Patent Application
20250164110
The present invention relates to a method for controlling a thermal combustion system and to a control logic for a thermal combustion system.
Combustion can be described as the rapid oxidation of combustible, such as fuel, resulting in the release of usable heat and production of a visible flame. Combustion is still a difficult subject, being truly interdisciplinary and requiring the merging of knowledge and skills in several fields. It involves the study of chemistry, kinetics, thermodynamics, electromagnetic radiation, aerodynamics and fluid mechanics, including multiphase flow and turbulence, heat and mass transfer, and quantum mechanics to name a few.
Oil refining, chemical processes, and power generation are energy-intensive industries with combustion applications in burners, process heaters, boilers, and cogeneration system, as well as flares and thermal oxidizers. Combustion for these industries presents unique challenges related to the variety of fuel compositions encountered. Combustion equipment must be flexible to be able to operate in a safe, reliable, efficient, and environmentally responsible manner under a wide array of fuel compositions and conditions. Demands placed on combustion systems change continuously with time and are becoming more stringent. The safety of combustion systems has always been essential, but emphasis of effective heat transfer, temperature uniformity, equipment scale-up, efficiency, controls, and—more recently—environmental emissions and combustion-generated noise has evolved over time. Such demands create tremendous challenges for combustion engineers.
A combustion system typically includes a fuel supply, a combustion air supply, and an ignition system that all come together at one or more burners. Typically, these components are operated by means of a control system. Specifically, the purpose of the control system is to start, operate and shut down the combustion process and any related auxiliary processes safely, reliably, and efficiently. The control system consists of various physical and logical components chosen and assembled according to a control philosophy and arranged to provide the user with an informative, consistent, and easy-to-use interface. During system start-up and at various times during normal operation, it is necessary to verify or change the status of these systems. During system operation, the control system needs various items of process information to optimize system efficiency. Additionally, the control system monitors all safety parameters at any time and will shut down the combustion system, if any of the safety limits are not satisfied.
For this purpose, a combustion control system has temperature controllers and air-fuel ratio as well as oxygen controllers in thermal oxidizers—although oxygen controllers are in general required, they can be considered necessary regarding efficiency optimization. Further, some combustion control systems also apply a feed forward principle as known from the automation industry. A typical control logic for thermal oxidizer using multiple sources for fuels and oxygen is described in “The John Zink Hamworthy Combustion Handbook—Design and Operations Vol. 2”, Charles E. Baukal Jr., editor, CRC Press, Boca Raton, Florida 2013 as follows:
Development of a fully metered control scheme for modulating fuel and air to the burner begins with the electronically linked parallel positioning scheme. Flow meters are linear with flow rate. Meter output signal scaling provides the firing rate and air to fuel ratio required for the application. The combustion air characterizer used for parallel positioning is not required because the transmitters are linear with flow rate. The temperature indicating controller (TIC) output sets the firing rate by serving as setpoint (SP) to each flow controller. Controller output mode, reverse or direct acting, defines the change in output signal direction with respect to process variable (PV) changes. For example, if the controller output increases as the PV increases, the controller mode is direct acting. In combustion control schemes, fail-closed fuel valves require a reverse-acting flow controller, while fail-open combustion air valves require direct-acting flow controllers. It is clear from controller mode definitions that the TIC should be reverse acting. That is, the TIC output should decrease, reducing the firing rate, in response to an increase in temperature, the PV. Addition of high and low signal selectors provides cross limiting of the fully metered control scheme. The low signal selector compares demanded firing rate from the TIC to the actual combustion airflow rate and applies the lower of the two signals as the SP to the fuel flow controller. The low signal selector ensures that the fuel SP cannot exceed the amount of air available for combustion. The high signal selector compares demanded firing rate from the TIC to actual fuel flow rate and applies the higher of the two signals as the SP to the airflow controller. This ensures that the SP is never lower than required for combustion of actual fuel flow rate. Together, the high and low signal selectors ensure that unburned fuel does not occur in the combustion system. Unburned fuel accumulations can cause explosions. Cross limiting by the signal selectors causes airflow to lead fuel flow during load increases and for airflow to lag fuel flow during fuel decreases. This lead/lag action explains why the fully metered cross-limiting control system is often called “lead-lag” control. Whatever the name, the system performs the function of maintaining the desired air/fuel mixture during load changes. The system also provides fuel flow rate reduction in the even airflow is lost or decreased. It is possible to trim the control scheme using measurement of flue gas O2 content. For most systems, the O2 signal should be used to “trim”, and not be a primary control. Many O2 analyzers are high maintenance and/or too slow in response to be sued as a primary control in the combustion process. The O2 controller is utilized for SP injections and provides tuning parameters to help process customization. High and low signal limiters restrict the O2 controller output to a trimming function, normally 5 to 10% of the normal combustion airflow rate. A multiplication function (X) in the combustion airflow transmitter signal makes the O2 trim adjustment. The multiplier gives a fixed trim gain. Substituting a summing function for the multiplier would result in high trim gain at low flow rates and could produce a combustion air deficiency. O2 trim may be applied to the combustion airflow controller SP rather than the flow transmitter signal. If this technique is used, the airflow signal to the low signal selector must retain trim modification. Multiple fuels and O2 sources are accommodated by the cross-limiting scheme, as shown in
However, the typical design of today's combustion control systems does not consider any variations in the flow of the combustibles, e.g., waste gas flow, which are fed to the combustion. In particular, waste gas flows may have variations in their flow. The rapid introduction or sudden loss waste flows into a combustion system of the prior art typically leads to temperature jumps and a likelihood of trips or loss of authorization for waste operation. Further, the last stage of oxidation systems of the prior art must be operated at over-stoichiometric conditions, i.e., an excess of air or oxygen for safe operation. This operation principle inevitably leads to the formation of nitrogen oxides, which reach even higher levels if bound nitrogen is present in the waste flow to the combustion system. However, environmental regulations set strict limits to the emission of nitrogen oxides from oxidation and combustion processes.
Accordingly, there was still a need for a method for controlling a thermal combustion system, which allows to solve the problems mentioned above.
It was found that this problem is solved in that first, the flow of a waste stream from a process underlying a known reaction is measured and when a change of flow is measured, predicting if the flow measured leads to a temperature change in the combustion of the stream of step a). When a temperature change is predicted, the ratio of air to compounds with calorific value and optional inert compounds in the waste stream is calculated, which is required to keep the temperature in the thermal combustion system constant, and the ratio is adjusted accordingly by increasing or decreasing the amount of fuel to be fed into the combustion system, and/or decreasing or increasing the amount of air to be fed into the combustion system.
Further, when the waste stream also comprises bound nitrogen, it is determined if the amount of nitrogen oxides to be formed in the combustion system can be kept at a minimum, when said combustion is performed with the ratio adjusted. When this is not the case, the ratio of air to compounds with calorific value and optional inert compounds in the combustion system is adjusted to a sub-stoichiometric value, which allows to keep the amount of nitrogen oxides to be formed in the combustion system at a minimum, wherein said sub-stoichiometric value is adjusted by an extremum-seeking controller.
An object of the present invention is therefore a method for controlling a thermal combustion system, comprising the steps of
The advantages of the method according to the present invention are:
The method according to the present invention is not subject to any limitations regarding the phase of the waste stream. Rather, the waste stream is any type of fluid, i.e., a gaseous or liquid waste stream.
Further, the method according to the present invention is also not subject to any limitations regarding the composition of the waste stream. Therefore, said waste stream comprises one or more compounds with calorific value. In addition, said waste stream also can comprise an inert compound, i.e., a compound without calorific value, for example carbon dioxide. Preferably, the waste stream comprises a compound with calorific value and an inert compound.
In the context of the present invention the term sub-stoichiometric in connection with an oxidizer such as air, air enriched with oxygen, or oxygen is used as known to the person skilled in the art and denotes that an amount of said oxidizer is involved which is less than the stoichiometric amount of the oxidizer.
According to the method of the present invention, the waste stream comes from a process underlying a known reaction. It is therefore known which compounds with calorific value and optional inert compounds, i.e., compounds without calorific value, are contained in the waste stream. Based on the compounds which are fed to the combustion, the skilled person can set up the balance equation underlying the combustion reaction in question. Resolving said balance equation adequately allows to take the necessary measurements for maintaining the operation value constant.
The composition of the waste stream is essentially constant. Therefore, it is possible to set up a diagram or an equation which gives the temperature of the combustion system as a function of the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and optional inert compounds. As it goes without saying, the inert compounds are not oxidized in the combustion. However, their presence in the waste stream and in the combustion system may have an effect on the temperature in the combustion system because of the heat capacity of the inert compounds. The method according to the present invention makes use of the thus obtained diagram or equation. Any changes in the flow of the waste stream automatically change the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and optional inert compounds. When a change in the flow of the waste stream is measured, one can predict the temperature change resulting from said flow change. Resolving the balance equation for the combustion system (combustion reaction) adequately allows to take the necessary actions for maintaining the operation value constant.
In an embodiment of the method according to the present invention the controller predicts the temperature for the sub-stoichiometric value adjusted in step d2) using a diagram or equation, which allows to determine the temperature of the combustion system and checks if the predicted temperature is within the operating window for the combustion system.
In the context of the present invention the term operating window or operating window for the combustion system is used to denote the temperature range in which the combustion system can be operated. This temperature range has a temperature limit at the lower end of said temperature range and a temperature limit at the upper end of said temperature range, hereinafter also referred to as the maximum temperature. The definite value for the minimum temperature is given by the specific combustion system, i.e., the specific compounds with calorific value and optional inert compounds which are subjected to the combustion and the specific safety and environmental regulations on the combustion on the combustion of the specific compounds. Therefore, the term minimum temperature is hereinafter also used equivalent with the allowed minimum temperature. The definite value for the maximum temperature is given by the mechanical design conditions of the combustion unit.
In a preferred embodiment of the method according to the present invention the operating window has a temperature range with a minimum temperature and a maximum temperature, wherein the minimum temperature is given by the allowed minimum temperature for the combustion of waste streams and the maximum temperature is given by the mechanical design conditions of the combustion unit.
Consequently, the sub-stoichiometric value adjusted in step d2) needs to be checked if the corresponding temperature predicted by the controller is within or outside the operating window for the combustion system. In the first case, the sub-stoichiometric value is approved and in the second case, the sub-stoichiometric value is dismissed.
In a further embodiment of the method according to the present invention the sub-stoichiometric value adjusted in step d2) is approved when the temperature predicted by the controller is within the operating window for the combustion system.
In an alternative embodiment of the method according to the present invention the sub-stoichiometric value adjusted in step d2) is dismissed, when the temperature predicted by the controller is outside the operating window for the combustion system, and the method continues with the value adjusted in step c2).
In principle, the method according to the present invention is not subject to a specific design of the combustion. Therefore, it is not subject to any limitations regarding the number of stages in the combustion. Typically, a combustion unit has one or two stages. Nevertheless, it is preferred that the combustion in the method according to the present invention is a two-stage combustion.
In another embodiment of the method according to the present invention the combustion is a two-stage combustion.
Preferably, the steps a) to d) are performed in the first stage of the combustion. This allows to take the adequate measures based on the conditions, e.g., temperature, in the first combustion stage for the combustion in the second stage to have a combustion outlet which meets the safety, legal and environmental regulations with respect to the composition of the combustion outlet.
In a preferred embodiment of the method according to the present invention steps a) to d) are performed in the first stage in case of a two-stage combustion or in the first and second stage in case of a three-stage combustion.
For safety reasons, it is preferred that the overall ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and optional inert compounds in the stream of step a) is adjusted to a value which ensures an excess of oxygen in the outlet of the combustion unit. Specifically, the excess of air, air enriched with oxygen, or oxygen is sufficient to ensure a complete combustion.
In another embodiment of the method according to the present invention the overall ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and optional inert compounds in the stream of step a) is adjusted to a value which ensures an excess of oxygen in the outlet of the combustion unit.
In a further preferred embodiment of the method according to the present invention the excess of air, air enriched with oxygen, or oxygen is sufficient to ensure a complete combustion.
Situations may occur where the sub-stoichiometric conditions may lead to a temperature in the first stage, either measured or predicted in the first stage, which may reach or even exceed the maximum temperature. This temperature, however, would be out of the operation window of the method according to the present invention. In a situation like this, it is preferred that the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and optional inert compounds in the combustion system is shifted to an over-stoichiometric value.
In another preferred embodiment of the method according to the present invention the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and optional inert compounds in the combustion system is shifted to an over-stoichiometric value when the temperature measured or predicted in the first stage reaches or exceeds the maximum temperature.
In the context of the present invention the term sub-stoichiometric is used as known to the person skilled in the art and denotes that an amount of a reagent is involved which is more than the stoichiometric amount of the reagent.
In detail, the step c2) of the method according to the present invention comprises a temperature measurement in the first stage and in the outlet of the combustion unit, and the thus measured temperatures are set as set point of the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value. Next, the amount of fuel, which is necessary to maintain the temperature in the combustion system constant, is determined. In addition or alternatively, the amount of air, air enriched with oxygen or oxygen relative to compounds with calorific value and optional inert compounds, which is necessary to maintain the temperature in the combustion system constant, is determined.
In an embodiment of the method according to the present invention the step c2) comprises the steps
The technical features of the method according to the present invention can be realized in a control logic for a thermal combustion system.
A further object of the present invention is therefore a control logic for a thermal combustion system, comprising
The control logic according to the present invention is not subject to any limitations regarding the phase of the waste stream. Rather, the waste stream is any type of fluid, i.e., a gaseous or liquid waste stream.
Further, the control logic according to the present invention is also not subject to any limitations regarding the composition of the waste stream. Therefore, said waste stream comprises one or more compounds with calorific value. In addition, said waste stream also can comprise an inert compound, i.e., a compound without calorific value, for example carbon dioxide. Preferably, the waste stream comprises a compound with calorific value and an inert compound.
In an embodiment of the control logic according to the present invention the combustion has two stages, and each of them comprises a flowmeter, a temperature indicating controller, and a feed forward block.
The feed forward block is preferably implemented for each stage of the combustion system. The outlet of each temperature indicating controller (stage1 and outlet) is a set point of the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and inert compounds. For each stage, a feed forward block, which then is also defined as a ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and inert compounds, is added to the outlet of each temperature indicating controller (1). This ensures a quick response of the control logic to disturbances in the waste stream flows.
The feed forward is derived from the adiabatic energy balance of the system, assuming that an immediate combustion of the compounds takes place in the combustion chamber, without consideration of any time delay or heat transfer to the wall, amongst others. The mathematical task underlying the feedforward is to maintain the temperature in the combustion chamber constant when changes in the flow of the waste stream occur. Mathematically, this means that the derivative of the temperature in the combustion chamber over the time should remain equal to zero. With this condition, the adiabatic energy equation can be rewritten for each flow change of a waste stream, which then allows to adjust the fuel flow being necessary to maintain the temperature in the combustion system constant (2).
Another transformation of each of these equations allows the calculation of the variation in the ratio of air, air enriched with oxygen, or oxygen to compounds with calorific value and inert compounds, which is the feed forward term added to the temperature controller outlet.
Alternatively, the results obtained in (2) can be used inside a feed forward block acting directly on the fuel flow rate controller. In that case, the feed forward block is removed from the temperature controller outlet (1) and implemented at the fuel flow rate controller set point.
In another embodiment of the control logic according to the present invention the feedforward block is adapted to perform the steps c2a) to c2c) or c2a), c2b) and c2d) of the method according to the present invention.
In a preferred embodiment of the control logic according to the present invention only the first stage comprises an extremum-seeking controller.
The example herein is performed using a computational model of a process based on the method shown in
Using the above tool, a change in one of the waste flows (Low heating value <5 MJ/kg, so 10 order of magnitude less than natural gas) is simulated as a jump function (from 0 to 15000 Nm3/h within 1 iteration). This large flow rate change would lead theoretically to a high temperature peak which is observed in stage 1 and 2 immediately after the waste gas jump. It must be noted that in a real system, this jump would never occur that fast since the temperature recorded reacts much more slowly than shown by the theoretical calculation. Hence, the first jump can be for this demonstration ignored.
This large peak inevitably initiates the temperature controllers to adjust their output. Without the feedforward (forward switched OFF), this leads few iterations later to a much larger dip in the combustion temperature in stage 1 and 2 than when the feedforward is switched on. The deviation to the temperature set point is reduced by more than 50% with the feedforward switched ON and this large gain demonstrate the advantages of the proposed controller method.
The advantages of the control logic shown in this theoretical simulation have been confirmed in practice since two thermal oxidizers have been retrofitted with the proposed concept and both show that the temperature spikes remain well within the operating rage when large waste flow rate variations (most of the time shut-off of up to 30% of the total combustor volume and heat flow rates) are occurring.
This performance is clearly visible on
Less than 60 min after the loss of waste event, the same waste stream was sent back to the oxidizer at a slightly slower speed that during the waste stream interruption. This time, the temperature in the first stage was barely impacted by the waste stream start-up. This shows that the control logic is responding well independently of the waste stream switch direction to the oxidizer and the relative amount of energy sent to the oxidizer.
| Number | Date | Country | Kind |
|---|---|---|---|
| 22153928.1 | Jan 2022 | EP | regional |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2023/051180 | 1/19/2023 | WO |
