U.S. patent number 3,672,455 [Application Number 05/028,417] was granted by the patent office on 1972-06-27 for drag bits.
This patent grant is currently assigned to Tarton Industries, Inc.. Invention is credited to James L. Foster, Jr..
United States Patent |
3,672,455 |
Foster, Jr. |
June 27, 1972 |
DRAG BITS
Abstract
An earth drilling bit of the drag type is provided having a body
with a plurality of radial slots at one end, each having a portion
extending across said one end from the axis, a plurality of
L-shaped wings removably fitted in said slots and held in place by
resilient means extending through passages in the body and
wings.
Inventors: |
Foster, Jr.; James L. (Ligonier
Township, Westmoreland County, PA) |
Assignee: |
Tarton Industries, Inc.
(N/A)
|
Family
ID: |
21843340 |
Appl.
No.: |
05/028,417 |
Filed: |
April 14, 1970 |
Current U.S.
Class: |
175/412;
175/418 |
Current CPC
Class: |
E21B
10/627 (20130101); E21B 10/38 (20130101) |
Current International
Class: |
E21B
10/36 (20060101); E21B 10/38 (20060101); E21B
10/00 (20060101); E21B 10/62 (20060101); E21c
013/00 () |
Field of
Search: |
;175/409,410,411,412,413
;299/92 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Champion; Marvin A.
Assistant Examiner: Favreau; Richard E.
Claims
I claim:
1. An earth drilling bit of the drag type adapted for rotation
about its longitudinal axis comprising a body, a plurality of
radial slots at one end having a portion extending across said one
end from the axis, a plurality of L-shaped wings removably fitted
in said slots, a passage through each said wings intermediate their
ends, a like plurality of passages in said body intersecting each
of said slots at a point axially offset from the passage in said
wings when said wings are inserted in said slots and a resilient
member extending through each of said passages biasing each of said
wings in both a direction parallel to the longitudinal axis of the
body and a direction transverse to the longitudinal axis of the
body into tight engagement with the slot and body, each said wing
extending radially beyond the body to provide a hole gauging
portion and axially ahead of the said one end of the body to
provide an end drilling face.
2. An earth drilling bit of the drag type as claimed in claim 1
wherein the resilient means is a spring steel roll pin.
3. An earth drilling bit of the drag type as claimed in claim 1
wherein the radial slot extends across said one end from the axis
and vertically up the side of the body to form an L-shaped
slot.
4. An earth drilling bit of the drag type as claimed in claim 1
wherein each wing has a forward face of generally planar form
having a layer of hard abrasive resistant material secured to and
over-laying said forward face to provide hard cutting edges.
5. An earth drilling bit of the drag type as claimed in claim 1
wherein the wings, in the portion extending ahead of the body, are
in the form of stepped segments, the steps increasing in length
ahead of the body from the axis outwardly.
6. An earth drilling bit of the drag type as claimed in claim 1
wherein each wing is a flat generally planar member having an
L-shaped body engaging recess at one end and a plurality of stepped
extensions at the other end forming a cutting edge extending ahead
of said body.
Description
This invention relates to drag bits and more particularly to a drag
bit having replaceable wings for use in all forms of earth boring
operations including drilling through the earth for oil, gas and
the like as well as for drilling in mining and quarrying
operations.
Earth boring bits are required to operate under greatly varied
conditions.
These variables include the rock formations in which they are used,
the types of rigs used to operate them, the rotational speeds, the
vertical applied loads, the nature of the drill "string" and the
drilling fluid used. The combined effects of all of these variables
ultimately determines the drill life, the rate of penetration and
the ability of the bit to drill through any given formation.
Drag bits are generally made with a body having radial wings
extending from the body radially and axially. These wings are
welded to the body or formed with the body to form a single unit.
Generally the wings have a cylindrical surface on their outer edges
that subtends a substantial circumferential arc. A typical
construction of such a drag bit is shown in U.S. Pat. No.
3,140,748.
Drag bits of this prior art type are used until the effective
diameter is reduced by wear after which they are discarded. There
is a very substantial loss of money in the discarded body and
unused wing area both in metal and lost machining. This discarded
body cannot be used except as scrap.
In order to overcome this very significant loss, it has been
proposed to provide an axial body portion to which are attached
removable and replaceable wings. Typical of these bits are those
illustrated in U.S. Pat. Nos. 2,978,049, 3,003,570 and 3,182,736.
These drag bits with replaceable wings have not met with complete
acceptance in the trade for a variety of reasons. First, they are
too complex and thus costly to machine. Second, they are difficult
to maintain because of their complex fastening systems. And third,
they do not provide a sufficiently rigid base for the wing
particularly against vertical loading.
I have invented a drag bit which eliminates the loss of discarded
bodies and yet is very simple and inexpensive to make and maintain.
I provide a main body and interchangeable wings which can be
quickly removed and replaced with new wings using the same main
body.
Preferably, I provide a drag bit adapted for rotation about its
longitudinal axis comprising a main body, a plurality of radial
slots at one end, extending across said one end from the axis and
vertically upwardly along a portion of the sides of said body, a
plurality of generally L-shaped wings removably fitted in said
slots, a passage through each of said wings intermediate their
ends, a like plurality of passages in said main body intersecting
each of said slots at a point slightly axially offset from the
passage in said wings when said wings are inserted in said slots
and a resilient member extends through said passages to bias said
wings into tight engagement with the slot and body, each wing
extending radially beyond the body to provide a hole gauging
portion and axially ahead of the said one end of the body to
provide an end drilling face. Preferably, each wing has a forward
face of generally planar form having a layer of hard alloy material
secured to each forward face to provide hard cutting edges limiting
wear on said forward faces. The resilient means extending through
the passages in the body and wings are sprung steel roll pins.
In the foregoing general description, I have set out certain
objects, purposes and advantages of my invention. Other objects,
purposes and advantages of this invention will be apparent from a
consideration of the following description and the accompanying
drawings in which:
FIG. 1 is an end view of a drag bit body according to my
invention;
FIG. 2 is a side elevation of the body of FIG. 1;
FIG. 3 is a section on the line III--III of FIG. 1;
FIG. 4 is a section on the like IV--IV of FIG. 1;
FIG. 5 is a side elevation of wing according to my invention;
FIG. 6 is an end elevation viewed from the right of FIG. 5;
FIG. 7 is an edge elevation of the view of FIG. 5;
FIG. 8 is an end view of a drag bit according to my invention;
FIG. 9 is a fragmental section on the line IX--IX of FIG. 10;
and
FIG. 10 is a side elevation of a drag bit according to my
invention.
Referring to the drawings, I have illustrated an elongated body 10
having a shank 11 which may be threaded internally or externally,
provided with slots and steps or any other conventional means by
means of which it can be attached to a drill string and rotated
about its axis. The body end opposite the shank 11 is provided with
a plurality of spaced apart grooves 12 which form between them
spaced apart lands 13. Each land 13 is provided with a radial slot
having a portion 14 extending along the length of the land and a
portion 14a extending transversely across the end of the body
opposite the shank to a central axial air passage 15. A hole 16 is
drilled through each land 13 and through the slot 14. Angular air
passages 17 are provided from the axial passage 15 to the grooves
12. The radial slot 14 and 14a is thus L-shaped with the two
portions lying at approximately right angles.
A plurality of wings 20, one for each radial slot 14 and 14a are
inserted in said slots and held in position by a spring steel roll
pin 21 which passes through a hole 22 in the wing and hole 16 in
the body. The hole 22 in each wing is slightly off center from the
hole 16 in the body so that the roll pin biases the wing into tight
engagement with the bottom portions of slot portions 14 and 14a.
Each wing is provided with a multi-stepped portion 23 which extends
axially ahead of the body portion to provide an end drilling face
and with a radially outwardly extending portion 24 to provide a
hole gauging face. The stepped portion 23 is preferably provided
with cylinders 25 and 25a of cemented carbide one, 25, extending
axially of the wing and bit, the other 25a extending diagonally.
The face of the wing 20 which is the forward or cutting face is
preferably provided with a longitudinal slot 26 and a transverse
slot 27 into which are brazed small pieces of cemented carbide 29
and 30 respectively, or which is filled with some hard facing or
cutting alloy to reduce the wear by abrasion during drilling.
It will be seen from the drawings that the wings in the bit of my
invention are fully supported against vertical axial thrust by the
groove 14a against which the edge 28 of the wing 20 abuts while
edge 28a of wing 20 is engaged in slot 14. The roll pin 21
constantly biases the wing into tight engagement with the grooves
14 and 14a.
I have illustrated and described a presently preferred embodiment
of my invention. However, it will be understood that this invention
may be otherwise embodied within the scope of the following
claims.
* * * * *