Language selection

Search

Patent 2939850 Summary

Third-party information liability

Some of the information on this Web page has been provided by external sources. The Government of Canada is not responsible for the accuracy, reliability or currency of the information supplied by external sources. Users wishing to rely upon this information should consult directly with the source of the information. Content provided by external sources is not subject to official languages, privacy and accessibility requirements.

Claims and Abstract availability

Any discrepancies in the text and image of the Claims and Abstract are due to differing posting times. Text of the Claims and Abstract are posted:

  • At the time the application is open to public inspection;
  • At the time of issue of the patent (grant).
(12) Patent Application: (11) CA 2939850
(54) English Title: PREDICTIVE LANDING FAILSAFE
(54) French Title: SYSTEME D'ATTERRISSAGE PREDICTIF A SECURITE INTEGREE
Status: Deemed Abandoned and Beyond the Period of Reinstatement - Pending Response to Notice of Disregarded Communication
Bibliographic Data
(51) International Patent Classification (IPC):
  • B66D 1/54 (2006.01)
  • H2P 25/02 (2016.01)
(72) Inventors :
  • KUTTEL, BEAT (United States of America)
  • WILLIAMS, KEVIN R. (United States of America)
  • ELLIS, BRIAN (United States of America)
(73) Owners :
  • CANRIG DRILLING TECHNOLOGY LTD.
(71) Applicants :
  • CANRIG DRILLING TECHNOLOGY LTD. (United States of America)
(74) Agent: SMART & BIGGAR LP
(74) Associate agent:
(45) Issued:
(86) PCT Filing Date: 2015-03-13
(87) Open to Public Inspection: 2015-09-17
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/US2015/020347
(87) International Publication Number: US2015020347
(85) National Entry: 2016-08-16

(30) Application Priority Data:
Application No. Country/Territory Date
14/656,930 (United States of America) 2014-03-13
61/952,452 (United States of America) 2014-03-13

Abstracts

English Abstract

A predictive landing failsafe system is adapted to slow or stop a permanent magnet AC motor in response to a selected condition, such as a power outage. In some embodiments, the predictive landing failsafe system may short two or more terminals of the AC motor in response to the selected condition. In some embodiments, one or more resistors may be coupled between the two or more terminals, the resistors lowering the short-circuit current and thus making a more smooth stop for the AC motor. In some embodiments, the AC motor may be used in a drawworks.


French Abstract

L'invention concerne un système d'atterrissage prédictif à sécurité intégrée conçu pour ralentir ou stopper un moteur à courant alternatif à aimant permanent en réponse à une condition sélectionnée telle qu'une panne de courant. Dans certains modes de réalisation, le système d'atterrissage prédictif à sécurité intégrée peut court-circuiter deux ou plus de deux bornes du moteur à courant alternatif en réponse à la condition sélectionnée. Dans certains modes de réalisation, une ou plusieurs résistances peuvent être couplées entre les deux ou plus de deux bornes, les résistances abaissant le courant de court-circuit et permettant un arrêt moins brutal du moteur à courant alternatif. Dans certains modes de réalisation, le moteur à courant alternatif peut être utilisé dans un treuil de forage.

Claims

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


Claims:
1. A predictive landing failsafe system comprising:
an AC motor, the AC motor powered by one or more phases of AC power
supplied through two or more terminals of the AC motor; and
a predictive landing failsafe controller, the predictive landing failsafe
controller
including a contactor, the contactor having a normal operating position
and a failsafe position, the contactor positioned to supply power to each
phase of the AC motor when in the normal operating position and to
electrically connect at least two terminals of the AC motor when in the
failsafe position, the contactor positioned to be automatically transitioned
from the normal operating position to the failsafe position in response to a
selected condition.
2. The predictive landing failsafe system of claim 1, wherein the AC motor
is a permanent
magnet AC motor.
3. The predictive landing failsafe system of claim 1, wherein the
predictive landing failsafe
controller further comprises a spring positioned to bias the contactor into
the failsafe
position and an electromagnet positioned to retain the contactor in the normal
operating
position against the pressure of the spring while power is supplied to the
electromagnet.
4. The predictive landing failsafe system of claim 3, wherein the AC power
is supplied by a
power source, and the power source is also used to energize the electromagnet,
so that a
failure of the power source de-energizes the electromagnet causing the
contactor to move
into the failsafe position.
11

5. The predictive landing failsafe system of claim 3, wherein the
electromagnet is
selectively de-energizable by the interaction of an operator.
6. The predictive landing failsafe system of claim 3, wherein the permanent
magnet AC
motor is a single phase AC motor having a live terminal and a neutral terminal
through
which single phase AC power is supplied, and the contactor, when in the
failsafe
position, electrically couples the live terminal with the neutral terminal.
7. The predictive landing failsafe system of claim 3, wherein the permanent
magnet AC
motor is a multi-phase AC motor having a terminal corresponding to each phase
of AC
power supplied to the permanent magnet motor, and the contactor, when in the
failsafe
position, electrically couples at least two terminals of the permanent magnet
AC motor.
8. The predictive landing failsafe system of claim 7, wherein the permanent
magnet AC
motor is a three phase AC motor, the permanent magnet AC motor having three
terminals, and the contactor, when in the failsafe position, electrically
couples two of the
three terminals.
9. The predictive landing failsafe system of claim 7, wherein the permanent
magnet AC
motor is a three phase AC motor, the permanent magnet AC motor having three
terminals, and the contactor, when in the failsafe position, electrically
couples the three
terminals.
10. The predictive landing failsafe system of claim 3, further comprising
at least one resistor
positioned between the at least two terminals of the permanent magnet motor.
12

11. The predictive landing failsafe system of claim 10, wherein the
resistor is a variable
resistor.
12. A hoist comprising:
a drum;
an AC motor, the AC motor powered by one or more phases of AC power
supplied through two or more terminals of the AC motor, the AC motor
positioned to rotate a shaft, the shaft coupled to the drum; and
a predictive landing failsafe controller, the predictive landing failsafe
controller
including a contactor, the contactor having a normal operating position
and a failsafe position, the contactor positioned to electrically couple a
power source to each phase of the AC motor when in the normal operating
position and to electrically connect at least two terminals of the AC motor
when in the failsafe position, the contactor positioned to be automatically
transitioned from the normal operating position to the failsafe position in
response to a selected condition.
13. The hoist of claim 12, where the hoist is a drawworks.
14. The hoist of claim 12, wherein the predictive landing failsafe
controller further comprises
a spring positioned to bias the contactor into the failsafe position and an
electromagnet
positioned to retain the contactor in the normal operating position against
the pressure of
the spring while power is supplied to the electromagnet.
13

15. The hoist of claim 14, wherein the power source is also used to
energize the
electromagnet, so that a failure of the power source de-energizes the
electromagnet
causing the contactor to move into the failsafe position.
16. The hoist of claim 14, wherein the electromagnet is selectively de-
energizable by the
interaction of an operator.
17. The hoist of claim 12, wherein the AC power source comprises a VFD, the
VFD
positioned to supply pulse width modulated AC power to each phase of the AC
motor.
18. The hoist of claim 12, wherein the AC motor is a permanent magnet AC
motor.
19. The hoist of claim 18, wherein the permanent magnet AC motor is a
single phase AC
motor having a live terminal and a neutral terminal through which single phase
AC power
is supplied, and the contactor, when in the failsafe position, electrically
couples the live
terminal with the neutral terminal.
20. The hoist of claim 18, wherein the permanent magnet AC motor is a multi-
phase AC
motor having a terminal corresponding to each phase of AC power supplied to
the
permanent magnet AC motor, and the contactor, when in the failsafe position,
electrically
couples at least two terminals of the permanent magnet AC motor.
21. The hoist of claim 20, wherein the permanent magnet AC motor is a three
phase AC
motor, the permanent magnet AC motor having three terminals, and the
contactor, when
in the failsafe position, electrically couples two of the three terminals.
14

22. The hoist of claim 20, wherein the permanent magnet AC motor is a three
phase AC
motor, the permanent magnet AC motor having three terminals, and the
contactor, when
in the failsafe position, electrically couples the three terminals.
23. The hoist of claim 18, further comprising at least one resistor
positioned between the at
least two terminals of the permanent magnet motor.
24. The hoist of claim 23, wherein the resistor is a variable resistor.
25. The hoist of claim 12, where the hoisting mechanism is a winch.
26. The hoist of claim 25, where the hoisting apparatus is an elevator
winch.

Description

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


CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
Predictive Landing Failsafe
Cross-Reference to Related Applications
[0001] This application is a non-provisional application which claims priority
from U.S.
provisional application number 61/952,452, filed March 13, 2014, which is
incorporated by
reference herein in its entirety.
Technical Field/Field of the Disclosure
[0002] The present disclosure relates generally to control systems for
electric motors, and
specifically to control systems for permanent magnet AC motor drawworks.
Background of the Disclosure
[0003] While undergoing a drilling operation, a drilling rig utilizes a
drawworks to raise and
lower pieces of oilfield equipment. For example, the drawworks is used to
raise and lower the
interconnected lengths of drill pipe, casing, or the like, herein referred to
as a tubular string, into
and out of the wellbore. The tubular string, as well as additional connected
equipment such as a
top drive, travelling block, tubular elevator, etc., may be very heavy. The
ability to precisely
control movement of the drawworks may be critical to prevent damage to
equipment as well as
maintain a safe work environment for workers on the drilling rig.
[0004] Typical drawworks may be run using electric motors such as alternating
current electric
motors. AC electric motors rely on alternating currents passed through
induction windings within
the stator to cause rotation of the rotor. So-called three phase AC motors
include three matched
sets of windings positioned radially about the stator. By supplying sinusoidal
AC power to each
of the sets of windings such that each set receives an alternating current
offset by 120 degrees, a
1

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
continuously rotating electromagnetic field can be induced by the stator. The
rotation of the
electromagnetic field in turn causes rotation of the rotor.
[0005] In a permanent magnet AC motor, the rotor includes one or more
permanent magnets
which, in response to the rotating electromagnetic field, cause the rotor to
rotate. Alternatively, if
the rotor is rotated and no AC power is supplied to the windings of the
stator, the movement of
the magnetic field of the permanent magnets may induce voltage in the windings
according to
Lenz's Law.
Summary
[0006] The present disclosure provides for a predictive landing failsafe
system. The predictive
landing failsafe system may include an AC motor. The AC motor may be powered
by one or more
phases of AC power supplied through two or more terminals of the AC motor. The
predictive
landing failsafe system may also include a predictive landing failsafe
controller. The predictive
landing failsafe controller may include a contactor, the contactor having a
normal operating
position and a failsafe position, the contactor positioned to supply power to
each phase of the AC
motor when in the normal operating position and to electrically connect at
least two terminals of
the AC motor when in the failsafe position. The contactor may be positioned to
be automatically
transitioned from the normal operating position to the failsafe position in
response to a selected
condition.
[0007] The present disclosure also provides for a hoist. The hoist may include
a drum. The hoist may
also include an AC motor. The AC motor may be powered by one or more phases of
AC power
supplied through two or more terminals of the AC motor. The AC motor may be
positioned to
rotate a shaft, the shaft coupled to the drum. The hoist may also include a
predictive landing
2

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
failsafe controller. The predictive landing failsafe controller may include a
contactor, the
contactor having a normal operating position and a failsafe position, the
contactor positioned to
electrically couple a power source to each phase of the AC motor when in the
normal operating
position and to electrically connect at least two terminals of the AC motor
when in the failsafe
position. The contactor may be positioned to be automatically transitioned
from the normal
operating position to the failsafe position in response to a selected
condition.
Brief Description of the Drawings
[0008] The present disclosure is best understood from the following detailed
description when
read with the accompanying figures. It is emphasized that, in accordance with
the standard
practice in the industry, various features are not drawn to scale. In fact,
the dimensions of the
various features may be arbitrarily increased or reduced for clarity of
discussion.
[0009] FIG. 1 is a block diagram of an oil rig electrical system consistent
with embodiments of
the present disclosure.
[0010] FIGS. 2A-2D depict predictive landing failsafe systems consistent with
embodiments of
the present disclosure coupled to different winding configurations for an
electric motor.
[0011] FIG. 3 depicts a drawworks utilizing a predictive landing failsafe
system consistent with
embodiments of the present disclosure.
[0012] FIG. 4 depicts a detailed view of the drawworks of FIG. 3.
[0013] FIG. 5 depicts a predictive landing failsafe system consistent with
embodiments of the
present disclosure.
3

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
Detailed Description
[0014] It is to be understood that the following disclosure provides many
different embodiments,
or examples, for implementing different features of various embodiments.
Specific examples of
components and arrangements are described below to simplify the present
disclosure. These are,
of course, merely examples and are not intended to be limiting. In addition,
the present
disclosure may repeat reference numerals and/or letters in the various
examples. This repetition
is for the purpose of simplicity and clarity and does not in itself dictate a
relationship between
the various embodiments and/or configurations discussed.
[0015] FIG. 1 depicts a block diagram of a partial oil rig electrical system
100 consistent with
embodiments of the present disclosure. In some embodiments, power may be
supplied to oil rig
electrical system 100 by generator 101. Generator 101 may be driven by engine
103. In some
embodiments, engine 103 may be driven by natural gas. In some embodiments,
power may be
supplied to oil rig electrical system 100 from line power 101'. As understood
in the art, line
power 101' may be sourced from, for example and without limitation, a local
utility power grid.
In some embodiments, line power 101' may be transformed from, for example,
high voltage to a
lower voltage by transformer 103'. In some embodiments, line power 101' and
generator 101
may be coupled to the rest of oil rig electrical system 100 through one or
more circuit breakers
104 as understood in the art. Generator 101 and line power 101' may supply
power through
supply line 105. In some embodiments, the power supplied may be rectified by
one or more
rectifiers 107. Here, rectifiers 107 are depicted as a single diode, but one
having ordinary skill in
the art with the benefit of this disclosure will understand that any suitable
rectifier arrangement
may be used, including without limitation, half bridge, full bridge, single or
multiphase, etc. The
4

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
output electricity, coupled to DC power bus 109, may then be used to power
other electrical
equipment.
[0016] In some embodiments of the present disclosure, the electrical equipment
may include AC
motor 111. AC motor 111 may, in some embodiments, be a permanent magnet AC
motor,
positioned to rotate in response to AC power supplied to AC motor 111. In some
embodiments,
AC power may be supplied using VFD controller 113 to control inverter 115.
Inverter 115 may
be positioned to provide pulse width modulated AC current to AC motor 111 as
controlled by
VFD controller 113. One having ordinary skill in the art with the benefit of
this disclosure will
understand that rectifier 107, VFD controller 113, and inverter 115 need not
be used to power
AC motor 111. Instead, AC power may be supplied directly from generator 101.
Additionally,
one having ordinary skill in the art with the benefit of this disclosure will
understand that AC
power may be supplied to oil rig electrical system 100 by, for example, a
municipal power
supply.
[0017] In some embodiments, AC motor 111 may be a single or multi-phase AC
motor. As
understood in the art, the number of phases of an AC motor corresponds to the
number of
windings or winding phase groups of AC motor. In a single phase AC motor, one
phase of AC
power is supplied to the windings of the AC motor through a single conductor,
with a neutral
conductor electrically coupled to the opposite ends of the windings. In a
three-phase AC motor,
such as depicted in FIG. 1, three phases of AC power are supplied to AC motor
111, each
through a separate conductor 117a-c coupled to a terminal of AC motor 111. In
a three-phase AC
motor, the windings are grouped into three winding phase groups. As depicted
in FIGS. 2A-2D,
terminals A, B, and C may be connected to the winding groups in a Wye
configuration (FIGS.
2A, 2B) or a delta configuration (FIGS. 2C, 2D). In each configuration, each
phase of the AC

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
power supplied to the AC motor is supplied to a corresponding terminal A, B,
or C, with a phase
offset 120 degrees to the other two phases.
[0018] As depicted in FIG. 1, oil rig electrical system 100 may further
include a predictive
landing failsafe system 119. Predictive landing failsafe system 119 may, as
depicted in FIG. 1,
include contactor 121. Contactor 121 may be positioned to selectively couple
or decouple each
of conductors 117a-c with terminals A, B, C of AC motor 111. When coupled,
conductors 117a-
c are capable of powering AC motor 111 through terminals A, B, C thereof. When
disconnected,
AC motor 111 is disconnected from the AC power oil rig electrical system 100.
[0019] In some embodiments, when contactor 121 decouples conductors 117a-c
from AC motor
111, contactor 121 is positioned to instead short between at least two
terminals A, B, C of AC
motor 111. If AC power is not supplied to AC motor 111, as the permanent
magnets on the rotor
of AC motor 111 rotate, the electromagnetic flux on each winding group varies
and, according to
Lenz's Law, electricity is induced into the windings. This generated
electricity is known as back
EMF. When at least two terminals A, B, C of AC motor 111 are shorted, the back
EMF of each
winding group creates a short circuit current. The magnetic field of the
permanent magnets of the
rotor of AC motor 111 are opposed by the induced electromagnetic field, and a
resultant braking
or stopping force is imparted on the rotor. This braking or stopping force is
known as dynamic
braking.
[0020] As depicted in FIGS. 2A-2D, contactor 121 may switch between a normal
operating
mode, in which each terminal A, B, C is coupled to a conductor 117a-c
respectively, and a
failsafe mode, in which each terminal A, B, C is disconnected from the
respective conductor
117a-c and at least two of which are connected directly together (dashed
lines). As depicted in
6

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
FIGS. 2A, 2C, terminals A and B are shorted together. As depicted in FIGS. 2B,
2D, all three
terminals A, B, C are shorted together. In the failsafe configurations,
because two or more of the
terminals are shorted together, dynamic braking occurs, thus slowing or
stopping AC motor 111.
In some embodiments, the dynamic braking force may be sufficient to completely
stop the
movement of AC motor 111.
[0021] In some embodiments, the short circuit current previously described
may, for example,
cause an abrupt and immediate stoppage of the rotor of AC motor 111. In some
embodiments, as
depicted in FIG. 5, one or more resistors 122a-c may be included in predictive
landing failsafe
system 119. Resistors 122ac may, for example, be adapted to lower the short
circuit current when
in the failsafe configuration. By lowering the short circuit current, the rate
of deceleration of the
rotor of AC motor 111 may be lowered, thus allowing the rotor to come to a
more smooth stop.
In some embodiments, resistors 122ac may be variable resistors as depicted. By
varying the
resistance of each of the resistors 122ac, the rate of deceleration may be
controlled. In some
embodiments, the selected resistance value for resistors 122ac may be small so
that sufficient
short circuit current remains to completely stop the rotor of AC motor 111
despite any external
load imparted on the rotor. In other embodiments, the selected resistance
value for resistors
122ac may be high enough that the rotor of AC motor 111 is slowed but may be
capable of
turning a desired speed under external load. In some embodiments, the selected
resistance value
for resistors 122ac may be optimized based on, for example, the intended
application of AC
motor 111 and any expected load during normal operation of AC motor 111.
[0022] In some embodiments of the present disclosure, predictive landing
failsafe system 119
may be coupled to oil rig electrical system 100 such that when power is being
supplied, contactor
121 remains in the normal operating mode. In response to a certain condition,
predictive landing
7

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
failsafe system 119 may be positioned to cause contactor 121 to trip into the
failsafe position,
thus halting the rotation of AC motor 111 immediately. In some embodiments,
the certain
condition may be a power outage or blackout on oil rig electrical system 100.
For example, in
some embodiments, contactor 121 may be held in the normal operating position
by a spring-
opposed electromagnet (not shown) powered by oil rig electrical system 100. If
a blackout
occurs, the electromagnetic attraction between the electromagnet and contactor
121 may cease,
allowing the spring to move the contactor into the failsafe position. In some
embodiments, the
condition may be a manual override triggered by an operator, such as in an "E-
stop" condition.
[0023] In some embodiments of the present disclosure, AC motor 111 may be used
as part of a
piece of oilfield equipment. With reference to FIG. 3, AC motor 111 may be
used to drive,
without limitation, drawworks 201, top drive 203, or a rotary table (not
shown). For the purposes
of this disclosure and to clarify the operation of the present disclosure, an
embodiment in which
AC motor 111 is used as part of drawworks 201 will be described. Additionally,
although
described herein as a drawworks, one having ordinary skill in the art with the
benefit of this
disclosure will understand that drawworks 201 may be any hoist apparatus and
is not limited to
lifting or supporting the described equipment.
[0024] FIG. 3 depicts oil rig 205. Oil rig 205 may include derrick 207.
Derrick 207 may be
positioned to support crown block 209. Crown block 209 may be coupled to
travelling block 211
by wireline 213. Wireline 213 may be coupled to drawworks 201. As understood
in the art,
crown block 209 and travelling block 211 may include one or more pulleys
positioned to allow
wireline 213 to lift or lower travelling block 211 relative to crown block 209
as wireline 213 is
paid in or out by drawworks 201. In some embodiments, travelling block 211 may
be coupled to
8

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
top drive 203. Top drive 203 may be used to support a string of interconnected
tubular members
such as tubular string 215 as depicted.
[0025] As depicted in FIG. 4, drawworks 201 may include AC motor 111. AC motor
111 may be
coupled by, for example a shaft (not shown), to drum 217. Wire line 213 may
wrap around drum
217 such that as drum 217 is rotated by AC motor 111, wire line 213 extends or
retracts
depending on the direction of rotation of drum 217.
[0026] As an example, a lowering operation for tubular string 215 will be
described. Once
tubular string 215 is properly coupled to travelling block 211, wireline 213
may be extended by
drawworks 201. As wireline 213 extends, travelling block 211 lowers, causing
tubular string 215
and any other equipment such as top drive 203 to be lowered. During normal
operation,
predictive landing failsafe system 119 may remain in the normal operating
mode. In the event of
a power outage or other condition, predictive landing failsafe system 119 may
trip into the
failsafe mode, causing rotation of AC motor 111, and thus rotation of
drawworks 201 to slow or
stop. As drawworks 201 slows or stops, wireline 213's extension is slowed or
stopped, causing
the descent of tubular string 215 to likewise slow or stop. By automatically
triggering this
slowing or stoppage of tubular string 215 without the need for additional
power or operator
input, damage to, for example, top drive 203, travelling block 211, or tubular
string 215 and any
associated components may be prevented. Additionally, damage to a wellbore or
to the seabed
for offshore drilling operations may likewise be prevented. Furthermore,
safety of rig personnel
may be increased and injuries may be prevented.
[0027] The foregoing outlines features of several embodiments so that a person
of ordinary skill
in the art may better understand the aspects of the present disclosure. Such
features may be
9

CA 02939850 2016-08-16
WO 2015/138838 PCT/US2015/020347
replaced by any one of numerous equivalent alternatives, only some of which
are disclosed
herein. One of ordinary skill in the art should appreciate that they may
readily use the present
disclosure as a basis for designing or modifying other processes and
structures for carrying out
the same purposes and/or achieving the same advantages of the embodiments
introduced herein.
One of ordinary skill in the art should also realize that such equivalent
constructions do not
depart from the spirit and scope of the present disclosure and that they may
make various
changes, substitutions, and alterations herein without departing from the
spirit and scope of the
present disclosure.

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

2024-08-01:As part of the Next Generation Patents (NGP) transition, the Canadian Patents Database (CPD) now contains a more detailed Event History, which replicates the Event Log of our new back-office solution.

Please note that "Inactive:" events refers to events no longer in use in our new back-office solution.

For a clearer understanding of the status of the application/patent presented on this page, the site Disclaimer , as well as the definitions for Patent , Event History , Maintenance Fee  and Payment History  should be consulted.

Event History

Description Date
Letter Sent 2020-03-13
Application Not Reinstated by Deadline 2020-03-13
Time Limit for Reversal Expired 2020-03-13
Common Representative Appointed 2019-10-30
Common Representative Appointed 2019-10-30
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2019-03-13
Inactive: IPC assigned 2016-09-30
Inactive: First IPC assigned 2016-09-27
Inactive: IPC removed 2016-09-27
Inactive: IPC assigned 2016-09-27
Inactive: Cover page published 2016-09-19
Inactive: Notice - National entry - No RFE 2016-08-30
Letter Sent 2016-08-25
Inactive: Inventor deleted 2016-08-25
Inactive: Inventor deleted 2016-08-25
Inactive: Inventor deleted 2016-08-25
Inactive: IPC assigned 2016-08-25
Application Received - PCT 2016-08-25
Inactive: First IPC assigned 2016-08-25
National Entry Requirements Determined Compliant 2016-08-16
Amendment Received - Voluntary Amendment 2016-08-16
Application Published (Open to Public Inspection) 2015-09-17

Abandonment History

Abandonment Date Reason Reinstatement Date
2019-03-13

Maintenance Fee

The last payment was received on 2018-01-09

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
  • additional fee to reverse deemed expiry.

Patent fees are adjusted on the 1st of January every year. The amounts above are the current amounts if received by December 31 of the current year.
Please refer to the CIPO Patent Fees web page to see all current fee amounts.

Fee History

Fee Type Anniversary Year Due Date Paid Date
Basic national fee - standard 2016-08-16
Registration of a document 2016-08-16
MF (application, 2nd anniv.) - standard 02 2017-03-13 2017-01-11
MF (application, 3rd anniv.) - standard 03 2018-03-13 2018-01-09
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
CANRIG DRILLING TECHNOLOGY LTD.
Past Owners on Record
BEAT KUTTEL
BRIAN ELLIS
KEVIN R. WILLIAMS
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
Documents

To view selected files, please enter reCAPTCHA code :



To view images, click a link in the Document Description column (Temporarily unavailable). To download the documents, select one or more checkboxes in the first column and then click the "Download Selected in PDF format (Zip Archive)" or the "Download Selected as Single PDF" button.

List of published and non-published patent-specific documents on the CPD .

If you have any difficulty accessing content, you can call the Client Service Centre at 1-866-997-1936 or send them an e-mail at CIPO Client Service Centre.


Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Description 2016-08-15 10 383
Drawings 2016-08-15 5 216
Representative drawing 2016-08-15 1 36
Abstract 2016-08-15 1 74
Claims 2016-08-15 5 141
Cover Page 2016-09-18 1 50
Notice of National Entry 2016-08-29 1 195
Courtesy - Certificate of registration (related document(s)) 2016-08-24 1 102
Reminder of maintenance fee due 2016-11-14 1 111
Courtesy - Abandonment Letter (Maintenance Fee) 2019-04-23 1 174
Commissioner's Notice: Request for Examination Not Made 2020-04-02 1 538
Patent cooperation treaty (PCT) 2016-08-15 2 74
International search report 2016-08-15 1 60
Patent cooperation treaty (PCT) 2016-08-15 3 144
National entry request 2016-08-15 6 215
Prosecution/Amendment 2016-08-15 2 64