ELECTRIC ACTUATOR HEALTH MONITORING
20230107181 · 2023-04-06
Inventors
Cpc classification
G05B23/0283
PHYSICS
G01M99/00
PHYSICS
G05B23/0235
PHYSICS
H02P29/024
ELECTRICITY
G01R31/008
PHYSICS
International classification
Abstract
A method for monitoring the health of an electromechanical actuator “EMA” includes: generating a reference profile curve that is representative of a required demand of a measurable characteristic of the EMA; defining upper and lower tolerance limits of said reference profile curve; measuring said characteristic of said EMA and generating a measured curve profile based on said measurement; determining if the generated measured profile curve lies within the upper and lower tolerance limits of said reference profile curve; and if said generated measured profile curve does not lie within the upper and lower tolerance limits, providing an indication that said EMA is unhealthy.
Claims
1. A method for monitoring the health of an electromechanical actuator “EMA” comprising: generating a reference profile curve that is representative of a required demand of a measurable characteristic of the EMA, defining upper and lower tolerance limits of said reference profile curve, measuring said characteristic of said EMA and generating a measured curve profile based on said measurement; determining if the generated measured profile curve lies within the upper and lower tolerance limits of said reference profile curve, and if said generated measured profile curve does not lie within the upper and lower tolerance limits, providing an indication that said EMA needs attention.
2. The method of claim 1, wherein said method of providing an indication that the EMA needs attention comprises providing a flag warning into a maintenance computer.
3. The method of claim 1, wherein if said generated measured profile curve does lie within the upper and lower tolerance limits, repeating said method.
4. The method of claim 1, wherein said characteristic comprises one or more of speed versus time, current versus time, voltage versus time or speed versus position.
5. The method of claim 1, further comprising: storing said reference profile curve in a memory of a computer.
6. The method of claim 1, further comprising: defining a frequency and/or test conditions at which future health tests are to be performed.
7. The method of claim 1, wherein said method is performed by a computer.
8. A system for monitoring the health of an electromechanical actuator “EMA”, said system being configured to perform the method of claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0014]
[0015]
[0016]
[0017]
[0018]
[0019]
[0020]
[0021] While the above-identified figures set forth one or more embodiments of the present disclosure, other embodiments are also contemplated, as noted in the discussion. In all cases, this disclosure presents the invention by way of representation and not limitation. It should be understood that numerous other modifications and embodiments can be devised by those skilled in the art, which fall within the scope and spirit of the principles of the invention. The figures may not be drawn to scale, and applications and embodiments of the present invention may include features and components not specifically shown in the drawings.
DETAILED DESCRIPTION
[0022] Described herein are examples of new systems and methods that are configured to utilize data that is currently already available in an aircraft, to control the electric motor in such a way that it is able to assess the health of the electromechanical actuator (EMA) without the need for any additional sensors.
[0023]
[0024] When in use, the electric motor 30 of the EMA 10 is started up, and the motor needs to accelerate in order to reach the required speed. This can be seen in
[0025] As can be seen in
[0026] An unhealthy EMA, or at least an EMA that needs attention, such as that depicted in
[0027] An unhealthy EMA, or at least an EMA that needs attention, may therefore be defined as being an EMA which is experiencing a certain level of drag. Such drag may mechanical drag or magnetic drag. As can be seen from
[0028] By providing a method and system that is configured to compare the measured speed of the motor with a speed demand curve of the motor, it is therefore possible to determine whether or not the EMA is healthy or unhealthy (and experiencing drag), or it at least requires attention before it becomes unhealthy. In this example, the new system and method therefore uses an existing motor speed sensor to determine whether or not an EMA is healthy or not.
[0029] In another example, the method or system may use an existing current sensor to determine whether an EMA is healthy or not.
[0030]
[0031] In a situation wherein the mode of operation is under degradation, however, for example, due to added friction load, the current measurements against the demand will be compromised. This may be due to there being a reduction in the supply voltage, an increase of unbalanced forces due to a bearing failure, or a short circuit of the motor windings.
[0032] This is shown in
[0033] In an alternative embodiment, the sensor that is being used to monitor the health of the EMA may comprise a voltage sensor. When the EMA experiences drag, the measured voltage readings will differ from a voltage demand curve, thereby indicating an unhealthy EMA, or at least an EMA that needs attention.
[0034] Other sensors that are already provided in an EMA may alternatively be used.
[0035] Although each of these sensors can be used individually to determine whether or not an EMA is healthy, the combination of the results of these sensors can also be used, to more accurately and efficiently identify an unhealthy EMA, or an EMA that needs attention.
[0036] For a given EMA the drive current limit is set to overcome this demand under the worst conditions. For example, the worst conditions may be considered to be when the temperature is cold and so drag may be at its highest, thereby meaning that there is a most demanding load condition. In contrast, in an ideal condition, the measured motor speed will align with the demand.
[0037] A new method for determining the health of an EMA using existing sensors that are normally found on an EMA is shown in
[0038] The new systems and methods described herein comprise using a reference demand speed versus position profile to investigate the health of the system. In order to do this, the system may be configured to perform the method 100 steps of generating 110 a speed versus position curve for a new electrically driven actuator. This speed versus position curve is later used as the reference curve for monitoring and determining the health of the EMA. The method may further comprise storing 120 the reference curve in a memory as a reference. The method may further comprise 130 defining limits the curve beyond which a maintenance flag should be raised. That is, the curve should have defined upper and lower tolerance limits. The method may further comprise 140 defining the frequency at which future health tests need to be performed, as well as the test conditions. That is, the method may define a mean, frequency and condition to measure the system speed demand taking into account load conditions etc. that would impact the curve in reality. The maximum and minimum tolerances that are acceptable should be taken into account. The method may further comprise 150 measuring the actual motor speed versus movement demand for a defined condition. The method may further comprise 160 determining if the generated curve is within the defined calculated reference curve for a given working condition. If the answer is no, the method performs the step 170 of providing a flag warning into a maintenance computer and continuing monitoring. If the answer is yes, then the method may comprise the step 180 of doing nothing. The method may then repeat from 110 onwards again.
[0039] The examples described herein allow for an increase in health monitoring of EMAs that may provide advanced notice of oncoming faults and which reduce Aircraft on Ground (AOG) and dispatch interruption. By improving the detection capability of a potentially failing component prior to it failing then it is possible to reduce AOG as the customer can plan replacement hardware in advance of the component failing. The examples are also able to utilize existing system hardware without the requirement for additional sensing.
[0040] While the invention has been described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.