• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    This installation for supplying a combustion chamber with at least one combustible fluid comprises at least one fuel-fuel combustion chamber supply circuit (2) and at least one circuit purge circuit (3). power supply connected to a source of relatively hot purge air and to said supply circuit and having at least two isolation valves (V1, V2) delimiting between them a cavity (C). It comprises ventilation means (5) for injecting into the cavity a flow of ventilation air relatively cold.
    公开号:FR3030629A1
    申请号:FR1463238
    申请日:2014-12-23
    公开日:2016-06-24
    发明作者:Pierre Montagne
    申请人:GE Energy Products France SNC；
    IPC主号:
    专利说明:

    [0001] FIELD OF THE INVENTION The invention relates, in general, to the fuel supply systems for a combustion chamber, in particular for a turbine combustion chamber. gas. As is known, gas turbines conventionally comprise a compressor, one or more combustion chambers and an expansion turbine. The combustion chamber or chambers are supplied with gaseous fuel by means of a feed circuit to be mixed with pressurized hot air leaving the compressor. The fuel supply system advantageously allows the combustion chambers to be fed from several types of fuels, for example natural gas, liquid fuel or synthesis gas or "syngas". The supply circuit must also allow the regulation of power parameters from the fuel source to the combustion chambers.
    [0002] In particular, it involves regulating the pressure, temperature and fuel flow. In order to allow the transport and transfer to the gas turbine of various types of fuels, to regulate pressure, temperature and flow conditions, the fuel system is equipped with a number of valves insulation and flow control and cooling and filtration systems. It is furthermore necessary for the supply circuit to be capable of separating portions of the circuit, for example from cavities, in order to avoid any contact between the hot air and the sources of gaseous fuel in order to avoid self-heating. ignition of the fuel and the creation of explosive mixtures.
    [0003] In particular, a gas turbine can operate with two types of fuels. For example, a first fuel is natural gas and a second fuel is syngas. Each fuel circuit, when not in use, can be purged with hot air typically taken from the compressor outlet of the turbine. In order to isolate each fuel circuit from this hot air, a double-type cavity designated by the term "block and bleed" is generally used. Furthermore, after the use of a fuel circuit, it should be purged beforehand with an inert gas, for example dinitrogen, before the introduction of the hot air sweep, and this, in order to avoid the creation an explosive mixture. For example, if the circuit of the second fuel is cut, so that following a fuel change no fuel flows in the latter, it is then purged the supply circuit of the second fuel with hot air. During this purge phase, a flow of hot air is maintained to the passages in the injectors provided for the second fuel to prevent the occurrence of condensate and limit the risk of gas return from the combustion chamber to the supply circuit. When the valves controlling the supply of fuel or hot air purge are closed, there remains a risk that, in some cases, leakage occurs through the cavities formed by the isolation valves, thus causing a risk of contact between hot air purge, whose temperature can reach 500 ° C, and fuel. The document US 2013/031 8993 provides in this regard to provide the supply circuit and the purge circuit control valves which delimit between them, in the supply circuit and in the purge circuit, cavities and use vents, in particular in the cavity of the purge circuit, so that hot air leaks are evacuated to the outside, thereby avoiding any risk of self-ignition of the fuel.
    [0004] It has also been proposed in US 2013/0 074 945 to provide leak separation using an inert gas, such as nitrogen, to separate cavities containing different gases. A pressure regulating valve makes it possible to test the pressure of the inert gas in the separation cavity, in order to compensate for the fuel pressure variations, and thus to avoid any suppression in the cavity of inert gas which can cause leaks. Reference may also be made to document US 2013/0167 935, which describes an installation for feeding a combustion chamber of a gas turbine equipped with a purge circuit for the combustion chamber and a cavity of the combustion chamber. supply circuit, by means of a flow of inert gas. In the state of the art, the solutions using inert gases to ensure the separation between the fuel and a hot purge air consist in filling a cavity delimited by two isolation valves at a predetermined and adjustable pressure in order to compensate for the variations. fuel pressure and hot air purge.
    [0005] The pressure level of the inert gases is advantageously chosen so as to be greater than the maximum pressure value of the history of the fuel or hot air pressures, which leads to disadvantages related to the high level of inert gas pressure. in the cavity, for example it is necessary to use an expensive compression system. This also results in a high consumption of inert gas caused by leakage through the isolation valve. This also requires being able to control other factors that can affect the level of fuel pressure and hot air purge, such as the ambient temperature and the level of load of the turbine. This technique also imposes requirements for the storage of high pressure inert gas. It should also be noted that the maintenance of the isolation valves of the fuel supply circuit is essential to the operational efficiency of the gas turbine and to the safety of the supply circuit. Thus, a leaking valve is likely to cause stopping of the turbine or to cause a dangerous mixture of fuel with other fluids present in the supply circuit or in the purge circuit, or in the control circuit. To date, the check of the good functioning of the valves is carried out essentially by physical inspection or by tests of pressurization. Such inspections are expensive because they require putting the turbine out of service. Although other control methods allow inline valve testing to be performed, these control methods require the turbine circuit to be modified and bypass or bypass installed in order to continue the continuous supply of the valves. combustion chambers. In view of the foregoing, the invention proposes to overcome the aforementioned drawbacks and, in particular, to provide an installation for supplying a combustion chamber, in particular a gas turbine, making it possible to reduce the gas requirements. inert without requiring to provide checks of the proper operation of the isolation valves at an increased frequency. The invention thus relates to an installation for supplying a combustion chamber with at least one combustible fluid, comprising at least one combustion fluid supplying circuit of the combustion chamber and at least one circuit purging circuit. power supply connected to a relatively hot air source and to said supply circuit and having at least two isolation valves delimiting between them a cavity in said purge circuit. This installation further comprises ventilation means for injecting into the cavity a flow of ventilation air relatively cold. It is thus possible to inject into the cavity a relatively cold air flow, at a temperature below the temperature of the purge air and chosen so as to avoid the self-ignition of the combustible gases possibly in contact with the air. hot air purge. This limits any risk of auto-ignition and the creation of explosive mixtures and without providing to inject into the cavity a flow of inert gas expensive to implement.
    [0006] According to another characteristic of the installation according to the invention, the ventilation means comprise means of connection to a source of instrumentation gas, for example air, at high pressure associated with a flow control valve. instrumentation gas.
    [0007] For example, the ventilation means comprise connection means to a compressor, for example the main compressor of the gas turbine, and expansion and cooling means for injecting into the cavity a cooled flow of purge air from the compressor.
    [0008] In one embodiment, the ventilation means comprise a calibrated passage for adjusting the flow of ventilation air injected into the cavity. According to another characteristic of the supply installation, the cavity is provided with a ventilation air evacuation vent which opens out of the installation. Moreover, the ventilation means comprise, in one embodiment, ambient air sampling means associated with a filter and a control valve of the ambient air flow and with a device able to maintain a flow of air. forced ambient air in the cavity.
    [0009] In a particular embodiment, the cavity is provided with two vents placed respectively on the side of the isolation valves and opening outwardly of the installation. In this case, the ventilation means may comprise a profiled member for separating the flow of ventilation air into two ventilation rates respectively led to the two vents. It will further be possible to provide, in the cavity, a third isolation valve separating the cavity into two secondary cavities in which the two ventilation flows are respectively injected.
    [0010] The subject of the invention is also, according to a second aspect, a method of supplying a combustion chamber with at least one combustible fluid, for the implementation of a feed installation comprising at least one circuit of supplying the combustion chamber with combustible fluid and at least one purge circuit of the supply circuits connected to a source of relatively hot air and with said supply circuit and having at least two isolation valves delimiting between them a cavity in said purge circuit, into which is injected into the cavity a flow of ventilation air relatively cold. Other objects, features and advantages of the invention will become apparent on reading the following description, given solely by way of nonlimiting example, and with reference to the appended drawings, in which: FIG. 1 illustrates a first example of realization of a fuel chamber supply installation according to the invention; FIG. 2 is a table showing the opening and closing phases of the control valves of the installation of FIG. 1; FIG. 3 shows a second embodiment of an installation according to the invention; FIG. 4 shows a variant of the installation of FIG. 3; FIG. 5 shows a third exemplary embodiment of the feed installation of a combustion chamber according to the invention; FIG. 6 illustrates a fourth embodiment of an installation according to the invention; FIG. 7 illustrates a fifth embodiment of a power supply installation according to the invention; and FIGS. 8 and 9 show variant embodiments of FIG. 7.
    [0011] Referring firstly to Figure 1 which schematically illustrates a first embodiment of a fuel supply system of a combustion chamber according to the invention. In the exemplary embodiment envisaged in the context of the present description, the installation is intended for feeding a combustion chamber of a gas turbine. It is more particularly to avoid any contact between a hot purge air from the compressor of the turbine and a fuel delivered to the injectors I of the combustion chamber of the gas turbine. As seen in FIG. 1, the supply installation comprises a supply circuit 2 connected to a source of fuel, for example a fuel, such as natural gas, liquid fuel or synthesis gas or " syngaz "to supply the injectors I with fuel. However, it will be considered in the remainder of the description that the fuel is gaseous. The supply circuit 2 here comprises a power supply line connected to a corresponding power source (not shown). Of course, it is not beyond the scope of the invention when the supply circuit comprises several supply lines connected to various types of fuel sources. The installation further comprises a purge circuit 3 which is connected to a source of hot air purge here constituted by the compressor of the gas turbine. This purge circuit is intended to continuously scan with hot air coming from the compressor the supply circuit and the injectors in order to purge the circuit, to avoid the appearance of condensate and to avoid the return of gases. from the combustion chamber to the supply circuit 2. It is also seen that the supply circuit 1 is provided with a second circuit 4 for purging the supply circuit, before the purge circuit is implemented. 3 with hot air and thus avoid any contact between the fuel and the hot air coming from the compressor.
    [0012] As can be seen, the supply circuit 2, the hot air purge circuit 3 and the nitrogen purge circuit 4 are each provided with a set of valves, such as V1, V2, V3 and V4 controlled by a remote control unit ensuring the implementation of supply and purge phases. More particularly, it is seen that the purge circuit 3 is provided with two isolation valves V1 and V2 which are provided to prevent contact between the hot purge air and the fuel, during normal operation of the installation.
    [0013] The valves V1 and V2 delimit between them a cavity C, that is to say an insulating circuit portion or the purge hot air supply lines and the fuel supply line or lines. As indicated above, due in particular to the sizing of the valves in a gas turbine feed system, it has been found that there may still be potential gas leaks in the isolation valves, and in particular in the valves V1 and V2. In order to avoid any risk of bringing the hot purge air into contact with the fuel in the cavity C, the installation is provided with ventilation means 5 which maintain a relatively cold air flow in the cavity. that is, at a temperature lower than that of the hot purge air so that the gaseous mixture in the cavity C is lower than the self-ignition temperature of the fuel. In different embodiments, it may for example be air taken from outside at room temperature or instrumentation air, that is to say taken from a control compressed air circuit. turbine equipment, especially at an ambient temperature and a pressure of the order of 6 to 8 bar, or the hot air from the compressor outlet of the gas turbine, cooled and expanded or removed at a lower stage of the compressor of the gas turbine judiciously chosen according to the pressure and the temperature. In the exemplary embodiment illustrated in FIG. 1, the ventilation of the cavity C takes place either from the hot air coming from the cooled and cooled compressor or from the instrumentation air of the installation. , that is to say the pressurized air circulating in the control circuits of the installation. Although in the example shown the ventilation means comprise two circuit branches 6 and 7 respectively recovering the instrumentation air and the other the hot purge air and which converge upstream of the cavity C, it will be noted that it is not beyond the scope of the invention when the ventilation means comprise only one of these branches supplying the cavity C is cooled and expanded purge hot air or air from an intermediate stage of turbine compressor (not shown) via a supply line 11 equipped with a valve V11, or air instrumentation. As can be seen, the first branch 6 comprises a single supply line in which the instrumentation air circulates. This supply line 6 is equipped with a V5 valve for controlling the air flow. As regards the other supply line 7, it is connected to the purge circuit 3, upstream of the control valve V1 and to the instrumentation air supply line 6, upstream of the connection area of the ventilation means to the cavity C. The supply line 7 is provided with a pressure reducing device 8 ensuring the expansion and cooling of the hot air coming from the compressor and a valve V6 flow control purge air cooled and cooled. Thus, during the operation of the installation, the cavity C is supplied with ventilation air which may be mixed with the hot air leakage through the isolation valve V1, and this air at the temperature of the mixture may be at its temperature. tower mixed with a gas leak through the valve V2 and finally rejected to the outside through a vent L with a valve V7. Thus, the entire portion of the cavity C between the points A and B is permanently ventilated, preferably in the direction A to B to limit the residence time of the air / gas mixture.
    [0014] The residence time of the ventilation air between points A and B and the temperature of the air / fuel gas mixture at point B is calculated to avoid self-ignition of the mixture. For example, it is possible to calculate the air flow to ensure that the residence time of the combustible gas in the hot air makes it impossible to self-ignite the gas mixture, at the temperature of the gas mixture lower than the temperature of the gas. auto-ignition of the fuel. Indeed, the autoignition time varies depending on the temperature of the gas mixture, the fuel / air mixture igniting faster as the temperature of the mixture increases. This is the reason why the ventilation means have a calibrated passage 9 capable of adjusting the air flow in the cavity C to ensure that the air flow makes it possible to evacuate towards the outside the potential leakage of fuel through the control valve V2, through the vent 8, ensuring that the residence time of the gas mixture in the cavity is less than the self-ignition time of the mixture. Of course, it is not beyond the scope of the invention if this function is provided by control valves V5, V6 and V11. For example, the temperature of the instrumentation air conveyed by the supply line 6 is at room temperature. With regard to the hot purge air from the compressor, its temperature after expansion and cooling is of the order of room temperature. But it is not beyond the scope of the invention if it rises to 200 ° C, the flow then being increased to overcome the self-ignition delay which is then shorter. Referring to Figure 2, the ventilation of the cavity C is implemented during the supply of fuel injectors. During this supply phase, the valves V1, V2 and V3 are closed, and the supply valve V4 is open.
    [0015] When venting the cavity C by means of the hot purge air, the valves V6 and V7 are opened, and the valve V5 and V11 is closed. On the other hand, when it is desired to ventilate the cavity by the compressed air used to actuate the instrumentation of the installation, the valve V5 is opened and the valve V6 is closed, the valve V7 of the vent remaining open. . Finally, when it is desired to ventilate the cavity by the intermediate air of the compressor of the turbine, the valve V11 is opened and the valves V6 and V5 are closed, the valve V7 of the vent remaining open. Reference will now be made with reference to FIGS. 3 to 9, other embodiments of the ventilation means for injecting into the cavity a flow of ventilation air.
    [0016] In these figures, elements identical to those described above with reference to Figure 1 bear the same reference numbers. In fact, these FIGS. 3 to 9 show the fuel supply circuit 2 associated with its control valve 4, the hot air purge circuit 3 equipped with its control valves V1 and V2 which delimit between them the cavity C and the second nitrogen purge circuit 4 for supply circuit 2, with its control valve 3. In the embodiment of FIG. 3, the ventilation means comprise a line 10 connected to the outside the installation to collect ambient air. This line 10 is equipped with a valve V5 and a filter F. In this case, the cavity C is provided with a single vent consisting of a discharge line L with its valve V7 and provided at the point B. The line L is here provided with an exhaust fan V. In this embodiment, the fan V is dimensioned so as to obtain a flow rate that depends on the type of gas and the temperature of the hot air. purge. In particular, the fan is dimensioned so that the extraction flow rate is sufficient to avoid any contact between the fuel and the hot air purge possibly present in the cavity C for a duration equal to or greater than the self-ignition delay . Of course, alternatively, it will be possible to use a fan sized so as to generate a displacement speed sufficient to evacuate the fuel / air mixture before the auto-ignition or to adjust the gas flow by providing a calibrated passage (not shown) in the ventilation means, for example at line 10, downstream of the valve 5.
    [0017] As is conceivable, according to this embodiment, the cavity C is depressed. The hot purge air is generally at a pressure greater than 10 bar, the venturi effect generated by the speed of the air passing through the cavity, and acting on a possible leakage of the valve V1, is negligible compared to the pressure difference between the cavity and the fuel circuit. In the embodiment of FIG. 3, the air is sucked by means of a fan V. In a variant, it is possible to mount the fan V in line 10, between the filter F and the valve V5 to maintain forced ventilation of ambient air injected into the cavity C (Figure 4). The advantage of this variant is to avoid the passage of an explosive mixture hot air / gas through a fan which by friction could generate a spark and therefore ignite the mixture.
    [0018] In the embodiment of FIG. 5, the cavity C comprises two discharge lines L and L 'respectively provided at the points A and B, that is to say provided respectively in the vicinity of the valves V1 and V2 defining the cavity C. In this case, the ventilation means are connected to the middle part of the cavity C.
    [0019] In this embodiment, the flow of ventilation air injected into the cavity C splits into two ventilation flows (arrows F and F ') discharged to the outside by the evacuation lines L and L'driving each of them. leaks, either fuel gas or hot air, to the outside under the control of valves V7 and V8.
    [0020] Thus, in this embodiment, the first evacuation line L evacuates a mixture of relatively cold air and fuel leaks, while the other evacuation line L evacuates a mixture of hot air purge and air. 'cold air.
    [0021] As can be seen, this embodiment corresponds in part to the arrangement of FIG. 1. In other words, the air used to sweep the cavity comes either from the instrumentation air 6, or from the intermediate stage of the compressor after expansion and cooling 7.
    [0022] The ventilation airflow must be sufficient to overcome a leakage counterpressure and contain each leak by directing it to the respective vents at points A or B. Of course, the residence time constraints at point B and the temperature of the mixture limiting any risk of self-ignition must be respected. As shown in FIG. 6, to facilitate the separation of the ventilation air flow, an aerodynamic section P may be provided in the zone in which the ventilation means open out in order to more easily separate the flow of ventilation air in two. flow directed respectively to the points A and B. Of course, as shown in Figure 7, such an embodiment is also compatible with the embodiments of Figures 3 and 4 in which the ambient air is used to ventilate the cavity .
    [0023] In other words, the embodiment according to which the cavity C has two outwardly opening vents can provide for taking the ventilation air from the outside, after filtering by means of a filter F to create a forced air flow by means of a fan B divided into two ventilation flows directed respectively to the points A and B by means of an aerodynamic profile P (Figure 7). Of course, in this case, the profile P may be optional if the forced air flow is sufficient.
    [0024] It would also be possible, alternatively, to suck the air using two fans provided on the discharge lines L and L ', as previously described with reference to FIG. 3. However, as mentioned previously, this device could have as disadvantage of putting the explosive mixture in contact with a fan which, by friction, could generate a spark and ignite the mixture. For example, the profile P can be made in the form of a particular connection, for example with three branches ensuring the connection of the ventilation means to the cavity C. Another advantage of the aerodynamic profile P consists in allowing a separation of fluids which can accept a larger leak. Referring finally to Figures 8 and 9, it can be provided that when the ventilation means are configured to generate two ventilation flows directed to two respective vents, the cavity C can be provided with a valve V9 so as to separate the cavity in two avoiding any mixing of the exhaust air flows discharged to their respective vents. Such an embodiment can of course be envisaged when the ventilation air comes from the control network of the instrumentation of the gas turbine or the purge air (FIG. 8), or from the ambient air ( Figure 9), or an intermediate stage of the compressor. Due to the physical separation created by the valve V9, this fluid separation mode can withstand a higher leakage back pressure, for example in the case where the valve V1 or the valve V2 is not completely closed, thus allowing a not inconsiderable flow.
    权利要求:
    Claims (11)
    [0001]
    REVENDICATIONS1. Installation for supplying a combustion chamber with at least one combustible fluid, comprising at least one circuit (2) for supplying the combustion chamber with combustible fluid and at least one circuit (3) for purging the combustion circuits. a supply connected to a source of relatively hot purge air and to said supply circuit and provided with at least two isolation valves (V1, V2) delimiting between them a cavity (C) in said purge circuit, characterized in it comprises ventilation means (5) for injecting into the cavity a flow of ventilation air relatively cold.
    [0002]
    2. Installation according to claim 1, wherein the ventilation means comprise connecting means (6) to a source of high pressure instrumentation gas associated with a valve (V5) for regulating the flow of instrumentation gas.
    [0003]
    3. Installation according to claim 2, wherein the ventilation means comprises connecting means (7) to a compressor and expansion and cooling means (8) for injecting into the cavity a cooled flow of purge air from of the compressor.
    [0004]
    4. Installation according to one of claims 1 and 2, wherein the ventilation means comprise a calibrated passage (9) for adjusting the flow of ventilation air injected into the cavity.
    [0005]
    5. Installation according to claim 1, wherein the ventilation means comprise ambient air sampling means associated with a filter (F) and a valve (V8) for adjusting the ambient air flow and a device ( V) capable of driving a forced ambient air flow into the cavity.
    [0006]
    6. Installation according to any one of claims 2 to 5, wherein the cavity is provided with a vent (V7) venting ventilation which opens outwardly of the installation.
    [0007]
    7. Installation according to any one of claims 2 to 5, wherein the cavity is provided with two vents (V7, V8) placed respectively on the side of the isolation valves and opening outwardly of the installation.
    [0008]
    8. Installation according to claim 7, wherein the ventilation means comprises a profiled member (P) for separating the flow of ventilation air in two ventilation rates respectively led to the two vents.
    [0009]
    9. Installation according to claim 8, wherein the cavity further comprises a third isolation valve (V9) separating the cavity into two secondary cavities in which are respectively injected the two ventilation rates.
    [0010]
    10. Power plant according to any one of claims 1 to 9 for the supply of a combustion chamber of a gas turbine.
    [0011]
    11. A method for supplying a combustion chamber with at least one combustible fluid, for the implementation of a feed installation comprising at least one fuel-fuel combustion chamber supply circuit (2). and at least one purge circuit (3) of the supply circuits connected to a source of relatively hot purge air and to said supply circuit and provided with at least two isolation valves (V1, V2) delimiting between they have a cavity (C) in the purge circuit, characterized in that a flow of relatively cold ventilation air is injected into the cavity.
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    法律状态:
    2015-11-18| PLFP| Fee payment|Year of fee payment: 2 |
    2016-06-24| PLSC| Publication of the preliminary search report|Effective date: 20160624 |
    2016-11-16| PLFP| Fee payment|Year of fee payment: 3 |
    2017-09-27| PLFP| Fee payment|Year of fee payment: 4 |
    2019-11-13| PLFP| Fee payment|Year of fee payment: 6 |
    2020-10-06| PLFP| Fee payment|Year of fee payment: 7 |
    2021-11-17| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1463238A|FR3030629B1|2014-12-23|2014-12-23|INSTALLATION AND METHOD FOR SUPPLYING A COMBUSTION CHAMBER HAVING A VENTILATED CAVITY BY HOT AIR FROM PURGE|FR1463238A| FR3030629B1|2014-12-23|2014-12-23|INSTALLATION AND METHOD FOR SUPPLYING A COMBUSTION CHAMBER HAVING A VENTILATED CAVITY BY HOT AIR FROM PURGE|
    US14/966,513| US10473060B2|2014-12-23|2015-12-11|Method and system for a gas turbine engine air ventilation purge circuit|
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