Patent Grant
11525417
This application is a U.S. national stage filing under 35 U.S.C. § 371 from International Application No. PCT/EP2018/072484, filed on 21 Aug. 2018, and published as WO2019/042813 on 7 Mar. 2019, which claims the benefit under 35 U.S.C. 119 to European Application No. 17189064.3, filed on 1 Sep. 2017, the benefit of priority of each of which is claimed herein, and which applications and publication are hereby incorporated herein by reference in their entirety.
Embodiments of the present invention relate to methods and control devices for physical and chemical apparatuses in which undesired oscillations may emerge spontaneously due to a feedback coupling, in particular to methods and control devices for a combustion apparatus.
Feedback coupling is inherent to many practical systems, and leads to oscillatory states (periodic states such as limit cycles and aperiodic states such as chaos) that may adversely affect the stability and safety of the systems such as an apparatus or even a whole plant. For example, a so-called thermoacoustic coupling may occur in apparatuses (systems) such as gas turbine engines, furnaces, boilers, rocket engines, and afterburners that are driven by confined combustion. Thermoacoustic coupling may lead to a self-excited instability, (also known as combustion instability, rumble, and reheat buzz), which appears spontaneously in the form of large amplitude pressure and heat release rate oscillations. The instability may be hazardous for the apparatus. Therefore, it is often desirable to suppress the thermoacoustic instabilities. Previously used control attempts (implicitly) assumed that the thermoacoustic instabilities correspond to limit cycle oscillations, possibly with harmonics. Therefore, the fact that the thermoacoustic system can undergo bifurcations to more complex nonlinear states, such as chaos is not taken into account. In fact, it is even possible that at onset of the instability when the system has just crossed the stability boundary, thermoacoustic oscillations correspond to a chaotic state. Previous methods will fail outright in such a scenario.
Accordingly, there is a need to improve control/suppression of instabilities.
According to an embodiment of a method for controlling a combustion apparatus having a combustion state in which a parameter related to the combustion state reflects a chaotic behavior, the method includes measuring the parameter and determining a time series of the parameter. The time series is shifted by a variable time delay for determining a time-shifted signal, and for forming a difference between the time-shifted signal and the time series for determining a time dependent first signal, so that a norm of the difference between the time-shifted signal and the time series is lowest. A time dependent second signal different to the first signal is determined. Determining the time dependent second signal includes at least one of using a frequency of a desired periodic combustion state of the combustion apparatus, and shifting the time series by a set time delay. The first signal and the second signal are combined for determining a control signal. The control signal is used to influence the combustion apparatus.
In the following, the difference between the time-shifted signal and the time series is also referred to as (time dependent) difference signal.
In the following, the combustion state in which the parameter related to the combustion state reflects a chaotic behavior, typically a chaotic thermoacoustic instability, is also referred to as chaotic combustion state and chaotic state of combustion, respectively.
The term “chaotic state” as used in this specification intends to describe a state of a system or apparatus exhibiting an aperiodic long-term behaviour with sensitive dependence on initial conditions. The term “aperiodic long-term behaviour” intends to describe that in the asymptotic dynamics the system or apparatus does not correspond to a fixed-point, a periodic orbit or a quasi-periodic behaviour. The system or apparatus may be (describable as) a non-linear deterministic system or apparatus, i.e. a system or apparatus in which the chaotic behaviour is not due to noisy or random forces, but rather due to the nonlinearity present in the system or apparatus, in particular a nonlinearity in the feedback coupling mechanism associated with thermoacoustic instability in the system or apparatus. The term “sensitive dependence on initial conditions” intends to describe that nearby initial conditions separate exponentially fast while the system or apparatus evolves in time.
The method allows transferring the combustion apparatus from the chaotic combustion state into a periodic combustion state, and subsequently into a periodic state with a dominant frequency (of the parameter) shifted to the frequency of the desired oscillating state and/or a periodic state with reduced amplitude of oscillations compared to the initial state. Accordingly, hazardous instabilities of the combustion apparatus such as high mechanical loading can reliably be dampened or even suppressed. Further, other undesired effects that may occur in the chaotic state such as deterioration of exhaust values and exceeding of desired exhaust values, respectively, e.g. increased nitrogen oxide(s) (NOx), may be avoided.
The first signal is effective to drive the combustion apparatus from a chaotic combustion state into a periodic combustion state.
Using a desired main frequency of the desired periodic combustion state for determining the second signal and, thus, the control signal of the combustion apparatus, allows driving the combustion state towards, more typically into the desired combustion state. Further, a damping of the amplitude of the oscillation of the parameter may be achieved.
Shifting the time series by a set time delay (τset which is different to the variable time delay τvar used to determine the time dependent first signal and the difference signal, respectively) to determine the second signal and, thus, the control signal of the combustion apparatus, also allows changing the dominant frequency of the combustion state as well as damping the amplitude of the oscillation of the parameter. Note that the set time delay (τset) determines the shift in the dominant frequency of the periodic combustion state.
Whether an open-loop control based on the desired main frequency or a feed-back control using a set time delay (τset) is more efficient to drive the apparatus into the desired periodic combustion state may depend on the details of the apparatus.
Both the variable time delay (τart) for the first signal S1 and the set time delay (τset) for the second signal S2 will typically be of the order of the time-period of the acoustic resonance frequency of the apparatus.
The set time delay (τset) may be determined based on mechanical, geometrical, chemical and/or thermodynamic properties of the combustion apparatus. For example, the set time delay may be determined based on the acoustic resonance frequency of the combustion apparatus.
The parameter may be any variable or observable that participates in the chaotic behaviour of the thermoacoustic oscillations.
The term “thermoacoustic oscillations” intends to describe fluctuations and/or oscillations in a medium such as a gas which are due to a feedback interaction between an acoustic field in the medium, and temporal fluctuations in the heat release rate from combustion (or from a flame). The term “thermoacoustic oscillations” shall embrace oscillations in a flame (and associated quantities such as the unsteady heat release rate from the flame), and in an acoustic field within an apparatus at least partly enclosing the flame, typically within a combustion chamber of the apparatus, that emerge spontaneously due to a constructive feedback interaction between the flame and the acoustic field.
The parameter may be a pressure in the apparatus, a temperature in the apparatus, a density in the apparatus, a radiation power of the combustion (typically a chemiluminescence from the flame) or a parameter related to one or more of the pressure, the temperature, the density and the radiation power.
Typically, the parameter is the pressure. The pressure in the apparatus can reliably be measured with high temporal resolution.
The measured values of the parameter are typically high-pass filtered. Accordingly, a (long-term) drift of the parameter is eliminated.
The norm of the difference signal may be determined as an integral or a sum of (all) absolute amplitude values of the difference signal, e.g. as sum absolute pressure values. Alternatively, a root mean square value of the amplitude values of the difference signal may be determined as norm of the difference signal.
To determine the first signal, the variable time delay is typically varied starting from a value close the inverse of the dominant frequency in the oscillations until the norm of the difference signal reaches a minimum value, typically a global minimum value.
Accordingly, the amplitude of the first signal is small, typically close to zero if the apparatus is in a periodic state. Thus, the proposed controlling does not require analyzing the state of the apparatus and/or switching on and off the first signal.
In one embodiment, determining the time dependent first signal includes determining a difference between a first subset of the time series and a second subset of the time series, wherein the variable time delay between the first second subset and the second subset is determined so that so that a norm of the difference signal determined as difference between the first subset and the second subset is lowest.
Combining the first signal and the second signal is typically achieved by adding the first signal and the second signal or by forming a weighted sum of the first signal and the second signal.
However, other functions F of the first signal and the second signal may also be used as control signal.
Using the control signal may include feeding the input signal to an actuator coupled with the combustion apparatus.
Using the control signal may also include converting the control signal to an input signal for the actuator and feeding the input signal to the actuator. For example, the input signal may be a time dependent voltage.
For reasons of safety (for the actuator employed), the control signal or the input signal may be saturated prior to feeding to the actuator.
Converting and/or saturating the control signal may also already be achieved during combining the first signal and the second signal using an appropriate function (F).
The actuator is typically configured to convert the input signal, which is in the following also referred to as primary control signal into a secondary control signal suitable to influence the combustion apparatus.
Typically, the primary control signal and the secondary control signal, respectively, may be used to modulate a fuel-oxidant ratio, e.g. a fuel-air ratio, of fuel and oxidant used in the combustion apparatus for combustion.
This may be achieved by modulating a flow rate of the fuel and/or a flow rate of the oxidant.
Modulating the fuel-oxidant ratio may be achieved with little additional expense and has been found to be efficient for transferring the combustion apparatus from the chaotic combustion state into a non-chaotic combustion state.
Alternatively or in addition, the control signal or the saturated control signal may be converted into an acoustic signal, and the acoustic signal may be applied to the combustion apparatus.
Typically, the method is performed in a cyclic manner and/or a continuously.
Furthermore, the time series may be analyzed to determine a characteristic of a current combustion state, to change an input parameter of the function (F), e.g. increase a gain or weight of first signal if the current combustion state is still chaotic, and/or to change the set time delay.
The characteristic may be a measure of non-periodicity, a distance from a bifurcation or the like.
The characteristic may also be a fluctuation characteristic, in particular a measure for the amplitude oscillations such as a root-mean-square value (rms-value) of the measured values of the parameter or a measure of statistical dispersion of the measured values of the parameter such as the standard deviation. The fluctuation characteristic may be used to decide if the controlling is to be switched on.
According to an embodiment of a control device, the control device includes a sensor for measuring a parameter related to a combustion state of a combustion apparatus, a controller coupled with the sensor, and an actuator coupled with the controller. The controller is configured to receive measured values of the parameter from the sensor and to determine a time series from the measured values of the parameter, to shift the time series by a variable time delay for determining a time-shifted signal, and form a difference between the time-shifted signal and the time series for determining a time dependent first signal, so that a norm of the difference between the time-shifted signal and the time series is lowest, to determine a time dependent second signal different to the first signal, wherein the second signal is determined based on a frequency of a desired oscillating state of the combustion apparatus and/or wherein determining the second signal comprises shifting the time series by a set time delay, and to outputting a function (F) of the first signal and the second signal as a primary control signal. The actuator is configured to convert the primary control signal into a secondary control signal suitable to influence the combustion apparatus.
For example, the control device may be configured to vary the variable time delay, determine (a corresponding time-shifted signal and) a corresponding difference signal until the norm of the difference signal is lowest and reaches a minimum value, respectively, to determine the time dependent first signal.
In the following the control device is also referred to as controller.
Typically, the control device is configured to perform any of the methods described herein.
The controller may include an observer unit configured to determine a characteristic of a current state of the combustion apparatus using the time series of the parameter.
The observer unit may further be configured to change an input parameter of the function (F) and/or to change the set time delay.
The sensor is typically a pressure sensor, a temperature sensor or a light sensor.
The sensor may provide the measured values of the parameter as respective voltage values.
The actuator may be an acoustic actuator, an electromagnetically driven membrane, a valve, for example a fast-response valve, or a pump.
According to an embodiment, a controlled system includes a chamber, typically combustion chamber, and the control device coupled with the chamber.
Typically, the controlled system forms a jet engine, a gas turbine engine, a furnace, a boiler, rocket engine, or an afterburner.
The components in the figures are not necessarily to scale, instead emphasis being placed upon illustrating the principles of the invention. Moreover, in the figures, like reference numerals designate corresponding parts. In the drawings:
In the following Detailed Description, reference is made to the accompanying drawings, which form a part hereof, and in which is shown by way of illustration specific embodiments in which the invention may be practiced. In this regard, directional terminology, such as “top,” “bottom,” “front,” “back,” “leading,” “trailing,” etc., is used with reference to the orientation of the Figure(s) being described. Because components of embodiments can be positioned in a number of different orientations, the directional terminology is used for purposes of illustration and is in no way limiting. It is to be understood that other embodiments may be utilized and structural or logical changes may be made without departing from the scope of the present invention. The following detailed description, therefore, is not to be taken in a limiting sense, and the scope of the present invention is defined by the appended claims.
Reference will now be made in detail to various embodiments, one or more examples of which are illustrated in the figures. Each example is provided by way of explanation, and is not meant as a limitation of the invention. For example, features illustrated or described as part of one embodiment can be used on or in conjunction with other embodiments to yield yet a further embodiment. It is intended that the present invention includes such modifications and variations. The examples are described using specific language which should not be construed as limiting the scope of the appending claims. The drawings are not scaled and are for illustrative purposes only. For clarity, the same elements or manufacturing steps have been designated by the same references in the different drawings if not stated otherwise.
With reference to
In the exemplary embodiment, the controlled apparatus or system 150 consists of a combustion apparatus 50 and a control device 100 coupled with the combustion apparatus 50.
In the following the combustion apparatus 50 is also referred to as combustor 50.
A sensor 110 of the control device 100 is coupled with the combustor 50 to measure a parameter p related to a combustion state of the combustion apparatus 50 at different times t, for example pressure fluctuations.
The sensor 110 is further coupled with a controller 120 of the device 100 so that the controller 120 can receive measured values p1(t) of the parameter p.
The controller 120 may receive one measured values, typically several measured values p1 per control cycle or a set of measured values p1 per control cycle.
Further, the controller 120 may determine time series S0(t) of the measured values p1(t) of the parameter p. This may include appending the measured value(s) p1(t) as or to an end of a storage structure such as an array, and an optional subsequent high-pass filtering.
Based on the time series S0(t), the controller 120 may determine a primary control signal S(t) that is fed to an actuator 130 of the control device 100.
The actuator 130 is connected with the controller 120 and coupled with the combustor 50.
Accordingly, the actuator 130 may convert the primary control signal S(t) into a secondary control signal p2(t) that is used to influence the combustion apparatus 50 in such a way that a chaotic combustion state of the combustion apparatus 50 is left and/or that the combustion apparatus 50 reaches a desired (non-chaotic) combustion state.
For example, a fuel-oxidant ratio of the combustion apparatus 50 may be modulated using the secondary control signal p2(t).
As illustrated in
The first signal S1(t) may be determined by the controller 120 as follows.
A variable time delay τvar may be initialized with a small value. Alternatively, the variable time delay τvar may be initialized with a value close to a time-period which corresponds to a frequency of a dominant peak in the spectrum of the parameter.
Thereafter, a time-shifted signal Sτ(t) may be determined. Typically, the time-shifted signal Sτ(t) is determined by time-shifting the time series S0(t) by the variable time delay τvar:
Sτ(t)=S0(t−τvar)
Thereafter, a difference signal SΔ(t, τvar)=Sτ(t)−S0(t)=S0(t−τvar)−S0(t) may be determined.
Thereafter, a norm|SΛ(t, τvar)| of the difference signal SΛ(t, τvar) may be determined.
Thereafter, the variable time delay τvar may be changed and the processes for determining the difference signal may be repeated using the variable time delay τvar.
Changing the variable time delay τvar and determining the difference signal SΔ(t, τvar) are typically repeated until the norm of the difference signal SΔ(t, τvar) reaches a smallest value. The finally determined difference signal SΔ may be used as the first signal S1.
Different thereto, the second signal S2(t) may be determined by the controller 120 based on the frequency of a desired periodic state of the combustion apparatus 50. In this embodiment, the second signal S2(t) is an open-loop control signal SOL(t).
Alternatively, or in addition, the second signal S2(t) may be based on the time series S0(t) and a set time delay τset.
For example, the second signal S2(t) may be determined as delayed time series S0(t−τset) or as a superposition SOL(t)+S0(t−τset) or weighted superposition.
According to an embodiment, the controller 120 is a two-stage controller that outputs a function F(S1(t), S2(t) {ak}) as control signal S(t).
Typically, F is a linear function: F (S1(t), S2(t) {ak})=a1 S1(t)+a2 S2(t) with weights (gains) a1, a2 ({ak}). The gains may be changed in time to achieve the desired combustion state. For example, a2 may be set to 0 as long as the τvar optimization is performed.
A first of the two stages 121, 122 of the controller 120 is a feed-back control stage 121 and determines the first signal S1(t).
A second of the two stages 121, 122 of the controller 120 determines the second signal S2(t).
For example, the second stage 122 may determine the second signal S2(t) as a weighted sum of an open-loop control signal SOL(t) and a feedback signal SFB(t): S2(t)=b1 SOL(t)+b2 SFB(t), with weights (gains) b1, b2({bi}).
Thus, the second stage 122 may be (may operate as) a feed-back control stage (b1=0) or an open-loop control stage (b2=0).
However, the second stage 122 may be (may operate as) a combined control stage (b1≠0, b2≠0).
The open-loop control signal SOL(t) may be determined as a time periodic function H having a period which is inversely related to a (main) frequency (fOL) of a desired periodic combustion state: SOL(t)=H(t, fOL), such as a sinus function sin(2π*fOL*t).
The feedback signal SFB(t) may be determined as time series S0(t) shifted by the set time delay τset: SFB(t)=S0(t−τset).
In other words, the controller 120 may also output a function G(S0(t), {ak, bi}, τset) as control signal S(t) as illustrated in
The set time delay τset may be modified till the combustion apparatus 50 reaches a desired combustion state with a desired frequency.
As further illustrated in
Depending on the characteristic, the observer unit 115 may change the function parameters {ak, bi}, τset explained above with respect to
For example, the observer unit 115 may increase the weight a1 if the characteristic indicates that the current state is still chaotic.
Further, the observer unit 115 may decide to activate the controlling only (e.g. by assigning non-zero values to the weights a1 and/or a2) if desired, e.g. if a fluctuation characteristic is above a respective threshold.
Likewise, the observer unit 115 may be configured to deactivate the controlling or part thereof based on the characteristic(s).
The observer unit 115 may also be an integral part of the controller 120.
In a block 1010, a parameter (p) which is related to the combustion state such as a pressure in a combustion chamber or a (fluidically) connected upstream or downstream duct such as an exhaust pipe, for example a sound pressure, a temperature in the combustion chamber or the upstream or downstream duct, a temperature of a flame, and a radiation power of the flame is measured to obtain measured values (p1) and therefrom a time series S0(t) of the parameter (p).
In a subsequent block 1020, a control signal S(t) may be determined on the basis of the time series S0(t). This is typically achieved as explained above with regard to
In a subsequent block 1030, the control signal S(t) is used to influence the combustion apparatus 50.
For example, the control signal S(t) may be fed to a suitable actuator such as an electromagnetically driven membrane or a valve of the combustion apparatus to modulate a fuel-oxidant ratio of the combustion apparatus.
As illustrated by the dashed arrow in
In the exemplary embodiment, the combustion apparatus 450 has two vertically orientated ducts 412, 414, typically steel ducts. The total length of the duct 412, 414 may be larger than 1 m and an inner diameter may be larger than about 10 cm.
Reactants, fuel and air in the exemplary embodiment, are injected at the bottom of the first (lower) duct 412 as indicated by the dashed arrows. Prior to passing the upper duct 414, the flow may meet a perforated plate 413 employed as a holder to stabilize the flame in the upper duct 414. The plate 413 may e.g. have a hexagonal pattern of the holes.
Considering a one-dimensional configuration in longitudinal direction, the flame remains stationary as the flame speed is equal to the speed of the unburnt flow at the flame location. By using perforated plates 413 as burners in a cross section of the reactant gas flow, heat is lost from the flame and the burning velocity decreases until it equals the unburnt mixture velocity. Therefore, a stable laminar flat flame confined in the upper duct 414 forming a combustion chamber is produced over a range of conditions.
However, hazardous self-excited instabilities may occur due to thermoacoustic coupling. For example, a constructive feedback coupling between unsteady fluctuations in the flame and the acoustics of the combustion chamber (formed by upper duct 414)—plenum (formed by lower duct 412) assembly.
A microphone 410 is attached to the lower duct 412 as sensor for measuring the pressure in the lower duct 412.
Alternatively, the microphone may be attached to the upper duct 414.
Furthermore, several microphones may be used as sensors.
In the exemplary embodiment, measured pressure values p1(t) may be transferred from the microphone 410 to the two stages 421, 422 of the two-stage controller 421, 422.
The controller stage 421 is implemented as feed-back control stage and configured to determine a first signal S1(t) as explained above with regard to
The controller stage 422 may have two subunits (sub-stages) 422a, 422b. The subunit 422a may determine the second signal S2(t) as open-loop control signal SOL(t), and subunit 422b may determine the second signal S2(t) a feedback signal SFB(t) as explained above with regard to
Depending on the switch setting of the illustrated switch of the controller stage 422, the controller stage 422 may either provide the open-loop control signal SOL(t) (when the switch is in the switch setting shown in
In the exemplary embodiment, each of the controller stages 421, 422 is connected with a corresponding compression driver 430 acting as actuators which are coupled with the lower duct 412. The actuators 430 are typically placed at identical axial distance from the flame in the duct 414.
The compression drivers 430 typically include a respective electromagnetically driven membrane. Accordingly, the combustion process may be influenced sufficiently powerful and swift. The (voltage) signals S1(t), S2(t), and S(t), as described above may be used to generate a corresponding motion of the membrane. The motion of the membrane in turn generates pressure fluctuations that influence the thermoacoustic coupling between the acoustic field within the ducts 412, 414 and the flame.
Alternatively, the controller stages 421, 422 may be coupled with a common compression driver 430.
After switching-on the controller stages 421, the chaotic combustion state is left as indicated by the resulting spectrum b.
After further switching-on the controller stages 422 in the switch setting shown in
It can be shown experimentally, that periodic combustion behavior can be locked to a desired frequency by changing the delay of the phase shift feedback (using sub stage 422b) or by changing the frequency of the open loop (using sub stage 422a). This may be particularly helpful for instance in combustors employing passive devices, which usually feature narrowband damping defined by their geometrical characteristics.
With the control devices described herein, the frequency of the instability can be adjusted to fall within the frequency band where the installed passive methods are effective.
Furthermore, the control device can be easily adjusted to follow (adapt to) any changes in the damper properties induced by changes in the operating conditions of the combustor.
Method 2000 includes the blocks 2010, 2020 and 2030 which typically correspond to the respective blocks 1010, 1020 and 1030 of method 1000.
Furthermore, after measuring values p1(t) of the parameter in block 2010, the obtained time series S0(t) is initially analyzed in a block 2015 of method 2000.
For example, a value th representing amplitude fluctuations of the time series S0(t) (or the measured parameter values p1(t)) may be analyzed in a sub block 2015a of block 2015.
If the value th is above a predetermined threshold th1, control block 2020 may be activated. Otherwise, method 2000 may return from sub block 2015c of block 2015 to block 2010.
Furthermore, based on the analysis in block 2015a, it may be decided in sub block 2015c to change one or more of the function parameters {ak, bi}, τset, fOL explained above, when the value th is above the threshold th1. Accordingly, current values of the function parameters {ak, bi}, τset, fOL may be updated in sub blocks 2016 and 2017 of block 2020, respectively.
Furthermore, it may be decided based on the analysis in block 2015a to change in a sub block 2018 of block 2020 a switch setting and, thus, how the open-loop control signal SOL(t) determined in a sub block 2022a of block 2020 and the feedback signal SFB(t) determined in a sub block 2022b of block 2020 are combined for forming the second signal S2(t).
Similar as explained above with regard to
The resulting primary control signal S(t) may be converted in a sub block 2031 of block 2030 into a secondary control signal p2(t) that is used in sub block 2032 of block 2030 to influence the combustion apparatus and the combustion state of the combustion apparatus, respectively.
Thereafter, method 2000 may return to block 2010.
According to an embodiment of a method for controlling a chemical reaction in a state in which a parameter related to the chemical reaction reflects a chaotic behavior, the method includes measuring the parameter and determining a time series of the parameter. The time series is shifted by a variable time delay and a difference between the time-shifted signal and the time series is formed for determining a time dependent first signal, so that a norm of the difference between the time-shifted signal and the time series is lowest. A time dependent second signal is formed, wherein determining the time dependent second signal includes at least one of using a frequency of a desired oscillating state of chemical reaction and shifting the time series by a set time delay. The first signal and the second signal are combined for determining a control signal. The control signal is used to influence the chemical reaction.
Typically, the chemical reaction exhibits a self-excited instability (to be controlled). The self-excited instability may be due to thermoacoustic coupling. Accordingly, the chemical reaction may be an exothermic chemical reaction, more typically a combustion (reaction). The chemical reaction may also be so a called (nonlinear) chemical oscillator.
Typically, the chemical reaction is controlled under at least partially confined conditions, more typically in a reactor or a chamber, for example a combustion chamber.
It is however also conceivable that the methods described herein are used for a physical system having a self-excited instability such as pulsed combustors, lasers, thermal convection loops, and other natural and artificial systems where chaotic oscillations may appear and are desired to be controlled via an external stimulus (perturbation).
According to an embodiment of a method for influencing a self-excited instability of a chemical or physical system, in particular a respective artificial system, for example a thermoacoustic instability of a combustor, the method includes measuring a parameter related to the thermoacoustic instability and determining a time series of the parameter, determining a control signal, and using the control signal to influence the instability. Determining the control signal includes determining a time dependent first signal as a difference signal between the time series and a time-shifted signal, which is time-shifted with respect to the time series so that a distance, between the time series and the time-shifted signal is lowest, determining a time dependent second signal different to the first signal, and at least one of determining a function of the first signal and the second signal such as a sum or weighted sum, and combining the first signal and the second signal. Determining the second signal includes shifting the time series by a set time delay and/or using a desired frequency of the chemical or physical system. The control signal is typically used to influence the chemical or physical system and the self-excited instability, respectively.
According to an embodiment of a control device, the control device includes a sensor for measuring a parameter related to a self-excited instability of a chemical or physical system, for example a thermoacoustic instability in a combustor, a controller coupled with the sensor, and an actuator coupled with the controller. The controller is configured to receive measured values of the parameter from the sensor and to determine a time series from the measured values of the parameter, to shift the time series by a variable time delay for determining a time-shifted signal, and to form a difference between the time-shifted signal and the time series for determining a time dependent first signal, so that a norm of the difference between the time-shifted signal and the time series is lowest, and to determine a time dependent second signal different to the first signal. The second signal may be based on a frequency of a desired periodic state of the chemical or physical system and/or on shifting the time series by a set time delay. The control device is further configured to output a function (F) of the first signal and the second signal as a primary control signal. The actuator is configured to convert the primary control signal into a secondary control signal suitable to influence the chemical or physical system and the self-excited instability, respectively.
Although various exemplary embodiments of the invention have been disclosed, it will be apparent to those skilled in the art that various changes and modifications can be made which will achieve some of the advantages of the invention without departing from the spirit and scope of the invention. It will be obvious to those reasonably skilled in the art that other components performing the same functions may be suitably substituted. It should be mentioned that features explained with reference to a specific figure may be combined with features of other figures, even in those cases in which this has not explicitly been mentioned. Such modifications to the inventive concept are intended to be covered by the appended claims.
Spatially relative terms such as “under”, “below”, “lower”, “over”, “upper” and the like are used for ease of description to explain the positioning of one element relative to a second element. These terms are intended to encompass different orientations of the device in addition to different orientations than those depicted in the figures. Further, terms such as “first”, “second”, and the like, are also used to describe various elements, regions, sections, etc. and are also not intended to be limiting. Like terms refer to like elements throughout the description.
As used herein, the terms “having”, “containing”, “including”, “comprising” and the like are open ended terms that indicate the presence of stated elements or features, but do not preclude additional elements or features. The articles “a”, “an” and “the” are intended to include the plural as well as the singular, unless the context clearly indicates otherwise.
With the above range of variations and applications in mind, it should be understood that the present invention is not limited by the foregoing description, nor is it limited by the accompanying drawings. Instead, the present invention is limited only by the following claims and their legal equivalents.
| Number | Date | Country | Kind |
|---|---|---|---|
| 17189064 | Sep 2017 | EP | regional |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2018/072484 | 8/21/2018 | WO |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2019/042813 | 3/7/2019 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 10095247 | Unni | Oct 2018 | B2 |
| 20180283305 | Urano | Oct 2018 | A1 |
| Number | Date | Country |
|---|---|---|
| 1429003 | Jun 2004 | EP |
| 101667104 | Oct 2016 | KR |
| WO-8503761 | Aug 1985 | WO |
| WO-2019042813 | Mar 2019 | WO |
| Entry |
|---|
| “International Application No. PCT/EP2018/072484, International Search Report and Written Opinion dated Nov. 20, 2018”, (dated Nov. 20, 2018), 12 pgs. |
| Number | Date | Country | |
|---|---|---|---|
| 20200200110 A1 | Jun 2020 | US |
