This application is the U.S. national phase of PCT Appln. No. PCT/AU2011/001190filed on 15 Sep. 2011, which claims priority to Australian Patent Appln. No. 2010904234filed on 20 Sep. 2010, the disclosures of which are incorporated in their entirety by reference herein.
This invention concerns a reamer for underground passageways made, for instance, for the installation of cables or pipelines to distribute services in a reticulated network.
Smaller underground passageways for cables and pipes are generally created by first drilling a pilot hole with the use of a drill string. Once both the near and far ends of the pilot hole are open, a reamer is attached to the drill string, at either the near or far end. Then the reamer is forced along the length of the hole while spinning to enlarge it to the required diameter; depending on the size of the pipe or cable to be installed.
Several reamers of gradually increasing sizes may be used, depending on the required final diameter. A number of variations are possible, for instance the reamer can be pushed through the hole (forward reaming) or drawn backwards through (back reaming).
Referring now to
While travelling through the hole, for instance in the direction indicated by arrow 18 the reamer is rotated by the drill string in the clockwise direction (anticlockwise from behind as shown by arrow 20). It is the rotation of the wings that enlarges the hole.
The main problem with reamers with wings fixed by welding is they cannot be easily repaired on site. Satisfactory repairs can only be undertaken in a well equipped engineering workshop. This presents another difficulty in that it is extremely difficult to achieve the axial run out tolerances required in a fabrication process. As a later development, reamers with wings bolted into cylindrical body or inner shaft with fixed datums were expected to overcome these problems. However, what occurred with reamers of this kind was that, in use, the bolts 22 were placed under high torsional load and were able to work loose, causing the wings 14 to deflect. This type of deflection increases the diameter of the reamer and makes it susceptible to binding in the hole; which can lead to loss of the reamer and drill string; and sometimes abandonment of the hole. Another problem is that the reamer may not be well stabilised in the hole. This causes vibration which further exacerbates the binding problem.
As a result the wings 14 that are welded or bolted to the cylindrical body 12 often utilize a stabilizing ring 24 which is welded to the tips of the cutting wings 14. Welding the wings to a stabilizing ring has two functions:
This effectively makes them fixed wings and removes the facility to replace the cutting wings 14 in the field. Consequently, it requires them to be returned to a workshop to carry out repairs.
The invention is a reamer for underground passageways, comprising:
The cutting wings may engage with the other components releasably to enable the wings to be replaceable in the field without the need to return the reamer to the workshop.
In addition, the cutting wings may engage with respective support pillars of the stabilization ring to resist relative rotation between them.
A plug may be used to connect the stabilization ring to the support housing and retain the circular sleeve in engagement with the cutting wings.
The plug may capture the central collar of the stabilization ring when it connects it to the support housing.
The engagement between the cutting wings and the support housing that resists rearward longitudinal movement may, in each case, comprise a flange extending from the wing that enters a recess in the bottom of the longitudinally extending slot.
The engagement between the cutting wings and the support wings that resists torsional forces may rely on a close fit between them and the use of bolts to interconnect the cutting wings with their respective support wings. For this purpose there may be bolt holes in the cutting wings that align with bolt holes in the support wings when the reamer is properly assembled. In one example there are four cutting wings fitted into four respective slots, and there are four pairs of support wings that are bolted to the cutting wings with two bolts each.
The engagement between the cutting wings and the circular sleeve of the stabilizing ring that resists radial movement may involve a step at the rear of each cutting wing that receives the front of the circular sleeve. In this way the circular sleeve overlies a rear flange of the cutting wings.
The engagement between the cutting wings and the support pillars may involve a flange in one entering a closed slot in the other.
There may be four pairs of support wings, four cutting wings and four support pillars.
Each of the support pillars of the stabilization ring may be penetrated by a bolt hole which aligns with a bolt hole in the support wings when the reamer is assembled, so that they can be bolted together.
The cutting wings may be sized for various diameters of passageway, and they may be shaped for forward reaming or back reaming depending on the requirement. They will generally have cutting edges that suit the terrain.
An example of the prior art has been described with reference to
An example of the invention will now be described with reference to the following accompanying drawings, in which:
Referring now to
Referring now to
Referring now to
Referring now to
The assembled reamer will now be described with reference to
The next step is to mount the stabilization ring 140 onto the rear of the forward part 160 of the reamer 100. To do so the support pillars 144 are aligned with the cutting wings 130 and slid into the slots 108 from the rear. The stabilization ring 140 is moved forward until the flanges 148 enter the slots 139 in the respective cutting wings 130. This engagement resists any rotation of the stabilization ring 140 relative to the reamer as a result of torsion forces during use. Also, in this position the forward part of the circular sleeve 142 overlies the step at the top of flange 138 extending rearward from the back of the cutting wings 130. In this way the circular sleeve 142 contains the rear flange 138 of the cutting wings and resists radial movement of them. Once the stabilization ring is properly mounted it is bolted onto the reamer by bolts that pass through holes 114 in the support wings 106, and holes 147 in the support pillars 144.
Finally, the plug 150 is inserted through collar 146 in the stabilization ring and connected to the hollow core of the support housing 102. The collar 146 is firmly supported to the support housing 102 by the plug 150.
In use, while travelling through the hole, for instance in the direction indicated by arrow 400 the reamer is rotated by the drill string in the clockwise direction (anticlockwise from behind as shown by arrow 420). It is the rotation of the cutting wings 130 that enlarges the hole. The forces applied to the cutting wings 130 are transmitted to the support wings 106, and are not absorbed by the bolts which secure the cutting wings 130 and support wings 106 to each other. Overall there is much more metal supporting the cutting wings than in the prior art arrangement described above. The result of this arrangement is that the bolts are not stressed and do not come loose. As an added measure of security, lock nuts are applied to the main bolts to minimise any chance of them coming loose.
The central core of the drill string, and reamer is hollow, and typically a lubricant ‘mud’ is pumped into this core to escape out of the reamer and flush the new cut debris from the hole.
The cutting inserts 136 fitted to the leading face of the cutting wings 130 wear away during use and require periodic replacement. To replace the cutting wings 130 the assembly process is reversed and new wings installed before reassembly. Since the cutting wings can be simply unbolted from the reamer, they are able to be replaced in the field when the cutting inserts are worn. The old cutting wings can then be sent back to the workshop for refurbishment.
Although the invention has been described with reference to a particular example, it will be appreciated by the appropriately skilled person that many modifications and additions are possible. For instance, the reamer may be reversible with cutting surfaces along both the forward and rearward facing edges of the cutting wings.
Number | Date | Country | Kind |
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2010904234 | Sep 2010 | AU | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/AU2011/001190 | 9/15/2011 | WO | 00 | 5/28/2013 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2012/037597 | 3/29/2012 | WO | A |
Number | Name | Date | Kind |
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5417292 | Polakoff | May 1995 | A |
6131675 | Anderson | Oct 2000 | A |
6250404 | Gunsaulis | Jun 2001 | B1 |
7997354 | Radford et al. | Aug 2011 | B2 |
20100175927 | Zulak | Jul 2010 | A1 |
Number | Date | Country |
---|---|---|
658510 | Oct 1951 | GB |
774075 | May 1957 | GB |
2341878 | Mar 2000 | GB |
2001090464 | Apr 2001 | JP |
2008070038 | Jun 2008 | WO |
Entry |
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International Search Report for PCT/AU2011/001190, Completed by the Australian Patent Office on Oct. 11, 2011, 3 Pages. |
Number | Date | Country | |
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20130248254 A1 | Sep 2013 | US |