Tool equipment for gas tightness detection of gas turbine

Abstract

The utility model discloses gas turbine airtightness detection tool equipment, and particularly relates to the field of gas turbines, comprising a support frame, a bidirectional threaded rod rotatably connected in the support frame, handles fixedly connected at two ends of the bidirectional threaded rod, a guide rod fixedly connected in the support frame, and a fixed plate slidably connected on the outer wall of the guide rod. The fixing plate is slidably connected to the top of the supporting frame and connected to the outer wall of the two-way threaded rod through threads, a sleeve is fixedly installed on one side of the fixing plate, a plugging air bag is fixedly connected to the inner wall of the sleeve, and a pressing ring is fixedly connected to the interior of the plugging air bag. According to the gas turbine port sealing device, the fixing plate and the blocking air bag are arranged, the blocking air bag expands to be tightly attached to the gas turbine port, the gas turbine port is sealed through expansion of the blocking air bag, the effect of rapidly sealing the gas turbine port is achieved, and workers can seal the gas turbine conveniently.

Description

Technical Field

[0001] The utility model relates to the field of gas turbines, and more specifically, to a tooling device for gas turbine air tightness detection. Background Art

[0002] A gas turbine is an internal combustion power machine that uses a continuously flowing gas as a working fluid to drive the impeller to rotate at high speed, converting the energy of the fuel into useful work. It is a rotating impeller heat engine. In the main flow of air and gas, the gas turbine cycle consists of only three major components: the compressor, the combustion chamber, and the gas turbine, which is generally called a simple cycle. Most gas turbines use a simple cycle solution.

[0003] When testing the sealing performance of a gas turbine, it is necessary to seal the air inlet and outlet ends of the gas turbine, and then inflate the interior of the gas turbine through a gas generator and an air pipe to allow the internal pressure of the gas turbine to reach the testing requirements, and finally test whether the gas turbine is leaking. However, the existing technology is too complicated when sealing and fixing the gas turbine, and it is not convenient for the gas turbine to be sealed and fixed quickly, and it is not convenient for the staff to test the air tightness of the gas turbine. In view of this problem, it is necessary for technical personnel in this field to develop a tooling equipment for gas turbine air tightness testing. Utility Model Content

[0004] In order to overcome the above-mentioned defects of the prior art, an embodiment of the utility model provides a tooling equipment for gas turbine air tightness detection, which provides a fixing plate and a sealing air bag, so that the sealing air bag is expanded and fits tightly on the port of the gas turbine, and the port of the gas turbine is expanded and sealed by the sealing air bag, so as to achieve the effect of quickly sealing the port of the gas turbine, making it convenient for the staff to seal the gas turbine, so as to solve the problems raised in the above-mentioned background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a tooling equipment for gas turbine air tightness detection, comprising a support frame, the support frame is rotatably connected with a two-way threaded rod inside, handles are fixedly connected with both ends of the two-way threaded rod, the support frame is fixedly connected with a guide rod inside, the outer wall of the guide rod is slidably connected with a fixing plate, the fixing plate is slidably connected to the top of the support frame, the fixing plate is threadedly connected to the outer wall of the two-way threaded rod, a sleeve is fixedly installed on one side of the fixing plate, a sealing airbag is fixedly connected to the inner wall of the sleeve, a pressure ring is fixedly connected to the inside of the sealing airbag, a plurality of air holes are opened inside the pressure ring, one side of the sealing airbag is fixedly connected with a connecting pipe, and one end of the connecting pipe is connected with an annular airbag.

[0006] In a preferred embodiment, one side of the annular airbag is fixedly connected to the inside of the fixing plate, and a spring is fixedly installed inside the annular airbag.

[0007] In a preferred embodiment, a pressure plate is fixedly connected to one side of the annular airbag, the pressure plate is sleeved on the outer wall of the connecting pipe, and the pressure plate is slidably connected to the inside of the fixed plate.

[0008] In a preferred embodiment, a cylinder is fixedly connected to the interior of the fixing plate, the cylinder is inserted into the interior of the annular airbag, and the blocking airbag is fixedly connected to the outer wall of the cylinder.

[0009] In a preferred embodiment, the outer wall of the cylinder is connected to an air pipe, and the air pipe is plugged into the interior of the fixing plate.

[0010] In a preferred embodiment, one end of the air pipe is fixedly connected to a gas generator, and an outer wall of the guide rod is provided with a limit plate, and the limit plate is slidably connected to the inside of the fixed plate.

[0011] In a preferred embodiment, a threaded rod is rotatably connected to the top of the limiting plate, the threaded rod is threadedly connected to the inside of the fixing plate, and a supporting block is fixedly connected to the top of the supporting frame.

[0012] Technical effects and advantages of the utility model:

[0013] 1. The utility model provides a fixing plate and a plugging airbag, so that the plugging airbag expands and fits tightly on the port of the gas turbine, so that the port of the gas turbine is expanded and sealed by the plugging airbag, so as to achieve the effect of quickly sealing the port of the gas turbine, and facilitate the staff to seal the gas turbine;

[0014] 2. The utility model is provided with a limit plate and a threaded rod. After the port of the gas turbine is sealed, the staff can rotate the threaded rod to make the threaded rod descend along the inside of the fixed plate through the thread, and squeeze the limit plate to descend along the inside of the fixed plate, so that the limit plate is stuck on the outer wall of the guide rod, and the fixed plate is limited and fixed, thereby improving the stability of the fixed plate and preventing the fixed plate from displacement. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0016] Figure 2 This is a cross-sectional view of the fixed plate structure of the utility model;

[0017] Figure 3 For this utility model Figure 2 A magnified view of the structure of part A;

[0018] Figure 4 For this utility model Figure 2 Enlarged view of the structure of part B.

[0019] The accompanying drawings are marked as follows: 1. support frame; 2. bidirectional threaded rod; 3. handle; 4. guide rod; 5. fixing plate; 6. sleeve; 7. sealing airbag; 8. pressure ring; 9. air hole; 10. connecting pipe; 11. annular airbag; 12. spring; 13. pressure plate; 14. cylinder; 15. air pipe; 16. gas generator; 17. limit plate; 18. threaded rod; 19. support block. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0021] Example 1: Refer to the attached specification Figure 1-4 The utility model is a gas turbine air tightness detection tooling equipment, including a support frame 1, see Figure 1 The support frame 1 is internally rotatably connected with a bidirectional threaded rod 2, and both ends of the bidirectional threaded rod 2 are fixedly connected with handles 3. The support frame 1 is internally fixedly connected with a guide rod 4, and the outer wall of the guide rod 4 is slidably connected with a fixing plate 5. The fixing plate 5 is slidably connected to the top of the support frame 1. The fixing plate 5 is connected to the outer wall of the bidirectional threaded rod 2 by threads, and a sleeve 6 is fixedly installed on one side of the fixing plate 5. For details, see Figure 3 The inner wall of the sleeve 6 is fixedly connected with a blocking airbag 7, the inside of the blocking airbag 7 is fixedly connected with a pressure ring 8, a plurality of air holes 9 are opened inside the pressure ring 8, one side of the blocking airbag 7 is fixedly connected with a connecting pipe 10, and one end of the connecting pipe 10 is connected with an annular airbag 11;

[0022] One side of the annular airbag 11 is fixedly connected to the inside of the fixing plate 5, a spring 12 is fixedly installed inside the annular airbag 11, one side of the annular airbag 11 is fixedly connected to a pressure plate 13, the pressure plate 13 is sleeved on the outer wall of the connecting pipe 10, the pressure plate 13 is slidably connected to the inside of the fixing plate 5, the inside of the fixing plate 5 is fixedly connected to a cylinder 14, the cylinder 14 is inserted into the inside of the annular airbag 11, and the blocking airbag 7 is fixedly connected to the outer wall of the cylinder 14, see Figure 2 The outer wall of the cylinder 14 is connected to an air pipe 15, which is plugged into the interior of the fixed plate 5. One end of the air pipe 15 is fixedly connected to a gas generator 16. Figure 4The outer wall of the guide rod 4 is provided with a limit plate 17, which is slidably connected to the inside of the fixed plate 5, and the top of the limit plate 17 is rotatably connected to a threaded rod 18, which is threadedly connected to the inside of the fixed plate 5, see Figure 1 A support block 19 is fixedly connected to the top of the support frame 1.

[0023] It should be noted that, when the staff detects the sealing of the gas turbine, firstly, the gas turbine is placed on the support block 19, and the handle 3 is turned, so that the handle 3 drives the bidirectional threaded rod 2 to rotate, and then the bidirectional threaded rod 2 drives the two fixing plates 5 to move toward the direction of the gas turbine on the support block 19, so that the fixing plate 5 drives the sleeve 6 to be sleeved on the outer wall of the port of the gas turbine, so that the port of the gas turbine is inserted into the inside of the blocking airbag 7. As the staff continues to turn the handle 3, the gas turbine will be pressed against the pressure plate 13 through the pressure ring 8 inside the blocking airbag 7. , let the pressing plate 13 slide along the inside of the fixing plate 5 and squeeze the annular airbag 11 to shrink. The shrinkage of the annular airbag 11 will discharge the gas into the inside of the blocking airbag 7 through the connecting pipe 10. The blocking airbag 7 receives the gas and expands. Since the outer wall and the inner wall of the blocking airbag 7 are respectively fixedly connected to the inner wall of the sleeve 6 and the outer wall of the cylinder 14, the blocking airbag 7 can only be tightly fitted on the gas turbine port when it expands, so that the port of the gas turbine is sealed by the expansion of the blocking airbag 7, so as to achieve the effect of quickly sealing the port of the gas turbine, which is convenient for the staff to seal the gas turbine;

[0024] Furthermore, after the port of the gas turbine is sealed, the staff can start the gas generator 16 to make the gas generator 16 work to exhaust gas into the gas pipe 15, and then make the gas pipe 15 discharge gas into the gas turbine through the cylinder 14, until the internal pressure of the gas turbine reaches the detection requirement, and then stop increasing the pressure inside the gas turbine. At this time, the staff can detect the connection seals at various locations of the gas turbine to determine whether the airtightness of the connection seals at various locations is qualified;

[0025] Furthermore, after the staff turns the handle 3 and finally seals the port of the gas turbine, the staff can stop turning the handle 3 and start turning the threaded rod 18, so that the threaded rod 18 descends along the inside of the fixed plate 5 through the thread, and squeezes the limiting plate 17 to descend along the inside of the fixed plate 5, so that the limiting plate 17 is stuck on the outer wall of the guide rod 4, and the fixing plate 5 is limited and fixed, thereby improving the stability of the fixing plate 5 and preventing the fixing plate 5 from being displaced by the pressure when the pressure is increased inside the gas turbine, resulting in the failure to reach the detection pressure inside the gas turbine.

[0026] Finally, a few points should be explained: First, in the description of this application, it should be noted that, unless otherwise specified and limited, the terms "installed", "connected" and "connected" should be understood in a broad sense, which can be a mechanical connection or an electrical connection, or the internal communication of two components, or a direct connection. "upper", "lower", "left" and "right" are only used to indicate relative positional relationships. When the absolute position of the object being described changes, the relative positional relationship may change;

[0027] Secondly: In the drawings of the embodiments disclosed in the present utility model, only the structures related to the embodiments disclosed in the present utility model are involved, and other structures can refer to the general design. In the absence of conflict, the same embodiment and different embodiments of the present utility model can be combined with each other;

[0028] Finally: The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present utility model should be included in the protection scope of the present utility model.

Claims

1. A gas turbine air tightness detection tooling device, comprising a support frame (1), characterized in that: The support frame (1) is rotatably connected to a bidirectional threaded rod (2), and handles (3) are fixedly connected to both ends of the bidirectional threaded rod (2). The support frame (1) is fixedly connected to a guide rod (4), and the outer wall of the guide rod (4) is slidably connected to a fixing plate (5). The fixing plate (5) is slidably connected to the top of the support frame (1). The fixing plate (5) is connected to the outer wall of the bidirectional threaded rod (2) by threads. A sleeve (6) is fixedly installed on one side of the fixing plate (5), and a blocking airbag (7) is fixedly connected to the inner wall of the sleeve (6). A pressure ring (8) is fixedly connected to the inside of the blocking airbag (7), and a plurality of air holes (9) are opened inside the pressure ring (8). A connecting pipe (10) is fixedly connected to one side of the blocking airbag (7), and one end of the connecting pipe (10) is connected to an annular airbag (11).

2. The gas turbine air tightness detection tooling equipment according to claim 1, characterized in that: One side of the annular airbag (11) is fixedly connected to the inside of the fixing plate (5), and a spring (12) is fixedly installed inside the annular airbag (11).

3. The gas turbine air tightness detection tooling equipment according to claim 2 is characterized in that: A pressure plate (13) is fixedly connected to one side of the annular airbag (11), the pressure plate (13) is sleeved on the outer wall of the connecting pipe (10), and the pressure plate (13) is slidably connected to the inside of the fixed plate (5).

4. The gas turbine air tightness detection tooling equipment according to claim 3 is characterized in that: The interior of the fixing plate (5) is fixedly connected with a cylinder (14), the cylinder (14) is inserted into the interior of the annular airbag (11), and the blocking airbag (7) is fixedly connected to the outer wall of the cylinder (14).

5. The gas turbine air tightness detection tooling equipment according to claim 4 is characterized in that: The outer wall of the cylinder (14) is connected to an air pipe (15), and the air pipe (15) is inserted into the interior of the fixing plate (5).

6. The gas turbine air tightness detection tooling equipment according to claim 5 is characterized in that: One end of the air pipe (15) is fixedly connected to a gas generator (16), and the outer wall of the guide rod (4) is provided with a limit plate (17), and the limit plate (17) is slidably connected to the inside of the fixed plate (5).

7. The gas turbine air tightness detection tooling equipment according to claim 6 is characterized in that: The top of the limiting plate (17) is rotatably connected to a threaded rod (18), and the threaded rod (18) is threadably connected to the inside of the fixing plate (5), and the top of the supporting frame (1) is fixedly connected to a supporting block (19).

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