Automatic detection device for gas turbine

Abstract

The utility model relates to the technical field of gas turbines, in particular to an automatic detection device for a gas turbine, which comprises a gas turbine body, a gas inlet end of the gas turbine body is provided with a gas guide piece, the gas guide piece comprises a gas inlet pipe shell, and the gas inlet pipe shell is communicated and fixed at the gas inlet end of the gas turbine body. A plurality of air inlet screw cylinders are evenly fixed to the outer circumferential face of the air inlet pipe shell in a penetrating mode, communicating screw pipes are assembled to the multiple air inlet screw cylinders in a communicating mode, electronic valves are assembled to the communicating screw pipes in a communicating mode, and first air inlet pieces, second air inlet pieces and third air inlet pieces are assembled to the ends of the communicating screw pipes on the multiple air inlet screw cylinders in a communicating mode correspondingly. A first cooling part is assembled on the communicating screw pipe of the first air inlet part in a communicating manner; and a third cooling part and the first cooling part are sequentially assembled on the communicating screw pipe of the second air inlet part in a communicating manner. The air cooling grade is adjusted according to the air temperature, and the air cooling adjusting range of the gas turbine is guaranteed.

Description

Technical Field

[0001] The utility model relates to the technical field of gas turbines, and particularly relates to an automatic detection device for a gas turbine. Background Technique

[0002] When a gas turbine is working, the gas temperature at the outlet of the combustion chamber can be as high as over 1500 °C, which poses extremely high requirements on the materials of the blades and other high-temperature components. In order to protect these key components from high-temperature damage, effective cooling measures are usually required. By introducing cold air into the internal channels of the blades, the convective heat transfer between the cold air and the hot blade surface is used to take away the heat.

[0003] The existing patent with publication number CN201650463U and name "A Gas Turbine" includes a compressor, a combustion chamber, and a turbine. A cavity is provided on the side wall of the air distribution cylinder of the combustion chamber; the cavity is used to accommodate a coolant to protect the air distribution cylinder through the coolant; all the high-pressure gas generated by the compressor enters the air distribution cylinder to be mixed with the fuel in the air distribution cylinder for combustion. By providing a cavity on the side wall of the air distribution cylinder of the combustion chamber and accommodating the coolant in the cavity to cool and protect the air distribution cylinder through the coolant, the temperature of the air distribution cylinder of the combustion chamber can be effectively reduced, so that all the high-pressure gas generated by the compressor can enter the air distribution cylinder to be mixed with the fuel for combustion without leaving part of the high-pressure gas to cool the air distribution cylinder of the combustion chamber.

[0004] However, the above gas turbine cools the air through a coolant during use, but the intake end of the above gas turbine only has a single cooling component, and the cooling effect is single. It is impossible to adjust the air cooling level according to the air temperature, which affects the air cooling adjustment range of the gas turbine. Summary of the Utility Model

[0005] The utility model solves the problems in the related art and provides an automatic detection device for a gas turbine.

[0006] To solve the above technical problems, the present utility model is realized through the following technical solutions: An automatic detection device for a gas turbine, comprising a gas turbine body, a gas guiding member is arranged at the air inlet end of the gas turbine body. The gas guiding member includes an air inlet pipe shell, the air inlet pipe shell is connected and fixed at the air inlet end of the gas turbine body, and a plurality of air inlet screw cylinders are uniformly and penetratingly fixed on the outer circumferential surface of the air inlet pipe shell. And a communication screw pipe is connected and assembled on each of the plurality of air inlet screw cylinders, and an electronic valve is connected and assembled on the communication screw pipe. The communication screw pipe ends of the plurality of air inlet screw cylinders are respectively connected and assembled with a first air inlet member, a second air inlet member and a third air inlet member. A first cooling member is connected and assembled on the communication screw pipe of the first air inlet member. A third cooling member and a first cooling member are sequentially connected and assembled on the communication screw pipe of the second air inlet member. A second cooling member, a third cooling member and a first cooling member are sequentially connected and assembled on the communication screw pipe of the third air inlet member.

[0007] As a preferred solution, a controller and a temperature sensor are fixed at the other end of the air inlet pipe shell. The output end of the temperature sensor is electrically connected to the input end of the controller. The output end of the controller is respectively electrically connected to the input ends of the electronic valves on the first air inlet member, the second air inlet member and the third air inlet member.

[0008] As a preferred solution, one end of the communication screw pipe is connected and fixed with a screw ring, and the screw ring is threadedly assembled in the air inlet screw cylinder.

[0009] As a preferred solution, the first cooling member includes a cooling cylinder, and a plurality of mesh sheets are horizontally and penetratingly fixed on the outer circumferential surface of the cooling cylinder in the vertical direction.

[0010] As a preferred solution, the third cooling member includes a communication pipe, and a plurality of shunt pipes are vertically and penetratingly fixed in the middle of the communication pipe. And a wind cylinder is vertically and penetratingly sleeved outside the communication pipe. An air inlet pipe is penetratingly fixed on the upper part of the outer wall of the wind cylinder, and an air pump is connected and assembled on the air inlet pipe. An exhaust pipe is penetratingly fixed on the lower part of the outer wall of the wind cylinder.

[0011] As a preferred solution, the second cooling member includes a gas guiding cylinder, and a plurality of gas distribution pipes are vertically and penetratingly fixed in the middle of the gas guiding cylinder. And a sleeve is vertically and penetratingly sleeved outside the gas guiding cylinder. A liquid inlet pipe is penetratingly fixed on the upper part of the outer wall of the sleeve, and a liquid outlet pipe is penetratingly fixed on the lower part of the outer wall of the sleeve.

[0012] As a preferred solution, internal threads are provided on the inner walls of one ends of the cooling cylinder, the gas guiding cylinder and the communication pipe. And a communication screw shell is connected and fixed at the other end of the cooling cylinder, the gas guiding cylinder and the communication pipe. The communication screw shell is assembled and matched with the internal threads at any one end of the cooling cylinder, the gas guiding cylinder and the communication pipe. The communication screw shell is threadedly assembled and communicated with the end of the communication screw pipe.

[0013] Compared with the prior art, the beneficial effects of the utility model are as follows: During use, the air inlet cover on the air guiding part is connected and fixed to the air inlet end of the gas turbine body. Then, a plurality of air inlet screw cylinders on the outer wall of the air inlet cover are respectively connected and assembled with connecting screw pipes. Then, the end parts of the connecting screw pipes on the plurality of air inlet screw cylinders are respectively connected and assembled with a first air inlet part, a second air inlet part, and a third air inlet part. A first cooling part is connected and assembled on the connecting screw pipe of the first air inlet part. A third cooling part and a first cooling part are successively connected and assembled on the connecting screw pipe of the second air inlet part. A second cooling part, a third cooling part, and a first cooling part are successively connected and assembled on the connecting screw pipe of the third air inlet part. Later, the temperature sensor detects the external air temperature value. According to the detected air temperature, the controller controls the opening and closing of the electronic valves on the connecting screw pipes of the first air inlet part, the second air inlet part, and the third air inlet part. When the temperature is relatively high, the electronic valve on the third air inlet part is opened, and the air is gradually cooled through the second cooling part, the third cooling part, and the first cooling part, with a better cooling effect. At the same time, when the temperature is high, the electronic valve on the second air inlet part is opened, and the air is gradually cooled through the third cooling part and the first cooling part. When the temperature is low, the electronic valve on the first air inlet part is opened, and the air is gradually cooled through the first cooling part. Thus, the air cooling level is adjusted according to the air temperature, ensuring the air cooling adjustment range of the gas turbine. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 is the overall structural schematic diagram of the utility model;

[0015] Figure 2 is the exploded structural schematic diagram of the utility model;

[0016] Figure 3 is the structural schematic diagram of the air inlet part in the exploded state in the embodiment of the utility model;

[0017] Figure 4 is the structural schematic diagram of the second cooling part in the exploded state in the embodiment of the utility model;

[0018] Figure 5 is the structural schematic diagram of the third cooling part in the exploded state in the embodiment of the utility model;

[0019] Figure 6 is the structural schematic diagram of the first cooling part in the exploded state in the embodiment of the utility model.

[0020] In the figure: 1. Gas turbine body; 2. Air guide component; 21. Inlet pipe housing; 22. Inlet air screw barrel; 23. Controller; 24. Temperature sensor; 25. Connecting screw pipe; 251. Screw ring; 26. Electronic valve; 3. First air inlet component; 4. Second air inlet component; 5. Third air inlet component; 6. First cooling component; 61. Cooling barrel; 62. Mesh; 7. Second cooling component; 71. Air guide barrel; 72. Branch pipe; 73. Sleeve; 74. Liquid inlet pipe; 75. Liquid outlet pipe; 8. Third cooling component; 81. Connecting pipe; 82. Shunt pipe; 83. Air duct; 84. Inlet pipe; 841. Air pump; 85. Exhaust pipe; 9. Connecting screw housing. Detailed implementation mode

[0021] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. The following description of at least one exemplary embodiment is actually illustrative only and in no way limits the present invention and its application or use. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts belong to the scope of protection of the present invention.

[0022] It should be noted that the terms used here are only for describing the specific implementation mode and are not intended to limit the exemplary embodiments according to the present application. As used here, unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. In addition, it should be understood that when the terms "include" and / or "comprise" are used in this specification, they indicate the presence of features, steps, operations, devices, components and / or their combinations.

[0023] Unless otherwise specifically stated, the relative arrangement, numerical expressions and values of the components and steps set forth in these embodiments do not limit the scope of the present invention. At the same time, it should be understood that, for the sake of convenience of description, the dimensions of the various parts shown in the drawings are not drawn in actual proportional relationship. Technologies, methods and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, the technologies, methods and devices should be regarded as part of the authorized specification. In all the examples shown and discussed here, any specific value should be interpreted as merely exemplary and not as a limitation. Therefore, other examples of the exemplary embodiments may have different values. It should be noted that like reference numerals and letters denote like items in the following drawings, and therefore, once an item is defined in one drawing, it does not need to be further discussed in subsequent drawings.

[0024] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by orientation words such as "front, rear, upper, lower, left, right", "lateral, vertical, perpendicular, horizontal" and "top, bottom", etc. is usually based on the orientation or positional relationship shown in the drawings. It is only for the convenience of describing the present utility model and simplifying the description. Without contrary description, these orientation words do not indicate and imply that the device or element referred to must have a specific orientation or be constructed and operated in a specific orientation. Therefore, it should not be construed as a limitation on the protection scope of the present utility model; the orientation words "inside, outside" refer to the inside and outside relative to the contour of each component itself.

[0025] For ease of description, spatial relative terms such as "above...", "over...", "on the upper surface of...", "above-mentioned", etc. can be used here to describe the spatial positional relationship between a device or feature shown in the drawings and other devices or features. It should be understood that the spatial relative terms are intended to include different orientations in use or operation in addition to the orientation described in the drawings for the device. For example, if the device in the drawing is inverted, the device described as "above other devices or structures" or "over other devices or structures" will then be positioned as "below other devices or structures" or "under other devices or structures". Thus, the exemplary term "above..." can include both the orientations of "above..." and "below...". The device can also be positioned in other different ways (rotated 90 degrees or in other orientations), and corresponding interpretations should be made for the spatial relative descriptions used here.

[0026] In addition, it should be noted that the use of words such as "first", "second", etc. to limit components is only for the convenience of distinguishing the corresponding components. Without additional statement, the above-mentioned words have no special meaning. Therefore, it should not be construed as a limitation on the protection scope of the present utility model.

[0027] Such as Figures 1 to 5As shown in the figure, an automatic detection device for a gas turbine includes a gas turbine body 1. A gas guiding member 2 is provided at the air inlet end of the gas turbine body 1. The gas guiding member 2 includes an air inlet pipe shell 21. The air inlet pipe shell 21 is connected and fixed at the air inlet end of the gas turbine body 1. A plurality of air inlet screw cylinders 22 are uniformly and penetratingly fixed on the outer circumferential surface of the air inlet pipe shell 21. A communication screw pipe 25 is connected and assembled on each of the plurality of air inlet screw cylinders 22. A type ASCO 8262 electronic valve 26 is connected and assembled on the communication screw pipe 25. The communication screw pipe 25 ends of the plurality of air inlet screw cylinders 22 are respectively connected and assembled with a first air inlet member 3, a second air inlet member 4, and a third air inlet member 5. A first cooling member 6 is connected and assembled on the communication screw pipe 25 of the first air inlet member 3. A third cooling member 8 and a first cooling member 6 are successively connected and assembled on the communication screw pipe 25 of the second air inlet member 4. A second cooling member 7, a third cooling member 8, and a first cooling member 6 are successively connected and assembled on the communication screw pipe 25 of the third air inlet member 5. A type S7-1500 controller 23 and a type DS18B20 temperature sensor 24 are fixed at the other end of the air inlet pipe shell 21. The output end of the temperature sensor 24 is electrically connected to the input end of the controller 23. The output end of the controller 23 is respectively electrically connected to the input ends of the electronic valves 26 on the first air inlet member 3, the second air inlet member 4, and the third air inlet member 5. One end of the communication screw pipe 25 is connected and fixed with a screw ring 251, and the screw ring 251 is threadedly assembled in the air inlet screw cylinder 22. During use, the air inlet cover shell 21 on the gas guiding member 2 is connected and fixed to the air inlet end of the gas turbine body 1. Then, the communication screw pipes 25 are respectively connected and assembled to the plurality of air inlet screw cylinders 22 on the outer wall of the air inlet cover shell 21. Then, the communication screw pipe 25 ends of the plurality of air inlet screw cylinders 22 are respectively connected and assembled with a first air inlet member 3, a second air inlet member 4, and a third air inlet member 5. A first cooling member 6 is connected and assembled on the communication screw pipe 25 of the first air inlet member 3. A third cooling member 8 and a first cooling member 6 are successively connected and assembled on the communication screw pipe 25 of the second air inlet member 4. A second cooling member 7, a third cooling member 8, and a first cooling member 6 are successively connected and assembled on the communication screw pipe 25 of the third air inlet member 5. Later, the external air temperature value is detected by the temperature sensor 24. According to the detected air temperature, the controller 23 controls the opening and closing of the electronic valves 26 on the first air inlet member 3, the second air inlet member 4, and the third air inlet member 5. When the temperature is relatively high, the electronic valve 26 on the third air inlet member 5 is opened, and the air is gradually cooled through the second cooling member 7, the third cooling member 8, and the first cooling member 6, and the cooling effect is better. At the same time, when the temperature is high, the electronic valve 26 on the second air inlet member 4 is opened, and the air is gradually cooled through the third cooling member 8 and the first cooling member 6. When the temperature is low, the electronic valve 26 on the first air inlet member 3 is opened, and the air is gradually cooled through the first cooling member 6. Thus, the cooling level of the air is adjusted according to the air temperature.Guarantees the air cooling adjustment range of the gas turbine.

[0028] In one embodiment, as Figure 3 and Figure 6 shown, the first cooling member 6 of the liquid inlet pipe 74 includes a cooling cylinder 61. On the outer circumferential surface of the cooling cylinder 61 of the liquid inlet pipe 74, multiple mesh sheets 62 are horizontally penetrated and fixed along the vertical direction. During use, the cooling cylinder 61 is made of metal. The entering air contacts the wall of the cooling cylinder 61 and the mesh sheets 62, and the heat of the passing air is transferred to the outside, cooling the passing air.

[0029] In one embodiment, as Figure 3 and Figure 5 shown, the third cooling member 8 of the liquid inlet pipe 74 includes a communication pipe 81. In the middle of the communication pipe 81 of the liquid inlet pipe 74, multiple shunt pipes 82 are vertically penetrated and fixed. And a wind cylinder 83 is vertically penetrated and sleeved outside the communication pipe 81. An air inlet pipe 84 is penetrated and fixed on the upper part of the outer wall of the wind cylinder 83 of the liquid inlet pipe 74, and an air pump 841 is connected and assembled on the air inlet pipe 84. An exhaust pipe 85 is penetrated and fixed on the lower part of the outer wall of the wind cylinder 83 of the liquid inlet pipe 74. During use, the air enters the communication pipe 81 and is shunted by the multiple shunt pipes 82. The air contacts the shunt pipes 82, and the heat is transferred to the outer wall of the shunt pipes 82. Then the air pump 841 is started to drive the external air into the wind cylinder 83. The flowing air contacts the shunt pipes 82 and carries the heat in the passing air out, accelerating the air cooling effect.

[0030] In one embodiment, as Figure 3 and Figure 4 shown, the second cooling member 7 of the liquid inlet pipe 74 includes a gas guide cylinder 71. In the middle of the gas guide cylinder 71 of the liquid inlet pipe 74, multiple gas distribution pipes 72 are vertically penetrated and fixed. And a sleeve 73 is vertically penetrated and sleeved outside the gas guide cylinder 71. An inlet liquid pipe 74 is penetrated and fixed on the upper part of the outer wall of the sleeve 73 of the liquid inlet pipe 74, and an outlet liquid pipe 75 is penetrated and fixed on the lower part of the outer wall of the sleeve 73 of the liquid inlet pipe 74. During use, the air enters the gas guide cylinder 71 and is shunted by the multiple gas distribution pipes 72. The air contacts the gas distribution pipes 72, and the heat is transferred to the outer wall of the gas distribution pipes 72. The flowing coolant in the inlet liquid pipe 74 communicating with the coolant pipe contacts the gas distribution pipes 72 and carries the heat in the passing air out, accelerating the air cooling effect.

[0031] In one embodiment, as Figure 3As shown, internal threads are provided on the inner walls of one ends of the cooling cylinder 61, the air guide cylinder 71, and the connecting pipe 81. At the other ends of the cooling cylinder 61, the air guide cylinder 71, and the connecting pipe 81, a connecting spiral shell 9 is fixedly connected. The liquid inlet pipe 74 is assembled and fitted with the internal thread at any one end of the connecting spiral shell 9, the cooling cylinder 61, the air guide cylinder 71, and the connecting pipe 81. The liquid inlet pipe 74 is threadedly assembled and connected to the end of the connecting spiral shell 9 and the end of the connecting spiral pipe 25. The connecting spiral shells 9 at the adjacent ends of the cooling cylinder 61, the air guide cylinder 71, and the connecting pipe 81 are threadedly assembled and connected to the end of the connecting spiral pipe 25, which is convenient for assembly and connection to form an integral body to cool the passing air.

[0032] In this embodiment, during use, the air inlet cover 21 on the air guide member 2 is fixedly connected to the air inlet end of the gas turbine body 1. Then, a plurality of air inlet spiral cylinders 22 on the outer wall of the air inlet cover 21 are respectively connected and assembled with the connecting spiral pipes 25. Then, the ends of the connecting spiral pipes 25 on the plurality of air inlet spiral cylinders 22 are respectively connected and assembled with a first air inlet member 3, a second air inlet member 4, and a third air inlet member 5. A first cooling member 6 is connected and assembled on the connecting spiral pipe 25 of the first air inlet member 3. The liquid inlet pipe 74 is connected and assembled with a third cooling member 8 and a first cooling member 6 in sequence on the connecting spiral pipe 25 of the second air inlet member 4. The liquid inlet pipe 74 is connected and assembled with a second cooling member 7, a third cooling member 8, and a first cooling member 6 in sequence on the connecting spiral pipe 25 of the third air inlet member 5. Later, the temperature sensor 24 detects the external air temperature value. According to the detected air temperature, the controller 23 controls the opening and closing of the solenoid valves 26 on the connecting spiral pipes 23 of the first air inlet member 3, the second air inlet member 4, and the third air inlet member 5. When the temperature is relatively high, the solenoid valve 26 on the third air inlet member 5 is opened, and the air is gradually cooled through the second cooling member 7, the third cooling member 8, and the first cooling member 6, and the cooling effect is better. At the same time, when the temperature is high, the solenoid valve 26 on the second air inlet member 4 is opened, and the air is gradually cooled through the third cooling member 8 and the first cooling member 6. When the temperature is low, the solenoid valve 26 on the first air inlet member 3 is opened.

[0033] The above is the preferred embodiment of the present invention. Those skilled in the art of the present invention can also make changes and modifications to the above embodiment. Therefore, the present invention is not limited to the above specific embodiments. Any obvious improvements, substitutions, or variations made by those skilled in the art based on the present invention fall within the protection scope of the present invention.

Claims

1. An automatic detection device for a gas turbine, characterized in that, It includes a gas turbine body (1). A gas guiding member (2) is provided at the air inlet end of the gas turbine body (1). The gas guiding member (2) includes an air inlet pipe shell (21). The air inlet pipe shell (21) is connected and fixed at the air inlet end of the gas turbine body (1). A plurality of air inlet screw cylinders (22) are uniformly and penetratively fixed on the outer circumferential surface of the air inlet pipe shell (21). A communicating screw pipe (25) is connected and assembled on each of the plurality of air inlet screw cylinders (22). An electronic valve (26) is connected and assembled on the communicating screw pipe (25). The end portions of the communicating screw pipes (25) on the plurality of air inlet screw cylinders (22) are respectively connected and assembled with a first air inlet member (3), a second air inlet member (4), and a third air inlet member (5). A first cooling member (6) is connected and assembled on the communicating screw pipe (25) of the first air inlet member (3). A third cooling member (8) and a first cooling member (6) are successively connected and assembled on the communicating screw pipe (25) of the second air inlet member (4). A second cooling member (7), a third cooling member (8), and a first cooling member (6) are successively connected and assembled on the communicating screw pipe (25) of the third air inlet member (5).

2. The automatic detection device for a gas turbine according to claim 1, characterized in that: A controller (23) and a temperature sensor (24) are fixed at the other end of the air inlet pipe shell (21). The output end of the temperature sensor (24) is electrically connected to the input end of the controller (23). The output end of the controller (23) is respectively electrically connected to the input ends of the electronic valves (26) on the first air inlet member (3), the second air inlet member (4), and the third air inlet member (5).

3. The automatic detection device for a gas turbine according to claim 1, characterized in that: One end of the communicating screw pipe (25) is connected and fixed with a screw ring (251), and the screw ring (251) is threadedly assembled in the air inlet screw cylinder (22).

4. An automatic detection device for a gas turbine according to claim 1, characterized in that: The first cooling member (6) includes a cooling cylinder (61). A plurality of mesh sheets (62) are horizontally penetrated and fixed on the outer circumferential surface of the cooling cylinder (61) in the vertical direction.

5. An automatic detection device for a gas turbine according to claim 4, characterized in that: The third cooling member (8) includes a communicating pipe (81). A plurality of shunt pipes (82) are vertically penetrated and fixed in the middle of the communicating pipe (81). A wind cylinder (83) is vertically penetrated and sleeved outside the communicating pipe (81). An air inlet pipe (84) is penetrated and fixed on the upper part of the outer wall of the wind cylinder (83). An air pump (841) is connected and assembled on the air inlet pipe (84). An exhaust pipe (85) is penetrated and fixed on the lower part of the outer wall of the wind cylinder (83).

6. The automatic detection device for a gas turbine according to claim 5, wherein: The second cooling member (7) includes a gas guiding cylinder (71). A plurality of gas distributing pipes (72) are vertically penetrated and fixed in the middle of the gas guiding cylinder (71). A sleeve (73) is vertically penetrated and sleeved outside the gas guiding cylinder (71). A liquid inlet pipe (74) is penetrated and fixed on the upper part of the outer wall of the sleeve (73). A liquid outlet pipe (75) is penetrated and fixed on the lower part of the outer wall of the sleeve (73).

7. The automatic detection device for a gas turbine according to claim 6, characterized in that: Internal threads are provided on the inner walls of one ends of the cooling cylinder (61), the air guiding cylinder (71) and the connecting pipe (81), and a connecting spiral housing (9) is fixedly connected to the other ends of the cooling cylinder (61), the air guiding cylinder (71) and the connecting pipe (81). The connecting spiral housing (9) is assembled and fitted with the internal threads at any one end of the cooling cylinder (61), the air guiding cylinder (71) and the connecting pipe (81), and the connecting spiral housing (9) is threadedly assembled and connected to the end of the connecting spiral pipe (25).

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