CN118965819B - Wind turbine reliability assessment method, device and medium - Google Patents
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Abstract
The invention belongs to the technical field of electric power, and discloses a reliability assessment method, a device and a medium of a wind turbine, wherein the method comprises the steps of establishing a degradation-impact dependent competition failure model of each component of the wind turbine taking self-healing into consideration according to a nonlinear wiener process and a Markov principle, establishing a multi-failure model of each component of the wind turbine based on a multi-dimensional Copula function, selecting the Copula function, establishing a correlation model of failure among different components of the wind turbine, and carrying out parameter estimation on degradation and the Copula function based on a maximum likelihood method and a Monte Carlo method. The reliability curve of each component and system of the wind turbine can be obtained, and further the reliability of the wind turbine can be evaluated.
Description
Technical Field
The invention relates to the technical field of electric power, in particular to a method, a device and a medium for evaluating reliability of a wind turbine.
Background
Wind power generation is one of the most promising power generation modes in the field of new energy, and has complex structure composition and high coupling degree. Meanwhile, the working environment of the wind turbine generator is complex and changeable in service, and is often subjected to various stress load effects, so that the failure modes of the wind turbine generator are characterized by complexity, concealment and the like, and the failure modes are often the competing results of various failure modes. At present, competition failure aiming at multiple failure modes is often in extreme weather, and the problem that reliability assessment of a wind turbine generator is inaccurate and the like is caused because characteristics of recovery after impact of components of the wind turbine generator on the polar ends are not considered.
Disclosure of Invention
The invention provides a reliability evaluation method, a device and a medium for a wind turbine generator. In addition, in order to solve the problem of relevance of failure among the components of the wind turbine, the relevance among different components is obtained by establishing a multidimensional Archimedes Copula function model, and the reliability curves of the wind turbine system and the components are obtained by carrying out parameter estimation on the degradation quantity and Copula function model by using the maximum likelihood number and the Monte Carlo method.
The invention adopts the following technical scheme:
according to a first aspect of the present invention, there is provided a method for evaluating reliability of a wind turbine, the method comprising:
According to a nonlinear wiener process and a Markov principle, establishing a degradation-impact dependent competition failure model of each component of the wind turbine generator set considering self-healing;
Based on the multidimensional Copula function, establishing a multi-fault failure model of each component of the wind turbine generator;
Selecting a Copula function and establishing a failure correlation model among different components of the wind turbine generator;
And carrying out parameter estimation on the degradation amount and the Copula function based on a maximum likelihood method and a Monte Carlo method.
As an optimal technical scheme, the self-healing degradation-impact dependent competition failure model of each component of the wind turbine comprises a natural degradation model of the wind turbine, a random impact process model and a self-healing model of each component of the wind turbine, and the self-healing degradation-impact dependent competition failure model of each component of the wind turbine is established according to a nonlinear wiener process and a Markov principle, and the self-healing degradation-impact dependent competition failure model comprises the following steps:
establishing a natural degradation model of the wind turbine according to the nonlinear wiener process;
Establishing a random impact process model based on a Markov principle;
And establishing a self-healing model of each component of the wind turbine according to the natural degradation model and the random impact process model of the wind turbine.
As an optimal technical scheme, the method for establishing the natural degradation model of the wind turbine generator according to the nonlinear wiener process comprises the following steps:
the degradation model of the nonlinear wiener process is established as a natural degradation model of the wind turbine, and is expressed as follows:
;
Wherein: Representative of Degradation amount of time degradation process; as a drift coefficient, representing the degradation rate; As a non-decreasing time scale function, representing a nonlinear characteristic of the degradation process, Represents the amount of dimensional change per unit time,As a function of the drift,As a parameter of the time scale of the time,Is the diffusion coefficient; is a standard Brownian motion;
converting a closed expression of a probability density function of a natural degradation model of the wind turbine generator into a first-pass distribution probability solving problem that the standard Brownian motion exceeds a time-varying threshold value, and obtaining an approximate analytical formula of natural degradation failure is as follows:
;
Wherein: representing a natural degradation failure function, A time-varying threshold function is represented,Representing a given critical degradation failure threshold value,An exponential function based on e;
The cumulative distribution function approximation calculation formula of the distribution at the time of first pass is as follows:
;
Wherein: Representation of A cumulative distribution function of the distribution at the first pass threshold,The probability function is represented as a function of the probability,Indicating the moment at which the threshold value is reached,Is a composite function, representing a natural degenerate failure function,Representing a cumulative distribution function.
As a preferred technical solution, establishing a random impact process model based on a markov principle includes:
For the first Performance parameters, assuming Markov chains satisfying the 0-1 state for impact generation and natural degradation, are usedA representation state, expressed as:
;
describing the state transition process of the performance parameters by using the state transition matrix of the Markov chain to show the probability of mutual transition between different states, and if the current state is the occurrence of the impact, keeping the probability of the impact at the next moment as The probability of returning to natural degradation isAnd (2) andIf the current state is natural degradation, the probability of remaining natural degradation at the next moment isThe probability of impact occurrence isAnd (2) and;
Based on natural degradation and impact effect, will beDegradation of performance parametersExpressed as:
;
Wherein: To represent the degradation amount of the natural degradation process of the p-th performance parameter at time t, Is the additional degradation amount caused by impact at the t moment, the impact degradation amount,Subject to independent and identical expectationsVariance isIs a normal distribution of (c).
As an optimal technical scheme, the method for building the self-healing model of each component of the wind turbine according to the natural degradation model and the random impact process model of the wind turbine comprises the following steps:
When the system is subjected to the first Self-healing occurs after secondary impact, and the actual damage amount after self-healing of the system at the moment t is determined by the following formula:
;
Wherein: Is the first Duration of the secondary impact; is a self-healing influence function; Is the first The amount of degradation of the secondary impact;
determining the accumulated damage amount of the system at the moment t by the following formula :
;
Wherein: Is the first Duration of the secondary impact; Is the first The amount of degradation of the secondary impact is,Is the number of times of arrival of the impact.
As an optimal technical scheme, based on a multidimensional Copula function, a multi-fault failure model of each component of the wind turbine generator is established, and the method comprises the following steps:
determining a Copula function based on the joint distribution function and the edge distribution function of the multidimensional random variable The following relation is satisfied:
;
Wherein: In order to combine the functions of the distribution, As a function of the distribution of the edges,The degradation amount of the nth component of the wind turbine generator is the Copula function if the edge distribution function is continuousIs a deterministic function, if the edge distribution function is a unitary distribution, F (, ⋯,) is a joint distribution function with an edge distribution F 1(⋅) , F2(⋅) ,⋯, Fn (;
If the first wind turbine generator system H fault modes exist in each component, multiple coupling relations exist among the fault modes, k fault modes with multiple coupling relations exist, h-k fault modes with independent relations exist, and the corresponding joint distribution function is determined to be expressed as:
;
Wherein: For the life of the corresponding component, For a joint distribution function with a multiple coupling relationship,Component life for failure modes with multiple coupling relationships is less than nominal life,Component rated life for failure mode with multiple coupling relationships;
Establishing a k-dimensional Copula function Expressed as
;
Wherein: For all component rated life joint distribution functions with k multiple coupling relationship failure modes, For the ith component life distribution function with k multiple coupling relationship failure modes,Is a cumulative distribution function;
at the initial time, the component has no fault state, then The reliability of the individual components is:
;
Wherein, Is the firstThe degree of reliability of the individual components,As a function of the probability of occurrence,Is the firstComponent lifetime with k multiple coupling relationship failure modes,Is the firstThe life of the individual components;
representing the fault mode with the multi-element coupling relation as a Copula form to obtain the first The reliability of the individual components is:
;
Wherein: Is the first The corresponding first componentThe cumulative distribution function value of each failure mode,Is the firstCorresponding to the componentsAndThe combined distribution function value of the two fault modes; for reliability of failure modes without coupling relationship, In the form of Copula, a joint distribution function of failure modes with k multi-element coupling relations,Mathematical operators, expressed as the product of the reliability of failure modes without coupling relationships.
As a preferable technical scheme, the selection of the Copula function and the establishment of the correlation model of failure among different components of the wind turbine generator set comprise the following steps:
Establishing a first Copula function, a second Copula function and a third Copula function;
analyzing the multi-fault failure model of each component of the wind turbine by using the first Copula function, the second Copula function and the third Copula function to establish a correlation model of failure among different components of the wind turbine;
the distribution function expression and the probability density expression of the first Copula function are respectively:
;
Wherein: , is a different fault; Is a first parameter; is an Archimedes Copula distribution function; As a function of the probability density of the sample, A distribution function expression that is a first Copula function;
The distribution function expression and the probability density expression of the second Copula function are respectively:
;
Wherein: As a second parameter, the first parameter is, ,;A distribution function expression that is a second Copula function,A probability density expression that is a second Copula function;
the distribution function expression and the probability density expression of the third Copula function are respectively:
;
Wherein: as a third parameter, the first and second parameters, ;For the third Copula function distribution function expression,A probability density expression for a third Copula function;
The correlation model of failure among different components of the wind turbine generator comprises one of a series model, a parallel model and a voting model and a combination thereof;
in the series model, any one component failure can lead to an overall system failure;
in the parallel model, in the case where all components constituting the system are failed, the system is failed;
In the voting model, the system works normally under the condition that at least r components in n components forming the system have no faults, wherein r is more than or equal to 1 and less than or equal to n.
As a preferred technical solution, parameter estimation is performed on degradation and Copula functions based on a maximum likelihood method and a monte carlo method, including:
Constructing a maximum likelihood degradation model, wherein the maximum likelihood degradation model is used for carrying out parameter estimation on degradation quantity, and the maximum likelihood degradation model is expressed as:
;
Wherein: as a function of the maximum likelihood degradation, Is the firstThe dimensional parameters of the degradation of the individual components,Is the degradation process of the ith component, n is the number of components,In order to measure the number of times,Is the firstIn the degradation process ofFirst of all failureThe amount of degradation of the secondary measurement is,Is the firstThe total number of measurements of the individual faults,Is a distribution function of a standard normal variable,The time taken for the W-th measurement for the h-th fault,The variance of the time taken for the W-th measurement for the h-th fault of the i-th component,The expectation of the time taken for the W-th measurement of the h-th fault of the i-th component;
Parameter estimation is carried out on the Copula function based on the Monte Carlo method and the semi-parameter estimation method:
Solving parameter values by using a semi-parameter estimation method, and performing nuclear density distribution function Instead of an edge distribution function:
;
Wherein: Is the first A nuclear density distribution function of the individual components; is a semi-parameter estimate.
According to a second aspect of the present invention, there is provided a wind turbine reliability assessment apparatus, the apparatus comprising:
The first model building unit is configured to build a degradation-impact dependent competition failure model of each component of the wind turbine according to a nonlinear wiener process and a Markov principle, wherein the self-healing of the degradation-impact dependent competition failure model is considered;
The second model building unit is configured to build a multi-fault failure model of each component of the wind turbine generator based on the multi-dimensional Copula function;
the third model building unit is configured to select a Copula function and build a correlation model of failure among different components of the wind turbine generator;
And a parameter estimation unit configured to perform parameter estimation on the degradation amount and the Copula function based on the maximum likelihood method and the monte carlo method.
According to a third aspect of the present invention there is provided a readable storage medium storing one or more programs executable by one or more processors to implement the method as described above.
The invention has at least the following beneficial effects:
The method can better simulate the degradation process caused by multiple factors such as wind turbine generator environment and the like by adopting the nonlinear wiener method, and has the advantage of solving the random problem by using the Markov principle. In addition, each component of the wind turbine generator can adopt a self-protection mechanism when impacted, damage caused by the impact is self-recovered, and the reliability of the wind turbine generator can be accurately estimated by building a self-healing model. Secondly, the Archimedes Copula function family has good applicability in solving nonlinear relations, has simple structure and can accurately describe the correlation between fault modes and components. Finally, the Monte Carlo method and the semi-parameter estimation method have data simulation and iteration processes, so that the speed of estimating the unknown parameters can be further improved.
Drawings
FIG. 1 shows a flowchart of a wind turbine reliability assessment method according to an embodiment of the invention;
fig. 2 shows a block diagram of a wind turbine reliability evaluation device according to an embodiment of the present invention.
Detailed Description
The present invention will be described in detail below with reference to the drawings and detailed description to enable those skilled in the art to better understand the technical scheme of the present invention. Embodiments of the present invention will be described in further detail below with reference to the drawings and specific examples, but not by way of limitation. The order in which the steps are described herein by way of example should not be construed as limiting if there is no necessity for a relationship between each other, and it should be understood by those skilled in the art that the steps may be sequentially modified without disrupting the logic of each other so that the overall process is not realized.
The embodiment of the invention provides a reliability evaluation method of a wind turbine, as shown in fig. 1, which is a flow chart of the method, and comprises the following steps:
and step1, establishing a degradation-impact dependent competition failure model of each component of the wind turbine according to the nonlinear wiener process and the Markov principle, wherein the self-healing of the degradation-impact dependent competition failure model is considered.
In this embodiment, the degradation-impact dependent competition failure model of each component of the wind turbine considering self-healing includes a natural degradation model of the wind turbine, a random impact process model and a self-healing model of each component of the wind turbine.
In some embodiments, step 1 is specifically implemented by:
and 11, building a natural degradation model of the wind turbine according to the nonlinear wiener process.
Currently, most competition failure studies use a linear regression model X (t) =a+bt to describe the degradation process of the system. But linear regression models do not characterize the fluctuations and nonlinearities that exist during the degradation of the system. The present embodiment models the degradation process using a nonlinear Wiener (Wiener) process to more accurately describe the degradation behavior of the system.
The degradation model N 0 based on the nonlinear Wiener (Wiener) process is:
;
Wherein: Representative of Degradation amount of time degradation process; as a drift coefficient, representing the degradation rate; As a non-decreasing time scale function, representing a nonlinear characteristic of the degradation process, Represents the amount of dimensional change per unit time,As a function of the drift,As a parameter of the time scale of the time,Is the diffusion coefficient; is a standard brownian motion.
When the degradation amountWhen the threshold k for the degradation failure exceeds a predetermined threshold for the first time, the failure is determined, and the time t at this time is referred to as the first-pass time, the life of the system when the degradation failure occurs can be regarded as the life of the system. For the degradation model N 0, converting the closed expression of the probability density function of the nonlinear degradation failure model into the first-pass distribution probability problem that the standard Brownian motion exceeds the time-varying threshold value, and obtaining the approximate analytical expression of the natural degradation failure as follows:
;
Wherein: representing a natural degradation failure function, A time-varying threshold function is represented,Representing a given critical degradation failure threshold value,An exponential function based on e is represented.
ThenThe cumulative distribution function approximation calculation formula of the distribution at the time of first pass is as follows:
;
Wherein: Representation of A cumulative distribution function of the distribution at the first pass threshold,The probability function is represented as a function of the probability,Indicating the moment at which the threshold value is reached,Is a composite function, representing a natural degenerate failure function,Representing a cumulative distribution function.
And 12, establishing a random impact process model based on a Markov principle.
Due to the influence of factors such as material properties, working characteristics and the like, the impact effect of the performance parameters has a recoverable phenomenon, namely, for a certain performance parameter, the value of the performance parameter is recovered to a natural degradation process after impact change occurs.
For the firstPerformance parameters, assuming Markov chains satisfying the 0-1 state for impact generation and natural degradation, are usedA representation state, expressed as:
;
The state transition matrix of the Markov chain is utilized to describe the state transition process of the performance parameters, and then the probability of the mutual transition between different states is displayed. If the current state is that the impact occurs, the probability that the impact still occurs at the next moment is kept as The probability of returning to natural degradation isAnd (2) andIf the current state is natural degradation, the probability of natural degradation is thatThe probability of impact occurrence isAnd (2) andExpressed as:
;
comprehensively consider natural degradation and impact effect, and finally, the first Degradation of performance parametersExpressed as:
;
Wherein: To represent the degradation amount of the natural degradation process of the p-th performance parameter at time t, Is the additional degradation amount caused by impact at the t moment, the impact degradation amount,Subject to independent and identical expectationsVariance isIs a normal distribution of (c).
And 13, building a self-healing model of each component of the wind turbine according to the natural degradation model and the random impact process model of the wind turbine.
When the system is subjected to the firstSelf-healing occurs after secondary impact, and the actual damage amount after self-healing of the system at the moment t is determined by the following formula:
;
Wherein: Is the first Duration of the secondary impact; is a self-healing influence function; Is the first The amount of degradation of the secondary impact;
determining the accumulated damage amount of the system at the moment t by the following formula :
;
Wherein: Is the first Duration of the secondary impact; Is the first The amount of degradation of the secondary impact is,Is the number of times of arrival of the impact.
Due to the non-monotonicity of the system degradation process with self-healing mechanism, it cannot be given directlyIs a function of the distribution of (a). For a dependent competition failure system with a self-healing mechanism, the system is not failed, and the size of each impact is ensured to be smaller than a failure threshold valueWhile the total degradation of the system is less than。
And 2, building a multi-fault failure model of each component of the wind turbine based on the multi-dimensional Copula function.
N-dimensional Copula function with simple structure and accurate description of the correlation between components and failure mode, and with the definition domain of 0,1, zero reference plane with N-dimensional increment, and arbitrary variableSatisfies the edge distribution。
By the multidimensional Sklar theorem, we assume that the joint distribution function of the multidimensional random variable isThe edge distribution function isThere is a Copula functionThe relation is satisfied:
;
Wherein: In order to combine the functions of the distribution, As a function of the distribution of the edges,For the nth component degradation of the wind turbine generator, if the edge distribution function is continuous, the Copula functionIs a deterministic function, if the edge distribution function is a unitary distribution, F (, ⋯,) is a joint distribution function with an edge distribution F 1(⋅) , F2(⋅) ,⋯, Fn ()
And (3) assuming h (h is more than or equal to 2) fault modes exist in an ith component in the wind turbine generator, and a multi-element coupling relation exists between the fault modes. For failure modeRepresenting that k failure modes with multiple coupling relations exist, h-k failures with independent relations exist, andAnd (3) representing. Set the firstFailure mode of individual components. The corresponding joint distribution function can be expressed as:
;
Wherein: For the actual life of the component of the ith failure mode having multiple coupling relationships, For a component lifetime joint distribution function with a multiple coupling relationship,Component life for failure modes with multiple coupling relationships is less than nominal life,Component rated life for failure mode with multiple coupling relationships;
Establishing a k-dimensional Copula function Expressed as
;
Wherein: For all component rated life joint distribution functions with k multiple coupling relationship failure modes, For the ith component life distribution function with k multiple coupling relationship failure modes,In the form of a complex function whose value is equal to;
At the initial time, the assembly has no fault state, the firstThe reliability of the individual components is:
;
Wherein, Is the firstThe degree of reliability of the individual components,As a function of the probability of occurrence,Is the firstComponent lifetime with k multiple coupling relationship failure modes,Is the firstThe life of the individual components;
According to the incoordination property and the multidimensional Sklar theorem, the fault mode with the multi-element coupling relation is expressed as a Copula form to obtain the first The reliability of the individual components is:
;
Wherein: Is the first The corresponding first componentThe cumulative distribution function value of each failure mode,Is the firstCorresponding to the componentsAndThe combined distribution function value of the two fault modes; for reliability of failure modes without coupling relationship, In the form of Copula, a joint distribution function of failure modes with k multi-element coupling relations,Mathematical operators, expressed as the product of the reliability of failure modes without coupling relationships.
And 3, selecting a Copula function and establishing a failure correlation model among different components of the wind turbine generator.
By using different Copula functions, different dependency structures can be described, thus more accurately characterizing the joint distribution of multidimensional random variables. Compared with an elliptic Copula function, the Archimedes Copula function has the advantage that the Archimedes Copula function is not limited by radial symmetry, and can accurately capture the dependency relationship of different upper tails and lower tails.
The archimedes Copula distribution function expression is:
;
Wherein: 、 And Respectively represent Gumbel Copula function, clayton Copula function and FrankCopula function, a, beta andRespectively, are the parameters corresponding to each other,、A kind of electronic deviceIs a weighting coefficient, and。
Deriving the above equation to obtain a probability density function of the Copula function:
;
Wherein: respectively is Is a derivative of the (c).
In this embodiment, three Copula functions, namely, a first Copula function, a second Copula function and a third Copula function, are set, and specifically described as follows:
(1) The first Copula function is a binary Gumbel Copula function, and the distribution function expression and the probability density expression are respectively:
;
Wherein: , is a different fault; Is a first parameter; is an Archimedes Copula distribution function; As a function of the probability density of the sample, Is a distribution function expression of the first Copula function.
(2) The second Copula function is a binary Clayton Copula function, and the distribution function expression and the probability density expression are respectively:
;
Wherein: As a second parameter, the first parameter is, ,;A distribution function expression that is a second Copula function,A probability density expression that is a second Copula function;
(3) The third Copula function is a binary Frank Copula function, and the distribution function expression and the probability density expression are respectively:
;
Wherein: as a third parameter, the first and second parameters, ;For the third Copula function distribution function expression,A probability density expression for a third Copula function;
and (3) analyzing the model constructed in the step (2) based on the Copula function to establish a correlation model. Typical reliability models between different components are mainly a series model, a parallel model and a voting model:
In the series model, if any component fails, the whole system will fail, and the system is assumed to be composed of i components, and the components are independent of each other, i.e. if one component fails, the reliability of other components will not be affected. The system reliability expression is that
;
Wherein: for system reliability, n is the number of components.
When all components forming the system fail, the parallel system fails, and if i independent components are connected in parallel, the system reliability expression is as follows
;
Wherein: for system reliability, n is the number of components.
In the voting model, at least r (r is more than or equal to 1 and less than or equal to n) components in n components forming the system have no faults, and the system can work normally. The system reliability expression is that
;
Wherein: for system reliability, n is the number of components.
And 4, carrying out parameter estimation on the degradation amount and the Copula function based on a maximum likelihood method and a Monte Carlo method.
In one embodiment, the step 4 is specifically implemented by the following steps:
step 41, estimating parameters (degradation amount) by using the maximum likelihood degradation model.
The maximum likelihood degradation model is expressed as:
;
Wherein: as a function of the maximum likelihood degradation, Is the firstThe dimensional parameters of the degradation of the individual components,Is the degradation process of the ith component, n is the number of components,In order to measure the number of times,Is the firstIn the degradation process ofFirst of all failureThe amount of degradation of the secondary measurement is,Is the firstThe total number of measurements of the individual faults,Is a distribution function of a standard normal variable,The time taken for the W-th measurement for the h-th fault,The variance of the time taken for the W-th measurement for the h-th fault of the i-th component,The expectation of the time taken for the W-th measurement of the h-th fault of the i-th component;
step 42, estimating Copula function parameters based on the Monte Carlo method and the semi-parameter estimation method.
Because the sample likelihood function involves multidimensional integral differentiation and the integral function itself is complex, the Markov Chain Monte Carlo (MCMC) method has a data simulation and iteration process, and therefore, the MCMC method is adopted to estimate unknown parameters. Solving parameter values by using a semi-parameter estimation method, and performing nuclear density distribution functionInstead of an edge distribution function:
;
Wherein: Is the first A nuclear density distribution function of the individual components; is a semi-parameter estimate.
In conclusion, the reliability curve of each component and system of the wind turbine can be obtained according to the above, and further the reliability of the wind turbine is evaluated.
The embodiment of the invention also provides a reliability evaluation device of the wind turbine, as shown in fig. 2, the device comprises:
A first model building unit 401 configured to build a self-healing considered degradation-impact dependent competition failure model of each component of the wind turbine according to a nonlinear wiener process and a markov principle;
a second model building unit 402, configured to build a multi-failure model of each component of the wind turbine based on a multi-dimensional Copula function;
the third model building unit 403 is configured to select a Copula function and build a correlation model of failure among different components of the wind turbine generator;
a parameter estimation unit 404 configured to perform parameter estimation on the degradation amount and the Copula function based on the maximum likelihood method and the monte carlo method.
It should be noted that the structures of the devices described in this embodiment and the methods described in the foregoing are the same technical concept, and achieve the same technical effects by the same principles, which are not repeated here.
Embodiments of the present invention also provide a readable storage medium storing one or more programs executable by one or more processors to implement the method of any of the embodiments above.
Furthermore, although exemplary embodiments have been described herein, the scope thereof includes any and all embodiments having equivalent elements, modifications, omissions, combinations (e.g., of the various embodiments across), adaptations or alterations as pertains to the present application. The elements in the claims are to be construed broadly based on the language employed in the claims and are not limited to examples described in the present specification or during the practice of the application, which examples are to be construed as non-exclusive. It is intended, therefore, that the specification and examples be considered as exemplary only, with a true scope and spirit being indicated by the following claims and their full scope of equivalents.
The above description is intended to be illustrative and not restrictive. For example, the above-described examples (or one or more aspects thereof) may be used in combination with each other. For example, other embodiments may be used by those of ordinary skill in the art upon reading the above description. In addition, in the above detailed description, various features may be grouped together to streamline the invention. This is not to be interpreted as an intention that the features of the claimed invention are essential to any of the claims. Rather, inventive subject matter may lie in less than all features of a particular inventive embodiment. Thus, the following claims are hereby incorporated into the detailed description as examples or embodiments, with each claim standing on its own as a separate embodiment, and it is contemplated that these embodiments may be combined with one another in various combinations or permutations. The scope of the invention should be determined with reference to the appended claims, along with the full scope of equivalents to which such claims are entitled.
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