BACKGROUND
[0001] The present invention relates to a tubular component used for drilling and operating
hydrocarbon wells and landing heavy loads in a well or on or below the sea bed. The
term "drill string or landing string component" means any element with a substantially
tubular shape intended to be connected to another element of the same type or not
in order, when complete, to constitute either a string for drilling or performing
operations within a hydrocarbon well or a string for landing heavy loads in a well
or on or below the sea bed. The invention is of particular application to other components
used in a drill string or landing string such as drill pipes, heavy weight drill pipes,
drill collars, and the parts which connect drill pipes, heavy weight drill pipes,
and landing pipes known as tool joints.
[0002] When a drill string is taken apart, removed, or connected, gripping slips are used
to grip an area on the drill string or landing string component below the component
being removed from, or connected to, the drill string or landing string.
[0003] Gripping slips have inserts with teeth to clamp the drill string or landing string
component below the drill string or landing string component being removed or reconnected,
and hold up the unsupported weight of the string below the slips. Due to repeated
gripping of certain drill string or landing string components by the gripping slips,
the area of the drill string or landing string component where gripping takes place
may be more subject to fatigue failure from repetitive loading and unloading, and
notching from each application of the slips' teeth. Accordingly, manufacturing a drill
string or landing string component with a suitably long part life is challenging,
since the components in a drill string or landing string must be capable in many cases
of withstanding high tensile and compressive loads, bending and rotation under stress,
as well as frequent slips clamping which results in hoop stresses, notching, and potential
crushing of the drill string or landing string component.
[0006] Specifically
Wilson proposed:
"a thick wall rotary slip engaging elongated steel protector tube extending from the
first tool joint to the main portion of the drill pipe, the protector tube having
greater wall thickness than the main portion of the drill pipe, the protector tube
being made of a Martensite steel having a small, close knit, grain size to reduce
the penetration of the slip teeth that engage the protector tube when the joint is
supported in the rotary table by slips"
[0007] Wilson obtains a drill pipe with the protector tube that will run its full expected fatigue
life without failing in notches and marks caused by slips in the rotary table.
[0008] Accordingly, increasing tube wall thickness where slips are applied on a landing
pipe increases the landing pipe's resistance to stresses applied by the slips while
the landing pipe is in tension. A trade-off between resistance to stresses and weight
is needed to select tube wall thickness in the region where slips are to be applied.
[0009] Use of a material with a high Rockwell Hardness (HRC) makes the material stronger
and the pipe more resistant to slip crushing, but more brittle and less resistant
to crack initiation, and crack propagation, which may result from applying slips.
In practice, yield strength ranges can be selected and the pipe treated accordingly
to meet the desired material characteristics.
SUMMARY
[0010] It is an object and feature of an exemplary embodiment described herein to provide
a reduced weight landing pipe capable of maintaining high tensile loads. It is another
object and feature of an exemplary embodiment described herein to provide a landing
pipe less prone to fatigue and cracks. It is further an object and feature of an exemplary
embodiment described herein to provide a landing pipe that improves landing operations.
[0011] One advantage of an exemplary embodiment described herein lies in reducing landing
pipe weight, which reduces loading of drill string and landing string components and
other handling equipment and drilling rig components. Reducing pipe weight can increase
part life and extend the potential reach of the landing string. Another advantage
of an exemplary embodiment described herein is an integral pipe design, where the
pipe is designed with no welds. Identifying the location of a weld while running a
landing pipe may increase the time required to run the pipe. In contrast, an integral
design provides a larger vertical tolerance to apply the slips, such that it takes
less time to set the landing pipe in the slips, leading to faster operations on a
string.
[0012] In addition, an integral design yields a smoother bore with potentially less hydraulic
turbulence, and less hang-up for tools.
[0013] These and other objects, advantages, and features of an exemplary embodiment described
herein will be apparent to one skilled in the art from a consideration of this specification,
including the attached drawings and the appended Claims.
[0014] A landing pipe comprises a first tool joint, a second tool joint, and a main section
extending from the first tool joint to the second tool joint. In an exemplary embodiment
the first tool joint can be an upper tool joint and the second tool joint can be a
lower tool joint, or vice versa. The first tool joint outer diameter is greater than
the largest main section outer diameter, and a first portion of the landing pipe main
section has a greater tube wall thickness than a second portion of the landing pipe
main section. In one embodiment, the tube wall thickness of the second portion of
the landing pipe main section is reduced by boring the inner diameter. In another
embodiment, the tube wall thickness of the second portion of the landing pipe main
section is reduced by turning the outer diameter. In other embodiments, part of the
first portion of the landing pipe main section can also have a reduced tube wall thickness
directly adjacent to the first tool joint.
[0015] In an exemplary embodiment, the length of the second portion of the main section
is between 40-85 % of the overall landing pipe length, which provides sufficient length
to set the slips. In a preferred embodiment, the length of the second portion of the
main section is between 55-80 % of the overall landing pipe length.
BRIEF DESCRIPTION OF THE DRAWINGS
[0016] The characteristics and advantages of the invention are set out in more detail in
the following description, made with reference to the accompanying drawings.
Figure 1 depicts a schematic cross-sectional view of a first embodiment;
Figure 2 depicts a schematic cross-sectional view of a second embodiment;
Figure 3 depicts a schematic cross-sectional view of a second version of the first
embodiment;
Figure 4 depicts a schematic cross-sectional view of a second version of the second
embodiment.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0017] The present invention comprises a landing pipe designed to minimize weight. The present
invention proposes an advantageous trade-off between wall thickness and overall weight,
such that the landing pipe's resistance to crushing, tensile yielding, and fatigue
is improved, yet the weight is manageable.
[0018] Referring to Fig. 1, an exemplary landing pipe is composed of an upper tool joint
(1), a main portion consisting of a first portion (2a), where slips are intended to
engage the landing pipe, a second portion (2b), which has a lower tube wall thickness
than the main portion to reduce weight, and a lower tool joint (3). Tool joints may
be of the pin and box type, and threaded, to allow mating of multiple landing pipes
to form a drill string or landing string.
[0019] In a preferred embodiment, the material used for the landing pipe is a high strength
low alloy (HSLA) material such as 4100 or 4300 series alloy steel.
[0020] An exemplary embodiment of the present invention uses an integral design, defined
as a design without welds. In an exemplary embodiment, no weld is present on the landing
pipe between the main section first portion and the main section second portion. In
a preferred embodiment no welds are present between the tool joints and main section
such that the landing pipe design is entirely integral. Neither
Wilson nor
Huntsinger discloses a design which is integral in part or as a whole.
[0021] An exemplary embodiment of the present invention may have both an integral design
and different mechanical characteristics along its length. The tube main section (2)
requires a high yield strength to ensure a balance between pipe weight and resistance
to tensile loads. A preferred embodiment of the present invention may use a main section
with a higher yield strength, and tool joints (1, 3) with a lower yield strength.
In an exemplary embodiment of the present invention, tool joints have a greater cross
section than the main section, such that a higher force needs to be applied for the
tool joint to yield, compared to the force required for the main section to yield.
Tool joint threads are prone to damage due to their irregular shape, and use of a
lower yield strength may prevent cracks from initiating in the threads.
[0022] In a preferred embodiment, the yield strength range (determined by physical testing
with 0.2 % offset) for the drill pipe's main section is between 135 ksi and 180 ksi.
For commercial embodiments, a main section preferred yield strength range is between
150 ksi and 175 ksi. In a preferred embodiment the yield strength range of the tool
joints is between 120 ksi and 160 ksi. For commercial embodiments, a tool joint preferred
yield strength range is between 135 ksi and 150 ksi.
[0023] In an exemplary embodiment of the present invention, desired mechanical characteristics
are obtained by first heat treating the entire tube (1,2,3) to obtain the required
yield strength for the tube main section (2), and then applying a localized heat treatment
on the tool joints (1,3). In an exemplary embodiment of the present invention, the
localized heat treatment is applied using inductive coils, or any other method that
ensures homogenous heat, both axially and throughout the thickness of the locally
treated area. This localized heat treatment uses the same temperature as the heat
treatment for the entire tube, with a different treatment time (tempering time) based
on the material and thickness used. Tool joints treated with the localized heat treatment
described above have lower yield strength and lower material hardness than the pipe's
main section. A transition area exists between the low yield strength portions (tool
joints) and high yield strength portion (main section), which may be located on the
tool joints, preferably 1" from the taper between the tool joint and the pipe main
section.
[0024] Unlike
Huntsinger and
Wilson, the proposed invention does not use a protector tube. Indeed, the landing pipe's
main section extends from one tool joint to the other tool joint. According to the
present invention, the tube wall thickness is not increased. Instead, the present
invention reduces the landing pipe weight by removing material from the main section's
second portion.
[0025] Huntsinger disclosed using a protector tube with lower hardness than the main pipe portion (less
notch sensitive), but with a protector cross-section large enough to obtain a total
tensile and torsional strength no less than that of the main tube, despite the main
tube having higher unit tensile and torsional strength than the protector tube. In
other words,
Huntsinger disclosed that the main section should have a higher hardness than the protector
tube (notching being less of an issue outside of the protector tube).
Wilson selected a protector tube with a hardness of 30-38 HRC. The present invention does
not use a protector tube. Instead, the present invention can include a single main
section between the tool joints. In a preferred embodiment, there is no section between
the tool joints with a hardness lower than that of the main section, and there is
no section characteristic of a protector tube.
[0026] Referring to Fig. 1, in one exemplary embodiment the present invention utilizes a
standard API drill pipe nominal outer diameter (OD) of 6 5/8" for the main section,
the main section first portion (2a) having a constant inner diameter (ID), and the
main section second portion (2b) having an ID greater than that of the main section
first portion. Nominal values can be assigned certain tolerances to accommodate customers
and industry specifications. One example of an acceptable manufacturing tolerance
is 62/1000". Field tolerances may be up to 90 % of the remaining wall thickness. The
main section second portion (2b) is bored out, increasing the inner diameter. Referring
to Fig. 3, in another version of this embodiment part of the first portion of the
main section (2c) can also be bored out to an ID greater than the main section first
portion to reduce weight, in a region beginning at a first tool joint and finishing
at most 36" below the elevator shoulder of the first tool joint, defined as the junction
between the main portion and the first tool joint. One advantage of this embodiment
is improved landing pipe handling, which results from using a constant drill pipe
API OD along the entire main section length.
[0027] Referring to Fig. 2, in a second exemplary embodiment, the present invention utilizes
for the landing pipe main section first portion (2a) a non-API drill pipe OD of 6
29/32" nominal, which is compatible with commonly used landing pipe handling equipment
on rigs. While the landing pipe in this embodiment displays changes in outer diameter,
new generation rigs prevalently can and often use an API compatible elevator and slip
system with which the present invention is compatible with certain adjustments.
In the second exemplary embodiment, the main section second portion (2b) has a standard
API drill pipe nominal OD (6 5/8") to reduce weight, rather than a nominal 6 29/32"
OD for the full length of the main section. Referring to Fig. 4, in another version
of this embodiment part of the first portion of the landing pipe main section (2c)
can be turned down to an OD lower than the OD of the first portion (2b) of the landing
pipe main section to reduce weight, in a region beginning at an upper tool joint elevator
shoulder and finishing at most 36" below the elevator shoulder of the upper tool joint.
One advantage of this embodiment is the increased landing pipe slips area diameter
and the smooth ID bore throughout the length of the landing pipe. In contrast with
currently existing drill pipes, a smooth bore, such as the one present in this preferred
embodiment, minimizes fluid pressure losses compared to non-integral designs with
offsets and irregularities. The reduction in the OD of the main section first portion
directly adjacent to the upper tool joint elevator shoulder can either increase or
maintain the elevator shoulder surface area, allowing a modified elevator bore or
elevator bushing bore to have an increased or maintained loading capacity with a decreased
tool joint OD.
[0028] In both aforementioned exemplary embodiments the wall thickness of the main section
second portion is reduced such that the landing pipe weight is reduced by at least
5 % compared to a landing pipe with the wall thickness of the main section first portion
equal to the main wall thickness of the main section second portion.
[0029] In an exemplary embodiment, the length of the second portion (2b) of the main section
is between 40-85 % of the overall landing pipe length, which provides sufficient length
to set the slips. In a preferred embodiment, the length of the second portion of the
main section is between 55-80 % of the overall pipe length. In another preferred embodiment,
the length of the second portion of the main section is between 55 % and 65 % of the
overall pipe length.
[0030] Because many possible embodiments may be made of the invention without departing
from the scope thereof, it is to be understood that all matter herein set forth or
shown in the accompanying drawings is to be interpreted as illustrative and not in
a limiting sense.
1. (New): A landing pipe comprising:
a first tool joint with a first tool joint outer diameter;
a second tool joint with a second tool joint outer diameter;
a main section extending from the first tool joint to the second tool joint, said
main section having a main section first portion and a main section second portion,
wherein
the main section first portion has a first portion outer diameter, a first portion
inner diameter, and a first portion wall thickness which is half of a difference between
the first portion outer diameter and the first portion inner diameter,
the main section second portion has a second portion outer diameter, a second portion
inner diameter and a second portion wall thickness which is half of a difference between
the second portion outer diameter and the second portion inner diameter;
the first tool joint outer diameter is greater than both the first portion outer diameter
and second portion outer diameter; and the first portion wall thickness is greater
than the second portion wall thickness,
wherein the main section second portion has a length range of 40 % to 85 % of an overall
length of the landing pipe.
2. (New): The landing pipe as claimed in Claim 1, wherein the first portion of the main
section is integral to the second portion of the main section, with no welds between
the main section and both tool joints.
3. (New): The landing pipe as claimed in Claim 1, wherein the first tool joint, main
section and second tool joint are integral to each other, with no welds therebetween.
4. (New): The landing pipe as claimed in Claim 1, wherein the outer diameter of the first
portion of the main section is equal to the outer diameter of the second portion of
the main section, and the inner diameter of the second portion of the main section
is greater than the inner diameter of the main section first portion.
5. (New): The landing pipe as claimed in Claim 4, wherein the first portion outer diameter
and the second portion outer diameter are 6 5/8" nominal.
6. (New): The landing pipe as claimed in Claim 4, wherein part of the first portion of
the main section beginning at the first tool joint and finishing at most 36" below
an elevator shoulder of the first tool joint has an inner diameter which is greater
than the inner diameter of the first portion of the main section.
7. (New): The landing pipe as claimed in Claim 1, wherein the inner diameter of the first
portion of the main section is equal to the inner diameter of the second portion of
the main section and the outer diameter of the first portion of the main section is
greater than the outer diameter of the second portion of the main section.
8. (New): The landing pipe as claimed in Claim 7, wherein the outer diameter of the first
portion of the main section is 6 29/32" nominal and the outer diameter of the second
portion of the main section is 6 5/8" nominal.
9. (New): The landing pipe as claimed in Claim 7, wherein part of the first portion of
the main section beginning at an elevator shoulder of the first tool joint and finishing
at most 36" below the elevator shoulder of the first tool joint has an outer diameter
which is less than the outer diameter of the first portion of the main section.
10. (New): The landing pipe as claimed in Claim 1, wherein a tensile load capacity range
for the landing pipe is 1.5 million pounds to 4.5 million pounds.
11. (New): The landing pipe as claimed in Claim 1, wherein a material of the landing pipe
is a high strength low alloy steel.
12. (New): The landing pipe as claimed in Claim 11, wherein the material of the landing
pipe has yield strength range of 135 ksi to 180 ksi over the pipe main section.
13. (New): The landing pipe as claimed in Claim 12, wherein the material of the landing
pipe has yield strength range of 150 ksi to 175 ksi over the pipe main section.
14. (New): The landing pipe as claimed in Claim 11, wherein the material of the landing
pipe has yield strength range of 120 ksi to 160 ksi over the tool joints.
15. (New): The landing pipe as claimed in Claim 14, wherein the material of the landing
pipe has yield strength range of 135 ksi to 150 ksi over the tool joints.
16. (New): The landing pipe as claimed in Claim 1, wherein the second portion of the main
section has a length range of 55 % to 80 % of the overall length of the landing pipe.
17. (New): The landing pipe as claimed in Claim 4, wherein yield strength of the tool
joints is less than yield strength of the landing pipe main section.
18. (New): The landing pipe as claimed in Claim 1, wherein the wall thickness of the main
section second portion is reduced such that a weight reduction for the landing pipe
is at least 5 % compared to a landing pipe with the main portion first section wall
thickness equal to the main portion second section wall thickness.
19. (New): The landing pipe as claimed in Claim 1, wherein the second portion of the main
section is directly adjacent to the second tool joint.
20. (New): The landing pipe as claimed in Claim 1, comprising a threaded portion on at
least one tool joint, wherein such threaded portion has a lower yield strength and
decreased hardness compared to the main section.
21. (New): The landing pipe as claimed in Claim 20, wherein a lower yield strength and
decreased hardness compared to the main section result from a localized heat treatment
of the treaded portion.
22. (New): The landing pipe as claimed in Claim 1, comprising a yield strength transition
area between a portion of a tool joint and the main section of the landing pipe, said
yield strength transition area being at least 1" from a taper between the portion
of a tool joint and the main section of the landing pipe.
23. (New): The landing pipe as claimed in Claim 22, wherein the yield strength transition
area results from a localized heat treatment of the portion of a tool joint.