This invention relates generally to monitoring and diagnosing conditions within a processing system. More specifically, the invention is directed to a system and method for gathering diagnostic information based on specially constructed modules or seeds that travel through a flow path of the coal gasification system.
Broadly, gasification is the creation of combustible gas known as synthesis gas and commonly referred to as “syngas” herein, from carbon-containing fuels. Gasification is a well-known industrial process used for converting solid, liquid and gaseous feedstocks using reactants such as air, oxygen, and steam into gases such as hydrogen, carbon monoxide, carbon dioxide, and methane. The resulting gases can be used for generating electrical power, producing heat and steam, or as a feedstock for the production of various chemicals and liquid fuels, or any combination of the above.
In the gasification of a hydrocarbon fuel such as coal or coke, for example, the fuel, in particulated form, is fed into the gasifier reaction chamber together with an oxidizing gas. Reaction of the particulated fuel with the oxidizing gas results in the production of a raw synthesis gas which is carried from the gasifier for further treatment. The events within the reaction chamber produce not only a usable gas, but also a slag having a constituency which depends to a large degree on the fuel being burned and the operating. Because the gasifier for this purpose must be operated at a relatively high temperature and pressure which is well known in the industry, conditions within the combustion chamber must be monitored at all times. Of particular importance, during the initial start-up period when the fuel and oxidant mixture is injected into the reaction chamber, it is essential that the reaction ignition event takes place immediately. Any substantial delay could permit the accumulation of unsafe quantities of fuel and gas to the point where there is the danger of having an uncontrolled explosion within the reaction chamber as well as within other process equipment downstream of the gasifier. It is desirable, therefore, as a safety measure, to monitor the temperature within the gasifier not only during periods of normal operation, but also during the initial startup stage.
Normally, gasifiers are equipped with one or more temperature monitoring devices. One such device is the thermocouple, a plurality of which may be disposed throughout the refractory lined walls of the gasifier reaction chamber. The thermocouples are placed in the gasifier in such a way that they are separated by a thin layer of refractory from the flames in the reaction chamber. This is done to protect the relatively fragile thermocouple junctions from the very aggressive environment inside the reaction chamber. Consequently, the thermocouples do not sense the reaction temperature directly, but instead respond to the heat transmitted through the thin refractory layer from the reaction chamber. It can be appreciated that, as a result of the lag-time inherent in conductive heat transfer, there can be a considerable delay in thermocouple response to critical changes. This is especially true during gasifier startup when reaction initiation results in a rapid temperature rise which must be detected in order to confirm that the reactions have initiated and that unsafe levels of unreacted material are not accumulating within the gasifier and other downstream equipment. In addition, heat transfer lag-times effect thermocouple response to operating condition changes during normal gasifier operation. Thermocouples have also been used as single-point measurement devices within the radiant syngas cooler (RSC).
As an alternative to thermocouples, pyrometers are sometimes used to measure reaction temperature. Physically, the pyrometer is mounted external to the reactor and views the reaction chamber through a gas purged sight tube which normally extends from the pyrometer to the reaction chamber.
A major weakness of the pyrometer temperature monitor arises from the difficulty encountered in keeping the sight tube free of obstructions. The potential for obstruction is great, resulting from the atmosphere within the reaction chamber which is characterized by rapid swirling of particulate carrying gas. Further, a slag which results from ungasifiable material within the fuel, will likewise swirl around the reaction chamber, contacting the walls of the latter. In the course of gravitating towards the lower end of the gasifier, slag normally displays a tendency to cling to the reaction chamber walls. The clinging slag and the swirling particles interfere with the operation of the pyrometer sight tubes which are positioned in the reaction chamber walls. In addition, during the gasifier startup sequence, fuel is introduced into the reactor before oxidant. Depending upon the circumstances and upon the fuel, coal-water slurry for example, there exists an increased tendency for obstruction of the pyrometer sight tubes with unreacted fuel.
These obstructions prevent verification of startup by the pyrometer's response to reactor temperature change. While the problem of obstruction of the pyrometer sight path can in many instances be dealt with by proper adjustment of the sight tube purge gas, there are some difficulties inherent in the use of purge gas itself. If recycled process gas is used, the gas must first be cleaned so that it is entirely free of moisture and particulates, and then compressed for re-injection through the sight tube into the reaction chamber. This may require additional equipment (e.g. oil-free compressor, gas cleaning equipment, etc.) which adds to operations and maintenance expense.
Alternately, if a non-process gas (e.g. an inert gas such as nitrogen) is used as the purge gas, the product from the reaction chamber will be slightly diluted by the pyrometer purge gas. If the gasifier is producing a synthesis gas for a chemical process, the presence of a diluent gas may not be acceptable.
Much simulation has been performed in order to optimize these components, such as the feed injector, the gasifier and the radiant syngas cooler (RSC), and the behavior and thermal profile of the flame proceeding from the injector. However, there has been limited experimental validation of these simulations primary due to the inability of conventional sensors and probes to function or even survive the system's internal atmosphere. In view of the foregoing, the invention overcomes the problems encountered with both thermocouples and optical pyrometers to monitor the actual variables of interest within the gasification flow path.
One embodiment of the invention is directed to a coal gasification system that comprises a gasifier; a radiant syngas cooler (RSC) for receiving gasification products from the gasifier; and a seed introduced into a gas stream of the coal gasification system, wherein the seed gathers diagnostic information relating to an operating condition of the gas stream while traveling through the coal gasification system.
Another embodiment of the invention is directed to a seed for gathering diagnostic information relating to an operating condition while traveling through a gas stream of a coal gasification system, the seed comprising a core and at least one concentric shell surrounding the core.
Another embodiment of the invention is directed to a seed for gathering diagnostic information relating to an operating condition while traveling through a gas stream of a coal gasification system, the seed comprising a first resonant circuit for emitting a resonant frequency depending on a temperature of the first resonant circuit.
A method of gathering diagnostic information in a coal gasification system comprises the step of introducing a seed into a gas stream of the coal gasification system, whereby the seed gathers diagnostic information relating to an operating condition while traveling through the gas stream of the coal gasification system.
As used herein, a “seed” is defined as a specially constructed module that is introduced into the gas stream or processing path of the coal gasification system in order to help diagnose operating conditions within the coal gasification system. By way of example and not limitation, these operating conditions include average mass flow rates as a function of location within the system, temperature profiles, flame thermometry, and chemical analysis of the mass flow. The external geometry of a seed may be varied. Spheres or prolate spheroids might accommodate most aerodynamic requirements but a seed may be designed to exhibit scenario-desirable aerodynamic interactions that are, for purpose of example and not limitation, enabled by equipping the main body of a seed with a specially designed aerodynamic appendage, such as a propeller and the like. One embodiment of such a propeller is shaped similar to the maple tree seed propeller. The equipage of such an aerodynamic appendage moderates the speed with which the seed may move within the gas path. Such an appendage may be fabricated out of a shape memory alloy and deploy when the seed temperature reaches the critical point for the shape memory alloy structure to resume its preset shape. A further embodiment of the seed 200 is the addition of a coating of graphite on the seed's surface. The graphite coating serves to prolong the useful life of the seed within the hot gas path environment.
A seed gathers diagnostic information as it traverses the processing path and it transfers this information in one of two modalities. The first modality is on physical recovery of the seed after it has passed through the system or a portion thereof. The second modality is non-physical recovery of the seed and the information transfer takes place while the seed is in transit within the gasification system or has completed its transit of the system or during both of these opportunities. The seed's mechanism for gathering diagnostic information may be chemical-based, electronic-based, or a combination thereof.
One embodiment of a physically recovered seed that is useful for studying temperature profiles is the seed 100 illustrated in
Another embodiment of a physically recovered seed that is useful for studying composition profiles is also described by the seed 100 illustrated in
Another embodiment of a physically recovered seed that is useful for studying temperature profiles is the seed 140 illustrated in
To aid in the recovery of a seed, another embodiment includes a layer that fluoresces, is magnetic or a combination of both. This could be achieved by suitable section of materials. The seeds could be removed manually under suitable light conditions, or automatically under the influence of a magnetic field.
It will be appreciated that the physically recoverable seed of the invention is not limited to a seed having a spherical shape, and that the invention can be practiced with a seed having any desirable shape. For example, the core may be irregular in shape with an outer layer having varying thickness. In addition, the seed may have a graded index material having a density or other material property that changes with thickness.
An embodiment of a non-physically recoverable seed that is useful for studying the internal gas flows and temperature profiles within the gasification system is to construct the seed 100 or the seed 140 in such a manner as to modify its terminal velocity within the gas path. This can be done by adjusting the sphere's radius, R, and weight W. In the case of a free-falling object with no drag, the terminal velocity is unbounded and the time, tL, that the object will take to fall a distance s, starting from rest, is tL=√{square root over (2s/g)} where g is the acceleration due to gravity. If there is drag, then the time for the object to fall a distance s, starting from rest, is upper bounded by tU=s/νt, where νt is the terminal velocity. The terminal velocity of a sphere, discounting wall effects, is νt=√{square root over ((2W)/(CdρA))}{square root over ((2W)/(CdρA))}, where Cd is the drag coefficient, ρ is the gas density, and A is the frontal area of the sphere, ie, A=πR2. The drag coefficient of a sphere lies in the range 0.07 to 0.50, depending upon the Reynolds number respecting laminar or turbulent flow conditions. Thus, the time the seed spends falling within the gas path can be altered by constructing the seed with a different weight or radius.
An embodiment of a non-physically recoverable seed that is useful for studying temperature within the gasification system processing path is illustrated in
A variation on the embodiment illustrated in
A further variation on the embodiment illustrated in
An embodiment of a non-physically recoverable seed and the associated system elements that are useful for studying the mass flow pattern within the gasification path within the RSC 40 is illustrated in
In another embodiment, a non-physically recoverable seed with the active emitters attached to the injector surface can monitor the flow of seeds that are introduced directly into the gasifier 15, rather than into the RSC 20. In this embodiment, the seeds would need to be of reasonable size to be detected with a surface material constructed of a very high temperature material, such as a ceramic, alumina, zirconia, and the like. Likewise, the resonant electronic circuits are constructed with an appropriate high temperature metal, such as the type used in thermocouples, such as Pt, Pt/Rh, and the like.
It will appreciated that the non-physically recoverable seed on the invention is not limited to having a resonance circuit with a circuit element that changes material property, such as changes in dielectric or a circuit switching (fusible links) system. Rather, the invention can be practiced with a resonant circuit based upon physical deformation, for example, the expansion of a RF resonant cavity as a function of temperature. In another example, the resonance circuit may be a mechanically tuned high temperature material for operating in harsh environments.
Although this invention has been described by way of specific embodiments and examples, it should be understood that various modifications, adaptations, and alternatives may occur to one skilled in the art, without departing from the spirit and scope of the claimed inventive concept. All of the patents, articles, and texts mentioned above are incorporated herein by reference.
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Number | Date | Country | |
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20090031787 A1 | Feb 2009 | US |