main rotors 66, 70 coupled thereto) to slow down. When the standby period is over (i.e., when drilling resumes), the control system 118 adds oil back in to the fluid coupling 102, and the rotors 66, 70 are quickly brought back up to speed to resume compressing air at full speed. This ability to quickly bring the rotors 66, 70 back up to full speed reduces the amount of fuel and energy typically required to fully re-start the air compressor 62 every time a drilling operation occurs.

(12) In some constructions, the drill 10 experiences extended periods of standby during operation (e.g., when tramming the drill 10 long distance, during operator crew change, or in an arctic environment where the prime mover 114 is not shut down due to likely difficulty of restarting). In this situation the control system 118 removes all or substantially all of the oil from the fluid coupling 102, creating a disconnect between the input pump 106 and the output turbine 110. Once the oil is drained the output turbine 110 and the rotors 66, 70 remain stationary, but the input pump 106 continues to rotate (e.g., freewheels) due to its continued connection with the prime mover 114. Thus, the prime mover 114 simply continues to run at the same speed, without having to expend extra fuel to slow down or re-start itself.

(13) The variable speed control of the fluid coupling 102 also advantageously provides a soft-start option that allows the prime mover 114 to operate at a higher fuel efficiency when re-starting the air compressor 62. For example, when the output turbine 110 and the rotors 66, 70 of the air compressor 62 are still stationary, oil is slowly added to the fluid coupling 102, and the speed of the output turbine 110 and the rotors 66, 70 are gradually increased in a correspondingly slow, or soft, manner. This reduces the amount of fuel and energy typically required to start an oil flooded rotary screw compressor from standstill.

(14) In some constructions, the fluid coupling 102 also has the added feature of a lock-up structure or structures 122 that physically link and connect the input pump 106 to the output turbine 110 when the fluid coupling 102 is operating at full or near full operating speed (e.g., when the input pump is operating at 70% or more of a maximum operating speed). In some constructions, the lock-up structure is a collection of pads or other structures on the input pump 106 and/or output turbine 110 that expand radially due to centrifugal force to engage the other of the input pump 106 or output turbine 110 at high speeds and to lock in rotation of the input pump 106 with the rotation of the output turbine 110. Other constructions include different lock-up structures. The rotational locking of the input pump 106 to the output turbine 110 eliminates slippage between the input pump 106 and the output turbine 110 at full operating speeds, thereby optimally improving mechanical efficiency of the fluid coupling 102 and the air compressor 62 at these speeds.

(15) In some constructions, the fluid coupling 102 also reduces the need for venting of excess air in the air compressor 62 to the atmosphere (i.e., commonly referred to as blow-down). For example, it is common to vent excess air to the environment if an oil flooded rotary screw air compressor is too large for a given borehole, and there is too much air being generated by the oil flooded rotary screw air compressor for the given borehole. Such venting is often noisy and disruptive. By using a variable speed fluid coupling 102, the need to vent is reduced because the control system 118 can be used to slow down or speed up the output of the air compressor 62 as desired to more appropriately match the amount of air needed for a given borehole.

(16) The fluid coupling 102 additionally allows for continuous, smooth, and varying changes in the speed of the air compressor 62, without the use of additional wear parts (e.g., clutches like in the wet clutch system described above). This lack of additional wear parts provides for extended life of the fluid coupling 102 and the air compressor 62.

(17) The fluid coupling 102 also does not require additional pneumatic valves or a vacuum pump to be continuously powered to suck the air out of an outlet of the air compressor 62, as with the air control system described above.

(18) The control system 118 also has a much simpler control when controlling between high speed lock up operation and low speed start up and freewheeling disconnected operation, as compared with the control system for a wet clutch system or air control system.

(19) In some constructions, use of the fluid coupling 102 reduces fuel and energy consumption on a drill rig by as much as 50% as compared with a system that directly couples the prime mover 114 to the air compressor 62. This can result in hundreds of thousands of dollars of savings over the course of a year (e.g., 6000 operating hours) for a prime mover like prime mover (114).

(20) With continued reference to FIG. 2, in some constructions, the fluid coupling 102 is also, or alternatively, coupled to a hydraulic pump 130 (or other pump or device that may be driven by a prime mover and/or fluid coupling). In the illustrated construction, for example, the output turbine 110 is coupled to a power transfer transmission 134, which is coupled to the hydraulic pump 130, such that rotation of the power output turbine 110 powers the hydraulic pump 130. In some constructions the hydraulic pump 130 (or both the hydraulic pump 130 and the power transfer transmission 134) are coupled instead to the input pump 106 of the fluid coupling 102, such that rotation of the input pump 106 powers the hydraulic pump 130.

(21) With reference to FIG. 3, in some constructions, a torque converter fluid coupling 202 is used instead of the fluid coupling 102. The torque converter fluid coupling 202 is identical to the fluid coupling 102, except that an additional turbine 207 is provided between the input pump 206 and the output turbine 210. The additional turbine 207 redirects at least a portion of the flow of oil back to the input pump 206 for increased efficiency and torque amplification at high slip speeds. The torque converter fluid coupling 202 generates increased torque during start-up so that the prime mover 114 does not have to work as hard during start-up of the torque converter fluid coupling 202, thus providing even further fuel savings for the prime mover 114.

(22) Although the invention has been described in detail with reference to certain preferred embodiments, variations and modifications exist within the scope and spirit of one or more independent aspects of the invention as described.