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Patent 2253503 Summary

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Claims and Abstract availability

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(12) Patent Application: (11) CA 2253503
(54) English Title: STABILISER FOR BOREHOLE DRILLING APPARATUS
(54) French Title: STABILISATEUR DE MACHINE DE FORAGE DE PUITS
Status: Deemed Abandoned and Beyond the Period of Reinstatement - Pending Response to Notice of Disregarded Communication
Bibliographic Data
(51) International Patent Classification (IPC):
  • E21B 17/10 (2006.01)
(72) Inventors :
  • RUSSELL, MARK ALEXANDER (United Kingdom)
  • RUSSELL, FREDERICK BRIAN (United Kingdom)
(73) Owners :
  • CUTTING & WEAR RESISTANT DEVELOPMENTS LIMITED
  • CUTTING & WEAR RESISTANT DEVELOPMENTS LIMITED
(71) Applicants :
  • CUTTING & WEAR RESISTANT DEVELOPMENTS LIMITED (United Kingdom)
(74) Agent: GOWLING WLG (CANADA) LLP
(74) Associate agent:
(45) Issued:
(86) PCT Filing Date: 1997-05-23
(87) Open to Public Inspection: 1997-12-04
Availability of licence: N/A
Dedicated to the Public: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): Yes
(86) PCT Filing Number: PCT/GB1997/001417
(87) International Publication Number: WO 1997045620
(85) National Entry: 1998-11-03

(30) Application Priority Data:
Application No. Country/Territory Date
9611016.8 (United Kingdom) 1996-05-25

Abstracts

English Abstract


A drill string stabiliser (10) for bore hole drilling apparatus, which
comprises a plurality of fixed spiral blade arms (11) provided with
replaceable wear elements (12).


French Abstract

Stabilisateur (10) de train de tiges de forage conçu pour une machine de forage de puits et consistant en une pluralité de longerons fixes spiralés (11) pourvus d'éléments d'usure remplaçables.

Claims

Note: Claims are shown in the official language in which they were submitted.


CLAIMS
1. A drill string stabiliser (1) for bore hole drilling
apparatus, which comprises a plurality of fixed
blade arms (11,30,40,50,60,72,81,94) provided with
replaceable wear elements (12,20,44,53,63,74,96),
characterised in that
the blade arms are spiral and provided with
shoulders (31,41,51,61,71) defining longitudinal
grooves or recesses (32,42,80) in the external faces
of the blade arms; in that
replaceable wear elements are provided with
seating portions (22,45,54,73,82) which are located
in the longitudinal grooves or recesses; and in that
the shoulders and the seating portions of the
wear elements are provided with holes (52/55,62/64)
which, when a wear element is located in its groove
or recess, are aligned, such that a connecting means
(56,65,70,90) can be inserted into the holes to
secure the wear element to the blade arm.
2. A stabiliser according to Claim 1, in which the wear
elements comprise silicon carbide.
3. A stabiliser according to claim 1 or 2, in which
each spiral blade arm is provided with a single wear
element which extends for the full length of the
working surface of the blade arm.

11
4. A stabiliser according to claim 1, 2 or 3, in which
the wear elements extend to a radial distance of
from 10 to 500mm from the blade arm.
5. A stabiliser according to any preceding claim, in
which the connecting means is an elongate pin.
6. A stabiliser according to any of claims 1 to 4, in
which said hole in the wear element comprises a
recess (64) and said connecting means comprises a
nut (65) located in the holes (62) in the shoulders
(61) and in said recess, and a bolt (68) received in
a bolthole (67) in the wear element.
7. A wear element for a spiral blade stabiliser as
claimed in any preceding claim which wear element
comprises a working face, and a seating portion on
a side opposite thereto, the wear element being of
generally elongate shape and curved transversely to
its longitudinal axis to form a segment of a spiral
or helix, said seating portions being provided with
holes (62/64).

Description

Note: Descriptions are shown in the official language in which they were submitted.


CA 022~3~03 1998-ll-03
WO 97/45620 PCTIGB97/01417
STABLISER FOR BOREHOLE DRLLING APPARATUS
This invention relates to stabilisers for borehole
drilling apparatus and more particularly to a drill
string stabiliser having fixed blade arms provided with
replaceable wear elements.
Drill string stabilisers, sometimes referred to as
drill collar stabilisers, or as drill stem stabilisers,
are used in earth boring operations to centralise the
drill stem in a borehole during drilling operations,
especially in the drill collar section of the drill
string, for example, at distances of from 0-300 metres
above the drill bit. The drill string stabiliser has a
variety of functions as follows:
(i) to control the hole angle direction;
20(ii) to prevent the bit from drifting laterally;
and
(iii) to improve the cutting performance of the bit
by keeping it rotating centrally about its
25axis so as to provide a substantially equal
force loading on all three drill bit cones.

CA 022~3~03 1998-11-03
W097/45620 PCT/GB97/01417
In addition, where the surrounding rock formation is
not too hard, the stabiliser may also provide a re~ming
function for undersized or irregularly shaped boreholes.
This invention is particularly concerned with
rotatable stabilisers of the kind which rotate together
with the drill string.
The wall-contacting members of a rotatable
stabiliser are subject to the various forces attendant on
the entire drill string, which may include thrust forces,
fretting forces, and the forces resulting from drill
string manipulations, the conditions of the borehole, and
the fluid conditions internal and external to the drill
string.
In the rotary system of drilling, employing a liquid
circulating through the drill string and through the
annulus between the drill string and the borehole, it is
necessary that the stabiliser includes not only fluid
passage means therethrough to form part of the drill
string flow passage, but also fluid passage means to form
part of the annulus fluid passage. The annular fluid
passage means are provided at the outer periphery of the
stabiliser, with the result that the wall-contacting
portion of the stabiliser is not continuous around the
circumference thereof, but instead consists of a number

CA 022~3~03 1998-11-03
of blades azimuthally spaced apart by the fluid passage
means.
It is known to provide fixed blade arms,
incorporating wear elements, which are welded to the
stabiliser, or to a sleeve surrounding the stabiliser,
and such "welded-blade" stabilisers are disclosed in GB
2096210, US 2288124, and US 3268274.
10It is also known to provide rotatable stabilisers
with devices for connecting wear elements to fixed blade
arms, enabling the wear elements to be detached and
replaced. Such mechanisms include various slot and
groove connections, cap screw connections, tapering
wedging connections and combinations of these. Typical
arrangements are shown in US 3680647 and US 3818999. US
4662461 discloses a stabiliser having a plurality of
fixed blade arms with replaceable wear elements.
20Whilst all the above patents are concerned with
stabilisers in which the blades lie parallel to the axis
of the drill string, there is another class of
stabilisers, known as spiral blade stabilisers, for which
no solution to the problem of providing replaceable wear
elements has yet been found.
According to the present invention, there is
provided a drill string stabiliser for borehole drilling
~MENDED SHEET
IPEA/EP --
, . .. .. . . , _ . .

CA 022~3~03 1998-11-03
apparatus, which comprises a plurality of fixed blade
arms provided with replaceable wear elements,
characterised in that the blade arms are spiral and
provided with shoulders defining longitudinal grooves or
recesses in the external faces of the blade arms; in that
replaceable wear elements are provided with seating
portions which are located in the longitudinal grooves or
recesses; and in that the shoulders and the seating
portions of the wear elements are provided with holes
which, when a wear element is located in its groove or
recess, are aligned, such that a connecting means can be
inserted into the holes to secure the wear element to the
blade arm.
The stabiliser may be provided with any suitable
number of spiral blade arms, but usually two or three are
sufficient for most purposes. A larger number of blade
arms can, however, be used if appropriate.
The wear elements can comprise silicon carbide, or
similar hard materials. Preferably, each spiral blade
arm is provided with a single wear element, curved to
form a segment of a spiral or helix, which extends for
the full length of the working surface of the blade arm.
The wear element preferably has a surface which is proud
of the blade arm, and can, for example, extend to a
radial distance of from 10 to 500 mm from the blade arm.
:pr~ E~
_ . ~ . . . .
. .

CA 022~3~03 1998-11-03
Examples of spiral blade stabilisers provided with
replaceable wear elements in accordance with the
invention will now be described with reference to the
accompanying Drawings in which:
Figure 1 shows a side elevation of a prior art
spiral blade stabiliser;
Figure 2 shows a side elevation of a first
embodiment of a spiral blade stabiliser according to the
invention;
Figure 3 shows a perspective view from the side and
one end of a wear element suitable for use in a
stabiliser of the present invention;
Figure 4 shows a sectional end elevation of a spiral
blade stabiliser according to the invention, illustrating
three different types of seating for the wear element;
and
~t\/lENDED SH~ET
IPEa/EP -

CA 022~3~03 1998-ll-03
W097/45620 PCT/GB97/01417
Figures 5(a) to (e) illustrate various securing
devices by which the wear element can be secured to the
spiral blade arm.
Referring firstly to Figure l, there is illustrated
a prior art spiral blade stabiliser 1 having a body 2
provided with spiral blade arms 3 having wear surfaces 4.
Spiral channels 5 are provided between adjacent blade
arms to permit drilling fluid, carrying debris from the
borehole, to pass therealong.
Figure 2 illustrates a first embodiment of a spiral
blade stabiliser according to the invention, in which the
stabiliser lO has blade arms 11 having wear elements 12
seated in grooves 13 in the blade working surfaces 14.
Figure 3 shows a novel wear element for use in a
stabiliser according to the invention. The wear element
20, which is curved in two directions in order to conform
to the external surface of a spiral blade, has a working
surface 21, and a wedge-shaped seating portion 22.
The location of the wear element 20 on a spiral
blade arm is shown in figure 4, top right hand side. The
spiral blade arm 30 is provided with shoulders 31
defining a wedge-shaped groove 32 in the external surface
of the blade arm 30. The wear element 20 is seated on
the blade arm 30 such that the wedge-shaped seating

CA 022~3~03 1998-11-03
W097/45620 PCT/GB97/01417
portion 22 of the wear element fits tightly into the
groove 32. Although the seating faces 33, 34 are shown
as straight, they need not be straight, or symmetrical,
and any suitable curved shape can be used as appropriate.
The wear element 20 is seated proud of the blade arm 30
as shown.
Figure 4 also illustrates an alternative seating
arrangement. At the bottom right hand side there is
shown blade arm 40 having shoulders 41 defining a wedge-
shaped groove 42 with rounded bottom corners 43. The
wear element 44 is seated with its wedge-shaped seating
portion 45 in the ~loo~e 42, and is held tightly by the
sides thereof such that it extends proud of the blade 40.
Again, the sides do not have to be straight or
symmetrical.
Figure S shows various alternative arrangements for
mounting and securing the wear elements to the blade arms
of a stabiliser. In figure 5(a), the stabiliser blade
arm 50 has shoulders 51 having aligned, transversely
directed holes 52 therein. The flanged wear element 53
has a seating portion 54 in which there is a transverse
hole 55 which is aligned with the holes 52 to provide a
through passage. A tapered pin 56, which is a tight fit
in the passage formed by the holes 52 and 54, is inserted
therein to secure the wear element 53 in place.

CA 022~3~03 1998-11-03
W097/45620 PCT/GB97/01417
Figure 5(b) shows a second arrangement in which the
blade arm 60 is provided with shoulders 61 having a
passage 62 drilled transversely therethrough. The wear
element 63 has a corresponding recess 64 drilled therein
so as not to provide an obstruction to the passage 62
when the wear element is seated on the blade arm 60. A
barrel nut 65 is positioned in the passage 62 and aligned
such that its central threaded hole 66 is immediately
beneath a bolt hole 67 in the wear element 63. The
bolthole 67 is countersunk to accept a bolt 68 such that
the head of the bolt 69 is below the working surface of
the wear element 63.
In Figure 5(c) there is shown a further mounting
lS arrangement which is similar to that of Figure 5(a)
except that the tapered pin 56 is replaced by a roll pin
70 and the shoulders 71 of the blade arm 72 have straight
sides and curved corners to accommodate a similarly
shaped seating portion 73 of wear element 74.
Figure 5(d) shows a similar arrangement to that of
Figure 5(c) except that in this case the groove 80 in the
blade arm 81 is wedge-shaped to accommodate a wedge-
shaped seating portion 82 of the wear element.
Finally, Figure 5(e) shows a still further
arrangement which is similar to that of Figure 5(c)
except that the roll pin is replaced by a bent or cranked

CA 022~3~03 1998-11-03
pin 90 fixed at one end to a locking plate 91 carrying a
locking screw 92. Locking plate 91 and screw 92 fit
within a recess 93 of the blade arm 94 and the locking
screw is secured to the blade arm 94 via a screw threaded
hole 95. The bent or cranked pin provides a radial force
to maintain the flanged wear element 96 firmly secured to
the blade arm 94 and its orientation is maintained by the
locking plate and screw arrangement 91, 92.
Al~ r'~E~! SHEE~
~ ?~ ~ 'E~
. ,,, , , . . ~ ,

CA 022~3~03 1998-ll-03
W097/45620 PCT/GB97/01417
stated otherwise, each feature disclosed is one example
only of a generic series of equivalent or similar
features.
The invention is not restricted to the details of
the foregoing embodiment(s). This invention extends to
any novel one, or any novel combination, of the features
disclosed in this specification (including any
A~.r.Dmpanying claims, abstract and drawings), or to any
novel one, or any novel combination, of the steps of any
method or process so disclosed.
. . .

Representative Drawing
A single figure which represents the drawing illustrating the invention.
Administrative Status

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Event History

Description Date
Time Limit for Reversal Expired 2001-05-23
Application Not Reinstated by Deadline 2001-05-23
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2000-05-23
Appointment of Agent Request 1999-03-04
Revocation of Agent Request 1999-03-04
Inactive: Single transfer 1999-02-03
Classification Modified 1999-01-12
Inactive: IPC assigned 1999-01-12
Inactive: First IPC assigned 1999-01-12
Inactive: Courtesy letter - Evidence 1998-12-29
Inactive: Notice - National entry - No RFE 1998-12-23
Inactive: Applicant deleted 1998-12-22
Application Received - PCT 1998-12-21
Application Published (Open to Public Inspection) 1997-12-04

Abandonment History

Abandonment Date Reason Reinstatement Date
2000-05-23

Maintenance Fee

The last payment was received on 1999-04-23

Note : If the full payment has not been received on or before the date indicated, a further fee may be required which may be one of the following

  • the reinstatement fee;
  • the late payment fee; or
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Fee History

Fee Type Anniversary Year Due Date Paid Date
Basic national fee - small 1998-11-03
Registration of a document 1999-02-03
MF (application, 2nd anniv.) - small 02 1999-05-25 1999-04-23
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
CUTTING & WEAR RESISTANT DEVELOPMENTS LIMITED
CUTTING & WEAR RESISTANT DEVELOPMENTS LIMITED
Past Owners on Record
FREDERICK BRIAN RUSSELL
MARK ALEXANDER RUSSELL
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
Documents

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Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Cover Page 1999-01-20 1 27
Abstract 1997-11-03 1 47
Description 1998-11-03 10 287
Claims 1998-11-03 2 57
Drawings 1998-11-03 4 95
Representative drawing 1999-01-20 1 6
Reminder of maintenance fee due 1999-01-26 1 110
Notice of National Entry 1998-12-23 1 192
Courtesy - Certificate of registration (related document(s)) 1999-03-09 1 117
Courtesy - Abandonment Letter (Maintenance Fee) 2000-06-20 1 184
Correspondence 1999-03-04 1 39
PCT 1998-11-03 16 532
Correspondence 1998-12-29 1 31