Apparatus and Methods for Managing Equipment Stability
Apparatus and methods for determining the instability of equipment by measuring the reaction forces at different points at the base of the equipment are disclosed. A plurality of load sensors are symmetrically arranged at the base of the equipment. A Cartesian coordinate system is then imposed on the base of the equipment with the center of the base being the origin of the Cartesian coordinate system. The X-axis and the Y-axis of the Cartesian coordinate system are arranged to define a plane corresponding to the base of the equipment. Each load sensor is then designated with Cartesian coordinates and the reaction force at each load sensor is determined. An overall instability factor for the equipment is then determined from the Cartesian coordinates of each load sensor and the reaction force at that load sensor.
Oil field operations often entail the use of numerous storage tanks and other equipment. Storage tanks may be used to store the solid materials or the fluids that are used in the various stages of an oil field operation. For instance, sand bins may be used for handling the sand inventory on an oil field. However, such storage units are often tall, making them susceptible to tipping over due to instability.
Various factors may lead to instability of a storage tank on the field. For instance, instability may result from uneven settlement or leaning due to slope. Additionally, wind loads, uneven loading, or ancillary equipment forces may contribute to instability of a storage tank.
Earlier attempts use inclinometers to indicate whether a storage tank is leaning due to slope or uneven settlement. An inclinometer measures the angle of slope (or tilt), elevation or inclination of an object with respect to gravity. However, inclinometers fail to monitor the potential instability resulting from eccentric loads due to factors such as wind loads, imbalanced loading, or ancillary equipment forces.
Some specific example embodiments of the disclosure may be understood by referring, in part, to the following description and the accompanying drawings.
While embodiments of this disclosure have been depicted and described and are defined by reference to example embodiments of the disclosure, such references do not imply a limitation on the disclosure, and no such limitation is to be inferred. The subject matter disclosed is capable of considerable modification, alteration, and equivalents in form and function, as will occur to those skilled in the pertinent art and having the benefit of this disclosure. The depicted and described embodiments of this disclosure are examples only, and not exhaustive of the scope of the disclosure.
SUMMARYThe present invention is directed to apparatus and methods for monitoring instability of equipment. Specifically, the present invention is directed to apparatus and methods for determining the instability of equipment by measuring the reaction forces at different points at the base of the equipment.
In one exemplary embodiment, the present invention is directed to a method of monitoring the instability of an equipment comprising: symmetrically arranging a plurality of load sensors at a base of the equipment; imposing a Cartesian coordinate system on the base of the equipment; wherein center of the base is origin of the Cartesian coordinate system, wherein the Cartesian coordinate system comprises an X-axis and a Y-axis, and wherein the X-axis and the Y-axis define a plane corresponding to the base of the equipment; designating Cartesian coordinates to each load sensor; determining a reaction force at each load sensor; and determining an overall instability factor for the equipment from the Cartesian coordinates of each load sensor and the reaction force at that load sensor.
In another exemplary embodiment, the present invention is directed to a system for monitoring instability of an equipment comprising: a plurality of load sensors symmetrically arranged on a base of the equipment; an information handling system coupled to the plurality of load sensors, wherein the information handling system determines an overall instability factor for the equipment, and wherein the overall instability factor is determined based on reaction forces at the plurality of load sensors.
The features and advantages of the present disclosure will be readily apparent to those skilled in the art upon a reading of the description of exemplary embodiments, which follows.
DESCRIPTIONThe present invention is directed to apparatus and methods for monitoring instability of equipment. Specifically, the present invention is directed to apparatus and methods for determining the instability of equipment by measuring the reaction forces at different points at the base of the equipment.
The details of the present invention will now be discussed with reference to the figures.
Turning to
As would be appreciated by those of ordinary skill in the art, with the benefit of this disclosure, the load sensors A 204, B 206, C 208 and D 210 may be arranged in a number of different arrangements as long as they are arranged symmetrically. An arrangement of load sensors is considered symmetrical if when the reaction forces are evenly distributed between the load sensors, the resulting reaction force acts through the center of the base (and hence, the center of the load cell pattern) and the instability is zero. For instance,
A simple mathematical processor may manipulate the output of the load sensors to determine the effective center of gravity of base reaction forces. If the effective center of gravity of the base reaction forces lies within the boundaries of the perimeter supports where the load cells are located, then the tank is stable. However as the effective center of gravity of the base reaction forces approaches the support boundaries, the tank becomes more likely to become unstable. When the effective center of gravity of the base reaction forces crosses the support boundary and lies outside the supports, the tank is unstable and likely in the process of overturning. An instability factor is used to represent the potential for tipping. Because the load sensors are symmetrically arranged, when the reaction forces experienced at the load sensors are perfectly symmetrical, the total reaction force acts through the center of the base and the instability is zero. In contrast, when the effective center of gravity of the reaction forces is at the perimeter of the base, the instability factor is 1. Consequently, a user can constantly monitor the stability of the storage tank by tracking the instability factor which is output by the system.
In one exemplary embodiment, a particular instability factor may be preset as the designated threshold instability factor. In this embodiment, an alert in the form of an alarm or other appropriate notification mechanism may be utilized to notify the user when the instability factor exceeds the designated threshold instability factor. In one exemplary embodiment, the system may notify the user that the designated threshold instability factor is reached by transmitting a signal from the system to the user, who may be at a remote location. As would be appreciated by those of ordinary skill in the art, with the benefit of this disclosure, the signal may be transmitted over a wired or wireless network.
Returning now to
The instability factors for the X and Y direction are denoted as IX and IY, respectively, and are determined by multiplying the reaction forces at each load sensor by the respective coordinates to obtain the relative reaction force at each load sensor and summing the resulting relative reaction forces. Specifically, assuming that FA, FB, FC and FD are the reaction forces at the load sensors A 204, B 206, C 208 and D 210, respectively, the instability factors IX and IY are obtained using the following equations:
IX=(−FA+FB−FC+FD)/(FA+FB+FC+FD)
IY=(FA+FB−FC−FD)/(FA+FB+FC+FD)
Using the instability factors in the X and Y directions on the rectangular geometry, the overall instability factor, IA may be determined by the following logic:
If |IX|≧|IY| then IA=|IX| else A=|IY|
As would be appreciated by those of ordinary skill in the art, with the benefit of this disclosure, the same principle may be applied to other geometries by varying the equation used. For instance,
IA=(IX2+IY2)1/2
As would be appreciated by those of ordinary skill in the art, with the benefit of this disclosure, the calculation of the overall instability factor IA quantifies the instability of the storage tank system thereby providing an early indication of instability and opportunities to help manage and/or eliminate the risks involved.
Further, as depicted in
Although the present invention is disclosed in the context of storage tanks, as would be appreciated by those of ordinary skill in the art, with the benefit of this disclosure, the apparatus and methods described herein may be used in conjunction with any other storage units or other mobile or stationary equipment where stability is desirable. For instance, the present apparatus and methods may be used in conjunction with a loaded platform, cranes, fork lifts, etc. Moreover, it would be appreciated by those of ordinary skill in the art, with the benefit of this disclosure, that although the present invention is disclosed in conjunction with a storage tank resting on a base, the same principle may be applied to equipments standing on support legs or wheels.
Therefore, the present invention is well-adapted to carry out the objects and attain the ends and advantages mentioned as well as those which are inherent therein. While the invention has been depicted and described by reference to exemplary embodiments of the invention, such a reference does not imply a limitation on the invention, and no such limitation is to be inferred. The invention is capable of considerable modification, alteration, and equivalents in form and function, as will occur to those ordinarily skilled in the pertinent arts and having the benefit of this disclosure. The depicted and described embodiments of the invention are exemplary only, and are not exhaustive of the scope of the invention. Consequently, the invention is intended to be limited only by the spirit and scope of the appended claims, giving full cognizance to equivalents in all respects. The terms in the claims have their plain, ordinary meaning unless otherwise explicitly and clearly defined by the patentee.
Claims
1. A method of monitoring the instability of an equipment comprising:
- symmetrically arranging a plurality of load sensors at a base of the equipment;
- imposing a Cartesian coordinate system on the base of the equipment;
- wherein center of the base is origin of the Cartesian coordinate system,
- wherein the Cartesian coordinate system comprises an X-axis and a Y-axis, and
- wherein the X-axis and the Y-axis define a plane corresponding to the base of the equipment;
- designating Cartesian coordinates to each load sensor;
- determining a reaction force at each load sensor; and
- determining an overall instability factor for the equipment from the Cartesian coordinates of each load sensor and the reaction force at that load sensor.
2. The method of claim 1, wherein the step of determining an overall instability factor for the equipment using the Cartesian coordinates of each load sensor and the reaction force at that load sensor comprises:
- determining a first instability factor in the direction of the X-axis;
- determining a second instability factor in the direction of the Y-axis; and
- determining the overall instability factor using the first instability factor and the second instability factor.
3. The method of claim 2, wherein determining the first instability factor comprises:
- multiplying the reaction force at each load sensor by Cartesian coordinate of the load sensor on the X-axis to obtain a first relative reaction force at the load sensor;
- obtaining a sum of the first relative reaction forces at the load sensors; and
- dividing the sum of the first relative reaction forces at the load sensors by a sum of the reaction forces at the load sensors.
4. The method of claim 2, wherein determining the second instability factor comprises:
- multiplying the reaction force at each load sensor by Cartesian coordinate of the load sensor on the Y-axis to obtain a second relative reaction force at the load sensor;
- obtaining a sum of the second relative reaction forces at the load sensors; and
- dividing the sum of the second relative reaction forces at the load sensors by a sum of the reaction forces at the load sensors.
5. The method of claim 2, wherein for a rectangular base, the step of determining the overall instability factor using the first instability factor and the second instability factor comprises:
- determining an absolute value of the first instability factor;
- determining an absolute value of the second instability factor; and
- designating the greater of the absolute value of the first instability factor and the absolute value of the second instability factor as the overall instability factor.
6. The method of claim 2, wherein for a circular base, the step of determining the overall instability factor using the first instability factor and the second instability factor comprises determining the square root of the sum of the first instability factor squared and the second instability factor squared.
7. The method of claim 1, wherein the load sensor is selected from the group consisting of an electronic load cell, a hydraulic load cell, a scale, a load pin, a dual sheer beam load cell, a strain gauge, a pressure transducer and combinations thereof.
8. The method of claim 1, further comprising:
- designating a threshold overall instability factor; and
- providing an alert if the overall instability factor exceeds the threshold overall instability factor.
9. The method of claim 8, wherein the step of providing an alert if the overall instability factor exceeds the threshold overall instability factor comprises sounding an alarm.
10. The method of claim 8, wherein the step of providing an alert if the overall instability factor exceeds the threshold overall instability factor comprises transmitting a signal to a user at a remote location.
11. The method of claim 10, wherein the step of transmitting a signal to a user at a remote location comprises transmitting the signal over a wireless network.
12. The method of claim 1, wherein the equipment is a storage tank.
13. A system for monitoring instability of an equipment comprising:
- a plurality of load sensors symmetrically arranged on a base of the equipment;
- an information handling system coupled to the plurality of load sensors,
- wherein the information handling system determines an overall instability factor for the equipment, and
- wherein the overall instability factor is determined based on reaction forces at the plurality of load sensors.
14. The system of claim 13, wherein the equipment comprises a storage tank.
15. The system of claim 13, wherein the load sensor is selected from the group consisting of an electronic load cell, a hydraulic load cell, a scale, a load pin, a dual sheer beam load cell, a strain gauge, a pressure transducer and combinations thereof.
16. The system of claim 13, further comprising a notification mechanism, wherein the notification mechanism provides an alert if the overall instability factor exceeds a preset threshold overall instability factor.
17. The system of claim 16, wherein the notification mechanism comprises an alarm.
18. The system of claim 17, further comprising a network for transmitting the alarm to a user at a remote location.
19. The method of claim 18, wherein the network comprises a wireless network.
20. The method of claim 18, wherein the network comprises a wired network.
Type: Application
Filed: Apr 13, 2009
Publication Date: Oct 14, 2010
Inventors: Bruce C. Lucas (Marlow, OK), Steve Crain (Duncan, OK), Glenn H. Weightman (Duncan, OK)
Application Number: 12/422,450
International Classification: G01D 7/00 (20060101); G01B 5/004 (20060101);