A micro gas turbine generator set testing device and its use method
By designing an automated micro-gas turbine generator set test device, the motor drive threaded rod and transmission rod are used to achieve automated support and testing of gas turbine generator sets of different specifications, solving the problem of inconvenient operation of existing devices and improving the efficiency and stability of the test.
Patent Information
- Application Number
- CN202510591824.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2025-05-09
- Publication Date
- 2025-08-12
- Estimated Expiration
- 2045-05-09
AI Technical Summary
The existing micro-gas turbine generator set testing device is inconvenient to operate, cannot be tested efficiently, conveniently and stably, and it is difficult to adapt to gas turbine generator sets of different specifications. The test process is cumbersome and easy to damage the equipment.
A micro-gas turbine generator set testing device is designed, including bottom plate, mounting plate, movable plate, spacing adjustment component, height adjustment component, multi-point support component and test component. Automatic adjustment is achieved through the motor drive threaded rod and transmission rod, and the flexible installation of support and test modules is adapted to different specifications of gas turbine generator sets.
Multi-position support and automated adjustment of micro-gas turbine generator sets are realized, which improves the versatility and stability of testing, simplifies the testing process, reduces the need for manual adjustments, and protects the test equipment.
Smart Images

Figure CN120101848B_ABST
Abstract
Description
Technical Field
[0001] The present invention belongs to the technical field of testing devices, and in particular relates to a testing device for a micro gas turbine generator set and a method for using the same. Background Art
[0002] Micro gas turbine generator sets have gradually become a hot spot for research and application due to their advantages such as small size, fast start-up, flexible operation and low emissions. In order to ensure the stable and safe use of micro gas turbine generator sets, testing operations are required before the micro gas turbine generator sets leave the factory.
[0003] The Chinese utility model patent application number is CN202121685549.0, which discloses a portable motor speed detection tooling that is easy to quickly support and fix. It includes a mounting plate, an adjustment mechanism is fixedly installed on the surface of the mounting plate, and a fixing mechanism is fixedly installed inside the adjustment mechanism. Two support legs are fixedly installed on one side of the surface of the mounting plate, and a detection platform is fixedly installed on the top of the two support legs. Through the provided fixing mechanism, the motor is placed on the fixed fixing ring, and the adjusting and rotating handle drives the screw rod to rotate accordingly. The rotation of the screw rod drives the threaded dynamic fixing ring to move up and down inside the slide groove to tighten the motor. An adjustment mechanism is provided to adjust the slider so that it slides on the sliding track, driving the second support column to approach or move away from one end of the first support column, and quick adjustment can be performed according to motors of different sizes.
[0004] The above-mentioned existing detection tooling of this type is suitable for detecting the rotational speed of the motor. By sliding the second support column of the adjustment mechanism, the distance between the second support column and the first support column is adjusted, and thus it is suitable for supporting and placing equipment to be detected of different lengths and sizes. Then, the dynamic fixing ring and the fixed fixing ring are used to clamp and fix the equipment to be detected, so as to achieve stable placement of the equipment to be detected. However, the overall degree of automation is low, and when clamping the equipment to be detected with a complex shape, the clamping operation is inconvenient, the scope of use is small, and it cannot perform fixed detection on gas turbine generators of various specifications, which reduces the use effect.
[0005] Moreover, when conducting test operations, traditional test devices for micro gas turbine generator sets require manual continuous adjustment of the test devices, and even require specially processed suitable positioning parts to achieve fixed operations before testing the micro gas turbine generator sets, resulting in a cumbersome and inefficient test process. Moreover, due to different test items, the data collection location for the micro gas turbine generator will also be different. In traditional technologies, testers are required to move the test equipment, which not only increases the labor intensity of the test but also easily causes damage to the test equipment, which is not conducive to the normal progress of the test operation. Summary of the Invention
[0006] The technical problem to be solved by the present invention is to provide a micro gas turbine generator set testing device and a method of using the same, so as to solve the problem that the existing testing device is inconvenient to operate and cannot perform efficient, convenient and stable testing operations on the micro gas turbine generator set.
[0007] In order to solve the above technical problems, the present invention provides the following technical solutions:
[0008] A micro gas turbine generator set test device includes a base plate, a plurality of mounting plates are slidably connected to the base plate, two movable plates are symmetrically slidably connected to each mounting plate, a spacing adjustment component is provided between the two movable plates, a fixed shell is fixedly connected to the movable plate, a vertical plate is slidably connected in the fixed shell, and height adjustment components for adjusting the height position of the vertical plates are provided in both fixed shells, the upper ends of the vertical plates extend above the fixed shell and are installed with multi-point support components, and the multiple multi-point support components on the left and right sides work together to support and place the gas turbine generator set to be tested, a displacement component for adjusting the position of the mounting plate is provided between the mounting plate and the base plate, a movable frame is slidably connected to the base plate, and a test component is movably provided on the movable frame.
[0009] The following is a further optimization of the above technical solution by the present invention:
[0010] The height adjustment assembly includes a second threaded rod, and a threaded hole is vertically opened in the middle of the vertical plate. The second threaded rod is threadedly connected in the threaded hole. The bottom end of the second threaded rod is rotatably connected to the corresponding movable plate. The rotation of the second threaded rod drives the vertical plate to move up and down through the threaded cooperation.
[0011] Further optimization: transmission rods are rotatably installed in the two fixed shells, the transmission rods and the second threaded rods are arranged vertically, and the ends of the two transmission rods close to each other slide and are transmission connected; the transmission rods are transmission connected to the second threaded rod, and when the two movable plates move relative to each other, the two transmission rods are driven to extend and retract, and the rotation of the transmission rods is used to drive the second threaded rod to rotate.
[0012] Further optimization: the spacing adjustment assembly includes a first threaded rod, which is rotatably mounted on the mounting plate, and two connecting blocks are threadedly connected to the first threaded rod, and the connecting blocks are fixedly connected to the corresponding movable plates. One end of the first threaded rod is transmission-connected to a first motor, and the first motor is started to drive the first threaded rod to rotate, so as to drive the two connecting blocks and the two movable plates to move closer to or away from each other.
[0013] Further optimization: The multi-point support assembly includes a support plate, which is fixedly installed on the top surface of the vertical plate. The support plate is in the shape of an arc plate, and a number of through holes are evenly distributed on the side wall of the support plate. Automatic telescopic rods are provided in the through holes, and the telescopic ends of the automatic telescopic rods extend to the inner side of the support plate and are fixedly connected to the positioning plate.
[0014] Further optimization: the displacement assembly includes a third motor fixedly mounted on the mounting plate, the power output end of the third motor is connected to a gear, a rack is fixedly mounted on the top surface of the base plate, the rack is arranged along the direction of movement of the mounting plate, and the gear is meshed with the rack.
[0015] Further optimization: the movable frame is an arc-shaped frame, and a sliding slot is provided on the movable frame. The test assembly includes a mounting shell movably arranged in the sliding slot, and connecting plates are fixedly installed on both sides of the mounting shell, and the connecting plates are slidingly connected to the movable frame respectively. A fixed frame is installed in the mounting shell, and a detection module is installed on the fixed frame.
[0016] Further optimization: a connecting groove is opened on the end of any transmission rod away from the fixed shell, a connecting rod is slidably and transmission-connected in the connecting groove, and the end of the connecting rod away from the connecting groove is coaxial with the other transmission rod and fixedly connected.
[0017] Further optimization: the spacing adjustment component includes a bidirectional automatic telescopic rod fixedly mounted on the mounting plate, and the two telescopic ends of the bidirectional automatic telescopic rod are respectively fixedly connected to the corresponding movable plates;
[0018] The displacement assembly includes a displacement box fixedly mounted at a middle position on one side of the mounting plate, with a through hole formed on the displacement box; a movable worm gear is rotatably mounted inside the displacement box, the movable worm gear and the through hole being coaxially arranged; a third motor is fixedly mounted on the outer surface of the displacement box, and a driving worm is connected to the power output end of the third motor in a transmission manner, and the driving worm is meshed with the movable worm gear;
[0019] A threaded drive hole is coaxially opened in the middle of the movable worm wheel, a mounting groove is opened at the center position of the top surface of the bottom plate, a movable threaded rod is fixedly installed in the middle of the mounting groove, and the threaded drive hole of the movable worm wheel is threadedly connected to the movable threaded rod.
[0020] The present invention also provides a method for using a micro gas turbine generator set test device, based on the above-mentioned micro gas turbine generator set test device, comprising the following steps:
[0021] S1: First, the test device is adaptively adjusted according to the specifications of the micro gas turbine generator to be tested, and a suitable number of mounting plates are slid onto the top surface of the base plate. Then, the displacement assembly is activated to drive the mounting plates to move on the base plate to a position suitable for supporting the micro gas turbine generator.
[0022] S2: Start the spacing adjustment component to adjust the spacing between the two movable plates to meet the width requirement of the micro gas turbine generator, and then start the height adjustment component to adjust the height of the vertical plate to meet the support height requirement of the micro gas turbine generator;
[0023] S3: The micro gas turbine generator to be tested is placed between the support plates using an external lifting device. Then, according to actual needs, the automatic telescopic rod at the designated position is activated. The automatic telescopic rod drives the positioning plate to move and connect to the outer wall of the micro gas turbine generator, thereby achieving multi-point support operation for the micro gas turbine generator.
[0024] S4: Installing a detection module for testing the micro gas turbine generator onto a fixed frame in the mounting shell, then pushing the mounting shell, causing the connecting plate to slide on the movable frame, so that the mounting shell drives the detection module to move to a designated position corresponding to the micro gas turbine generator, and then locking the mounting shell in place;
[0025] S5: Connecting the input end of the detection module to the micro gas turbine generator, connecting the output end of the detection module to the external data acquisition device, starting the micro gas turbine generator, and operating the micro gas turbine generator to a specified operating condition. The detection module is started to collect operating data of the micro gas turbine generator under the specified operating condition and transmit the data to the external data acquisition device.
[0026] S6: After completing the test data collection of the micro gas turbine generator, the operator further analyzes and processes the data of the micro gas turbine generator, and then removes the micro gas turbine generator from the test device.
[0027] The present invention adopts the above technical solution, which has at least the following beneficial effects:
[0028] 1. The present invention can realize multi-position support operation of the micro gas turbine generator by setting multiple mounting plates, and the positions of the multiple support plates can be adjusted by using the cooperation of the height adjustment component and the spacing adjustment component. In addition, the multiple support plates on the left and right sides are used to accurately support micro gas turbine generators of different models. The multi-point support component is then used to perform multi-point support operation on the micro gas turbine generator, realizing automatic adjustment operation, and effectively improving the versatility and stability of the test device for testing micro gas turbine generators.
[0029] 2. The present invention installs the detection module inside the installation shell and installs the installation shell on the movable frame. During the test operation, the installation shell can be used to protect the detection module and centrally process the lines. By utilizing the movement of the movable frame, it is convenient to perform test operations of different projects at different positions of the micro gas turbine generator, facilitate the collection of test data, and improve the use effect.
[0030] The present invention will be further described below with reference to the accompanying drawings and examples. BRIEF DESCRIPTION OF THE DRAWINGS
[0031] Figure 1 This is a three-dimensional diagram of the overall structure of Example 1 of the present invention;
[0032] Figure 2 This is a schematic diagram of the three-dimensional structure at the location of the mounting plate in Example 1 of the present invention;
[0033] Figure 3 This is a schematic diagram of the cross-sectional three-dimensional structure of the mounting plate in Example 1 of the present invention;
[0034] Figure 4 Schematic diagram of the structure of the height adjustment assembly in Example 1 of the present invention;
[0035] Figure 5 Schematic diagram of the structure of the multi-point support assembly in Example 1 of the present invention;
[0036] Figure 6 Schematic diagram of the structure of the displacement assembly in Example 1 of the present invention;
[0037] Figure 7 Schematic diagram of the structure of the test assembly in Example 1 of the present invention;
[0038] Figure 8 Schematic diagram of the structure of the height adjustment assembly in Example 2 of the present invention;
[0039] Figure 9 This is a schematic structural diagram of the spacing adjustment assembly in Example 3 of the present invention;
[0040] Figure 10 Schematic diagram of the structure of the displacement assembly in Example 3 of the present invention.
[0041] In the figure: 1-base plate; 2-mounting plate; 3-movable plate; 4-spacing adjustment assembly; 5-fixed shell; 6-vertical plate; 7-height adjustment assembly; 8-multi-point support assembly; 9-displacement assembly; 10-movable frame; 11-test assembly; 12-side plate; 13-first threaded rod; 14-first motor; 15-connecting block; 16-second threaded rod; 17-worm; 18-second motor; 19-worm gear; 20-support plate; 21-top automatic telescopic rod; 22-positioning plate; 23-bracket; 24-fixed plate; 25 -rotating shaft; 26-third motor; 27-gear; 28-rack; 29-connecting plate; 30-positioning bolt; 31-mounting shell; 32-fixing frame; 33-detection module; 34-slide rail; 35-slide groove; 36-connecting groove; 37-connecting rod; 38-transmission rod; 39-sliding through groove; 40-lifting automatic telescopic rod; 41-two-way automatic telescopic rod; 42-displacement box; 43-through hole; 44-moving worm wheel; 45-driving worm; 46-threaded drive hole; 47-mounting groove; 48-moving threaded rod. DETAILED DESCRIPTION
[0042] Example 1: Figure 1-7 As shown, a micro gas turbine generator set test device includes a base plate 1, a plurality of mounting plates 2 are slidably connected to the base plate 1, two movable plates 3 are symmetrically slidably connected to each mounting plate 2, a spacing adjustment component 4 is provided between the two movable plates 3, a fixed shell 5 is fixedly connected to the movable plate 3, a vertical plate 6 is slidably connected in the fixed shell 5, and a height adjustment component 7 for adjusting the height position of the vertical plate 6 is provided in each of the two fixed shells 5. The upper end of the vertical plate 6 extends to the top of the fixed shell 5 and is installed with a multi-point support component 8. The multiple multi-point support components 8 on the left and right sides work together to support and place the gas turbine generator set to be tested, a displacement component 9 for adjusting the position of the mounting plate 2 is provided between the mounting plate 2 and the base plate 1, a movable frame 10 is slidably connected to the base plate 1, and a test component 11 is movably provided on the movable frame 10.
[0043] like Figure 2-4 As shown, the spacing adjustment assembly 4 includes a first threaded rod 13, which is arranged along the moving direction of the two movable plates 3. The two ends of the first threaded rod 13 are rotatably connected to the side plates 12, and the two side plates 12 are fixedly mounted on the top surface of the mounting plate 2. The first threaded rod 13 is rotatably mounted on the mounting plate 2 through the two side plates 12, which is convenient for assembly and installation.
[0044] The first threaded rod 13 is provided with two threaded sections symmetrically arranged on the center, and the thread rotation directions of the two threaded sections are opposite. The two threaded sections of the first threaded rod 13 are respectively threadedly connected to the connecting blocks 15. The first threaded rod 13 rotates through the two threaded sections to drive the two connecting blocks 15 to move towards or away from each other.
[0045] One end of the first threaded rod 13 is transmission-connected to a first motor 14, which is fixedly mounted on the corresponding side plate 12. The first motor 14 is started to drive the first threaded rod 13 to rotate, and the rotation of the first threaded rod 13 drives the two connecting blocks 15 and the two movable plates 3 to move toward or away from each other.
[0046] With this design, when it is necessary to adjust the distance between the two movable plates 3, the first motor 14 is started to drive the first threaded rod 13 to rotate. The rotation of the first threaded rod 13 drives the two connecting blocks 15 to move through the threaded cooperation. At this time, the two connecting blocks 15 drive the two movable plates 3 to move on the mounting plate 2, thereby realizing the adjustment operation of the distance between the two movable plates 3.
[0047] In addition to this embodiment 1, the first motor 14 can also be fixedly mounted on the mounting plate 2, and the power output end of the first motor 14 is connected to the first threaded rod 13 through a transmission box. When the first motor 14 is started, the transmission action of the transmission box drives the first threaded rod 13 to rotate.
[0048] like Figure 3-4 As shown, the height adjustment assembly 7 includes a second threaded rod 16, and a threaded hole is vertically opened in the middle of the vertical plate 6. The second threaded rod 16 is threadedly connected in the threaded hole. The bottom end of the second threaded rod 16 is rotatably connected to the corresponding movable plate 3. The rotation of the second threaded rod 16 drives the vertical plate 6 to move up and down through the threaded cooperation.
[0049] In this embodiment 1, the bottom end of the second threaded rod 16 is rotatably connected to the corresponding movable plate 3 via a bearing seat, and the bearing seat is used to support the second threaded rod 16 for rotation.
[0050] A transmission rod 38 is rotatably installed in each of the two fixed shells 5. The transmission rod 38 and the second threaded rod 16 are arranged vertically. The transmission rod 38 is transmission-connected to the second threaded rod 16. The rotation of the transmission rod 38 is used to drive the second threaded rod 16 to rotate.
[0051] In this embodiment 1, a worm 17 is integrally connected to the transmission rod 38 at a position inside the fixed housing 5 , and a worm wheel 19 is fixedly connected to the bottom end of the second threaded rod 16 , and the worm wheel 19 is meshed with the corresponding worm 17 .
[0052] The transmission rod 38 rotates to drive the worm 17 to rotate, and the worm 17 is meshed and connected with the worm wheel 19, thereby driving the second threaded rod 16 to rotate.
[0053] In this embodiment 1, a second motor 18 is fixedly mounted on any one of the fixed shells 5 or the movable plate 3 , and a power output end of the second motor 18 is transmission-connected to a corresponding transmission rod 38 , and the second motor 18 is started to drive the transmission rod 38 to rotate.
[0054] The two transmission rods 38 are slidably connected at one end thereof that is close to each other; when the two movable plates 3 move relative to each other, the two transmission rods 38 are driven to extend and retract.
[0055] In this embodiment 1, a connecting groove 36 is formed on the end of any one of the transmission rods 38 away from the fixed shell 5, and a connecting rod 37 is slidably and transmission-connected in the connecting groove 36, and the end of the connecting rod 37 away from the connecting groove 36 is coaxial and fixedly connected to the other transmission rod 38.
[0056] In this embodiment 1, the cross-sections of the connecting rod 37 and the connecting groove 36 are both set to be regular hexagons, and the connecting rod 37 is movably inserted into the connecting groove 36 to achieve sliding and transmission connection between the connecting groove 36 and the connecting rod 37.
[0057] With this design, when the height position of the vertical plate 6 needs to be adjusted, the second motor 18 is started, and the second motor 18 drives the corresponding transmission rod 38 to rotate, and drives another transmission rod 38 to rotate through the cooperation of the connecting rod 37 and the connecting groove 36. At this time, the two transmission rods 38 rotate through the engagement transmission of the worm 17 and the worm wheel 19 to drive the second threaded rod 16 to rotate. The second threaded rod 16 is threadedly connected to the threaded hole. The rotation of the second threaded rod 16 drives the vertical plate 6 to move up and down in the fixed shell 5, thereby adjusting the height position of the vertical plate 6 and improving the use effect.
[0058] In addition to this embodiment 1, the worm 17 and the worm wheel 19 can also be replaced by a helical gear set or a bevel gear set. The following is a specific description taking the helical gear set as an example: the helical gear set includes two helical gears, the axes of the helical gears are arranged vertically, one of the helical gears is coaxial and fixedly mounted on the transmission rod 38, and the other helical gear is coaxial and fixedly mounted on the second threaded rod 16, and the two helical gears are meshed and connected. The rotation of the transmission rod 38 is transmitted through the meshing of the two helical gears to drive the second threaded rod 16 to rotate, and the helical gears are existing technology and can be purchased directly on the market.
[0059] like Figure 5 As shown, the multi-point support assembly 8 includes a support plate 20, which is fixedly installed on the top surface of the vertical plate 6. The support plate 20 is in the shape of an arc plate, and a number of through holes are evenly distributed on the side wall of the support plate 20. A top-connected automatic telescopic rod 21 is provided in each of the through holes. The telescopic end of the top-connected automatic telescopic rod 21 extends to the inner side of the support plate 20 and is fixedly connected to a positioning plate 22.
[0060] In this embodiment 1, a bracket 23 is fixedly connected to the mounting end of the top-connected automatic telescopic rod 21, and the bracket 23 is fixedly mounted on the back of the support plate 20. The telescopic end of the top-connected automatic telescopic rod 21 is slidably connected to the inner surface of the through hole.
[0061] With this design, when in use, the micro gas turbine generator to be tested can be placed between the support plates 20 through external lifting equipment, so that the support plates 20 are used to support and place the micro gas turbine generator, and the automatic telescopic rod 21 at the designated position is started according to actual needs. The automatic telescopic rod 21 drives the positioning plate 22 to move, so that the positioning plate 22 is connected to the outer wall of the micro gas turbine generator, thereby realizing multi-point support operation of the micro gas turbine generator, effectively improving the stability during support and reducing the impact on the equipment.
[0062] In this embodiment 1, the top-connected automatic telescopic rod 21 adopts one of an electric telescopic rod, a hydraulic cylinder, and a telescopic cylinder.
[0063] like Figure 7 As shown, the movable frame 10 is an arc-shaped frame, and a sliding slot 39 is provided on the movable frame 10. The test assembly 11 includes a mounting shell 31 movably arranged in the sliding slot 39. Connecting plates 29 are fixedly installed on both sides of the mounting shell 31, and the connecting plates 29 are respectively slidably connected to the movable frame 10. A fixed frame 32 is installed in the mounting shell 31, and a detection module 33 is installed on the fixed frame 32.
[0064] In this embodiment 1, the overall structure of the connecting plate 29 is an L-shaped plate, and arc-shaped sliding grooves are respectively provided on both sides of the sliding groove 39 on the outer surface of the movable frame 10. Sliding blocks are slidably connected in the arc-shaped sliding grooves, and the sliding blocks are fixedly connected to the corresponding connecting plates 29.
[0065] With this design, the connecting plate 29 is slidably installed on the outer surface of the movable frame 10 through the cooperation of the arc-shaped slide groove and the sliding block, which is convenient for assembly and installation. In addition, the cooperation of the arc-shaped slide groove and the sliding block can also guide the movement of the connecting plate 29, thereby improving the use effect.
[0066] In the first embodiment, positioning bolts 30 are respectively threadedly connected on the side surfaces of the two connecting plates 29 that are away from each other.
[0067] With this design, when the positioning bolt 30 is rotated to move it toward the movable frame 10, the end of the positioning bolt 30 close to the movable frame 10 contacts the outer side surface of the movable frame 10, thereby positioning the connecting plate 29 on the movable frame 10, and positioning the mounting shell 31 and the detection module 33, which is convenient for use.
[0068] In this embodiment 1, when it is necessary to perform an exhaust test operation on the micro gas turbine generator, the detection module 33 can adopt a gas composition collection sensor. The gas composition collection sensor is an existing technology and can be directly purchased on the market. During the detection operation, the detection module 33 with the gas composition collection sensor is first fixedly installed on the fixed frame 32, and then the connecting plates 29 on both sides of the mounting shell 31 are slidably installed on the movable frame 10. By pushing the mounting shell 31, the connecting plates 29 slide on the movable frame 10, so that the mounting shell 31 drives the detection module 33 to move to the specified position corresponding to the micro gas turbine generator. After the position adjustment of the mounting shell 31 is completed, the positioning bolt 30 is rotated so that the end of the positioning bolt 30 close to the movable frame 10 is in contact with the outer side surface of the movable frame 10, thereby realizing the positioning of the connecting plate 29 on the movable frame 10, and then realizing the positioning of the mounting shell 31 and the detection module 33, which is convenient for use.
[0069] Then, pipes are installed on both ends of the mounting shell 31, one pipe is connected to the exhaust end of the micro gas turbine generator, and the other pipe is connected to the external gas processing equipment. Then, the micro gas turbine generator is operated to the specified working condition, and the gas composition acquisition sensor in the detection module 33 is started. At this time, the gas composition acquisition sensor collects data on the exhaust gas composition, and the detection module 33 transmits the gas composition data to the external data acquisition equipment based on wired or wireless signal transmission. At this time, the external data acquisition equipment is used to implement the exhaust test operation of the micro gas turbine generator, which is convenient to use.
[0070] In addition to the present embodiment 1, the detection module 33 may adopt a temperature acquisition sensor, a pressure acquisition sensor, a power generation collector, etc.; the temperature acquisition sensor is used to detect the temperature of the micro gas turbine generator during operation; the pressure acquisition sensor is used to detect the pressure data of the exhaust end of the micro gas turbine generator during operation; the power generation collector is used to detect the power generation of the micro gas turbine generator during operation; the temperature acquisition sensor, the pressure acquisition sensor, and the power generation collector are all existing technologies and can be directly purchased on the market.
[0071] like Figure 1-2 and Figure 6 The displacement assembly 9 includes a third motor 26 fixedly mounted on the mounting plate 2, the power output end of the third motor 26 is transmission-connected to a gear 27, a rack 28 is fixedly mounted on the top surface of the base plate 1, the rack 28 is arranged along the direction of movement of the mounting plate 2, and the gear 27 is meshed with the rack 28.
[0072] In this embodiment 1, a rotating shaft 25 is coaxially and fixedly installed on the gear 27, and both ends of the rotating shaft 25 are rotatably connected to fixed plates 24. The two fixed plates 24 are symmetrically arranged and fixedly installed on the side walls of the mounting plate 2. The fixed plates 24 and the rotating shaft 25 are used to support the gear 27 for rotation.
[0073] In this embodiment 1, the power output end of the third motor 26 is in transmission connection with the rotating shaft 25 , and the third motor 26 is started to drive the rotating shaft 25 to drive the gear 27 to rotate.
[0074] With this design, in order to meet the stable testing requirements of micro gas turbine generators of different specifications, an appropriate number of mounting plates 2 can be installed on the base plate 1, and the third motor 26 is used to drive the rotating shaft 25 to rotate. The gear 27 on the rotating shaft 25 engages and rotates with the rack 28 to realize the movement of the mounting plate 2 on the base plate 1, and then the mounting plate 2 can be moved to a position suitable for supporting the micro gas turbine generator, thereby completing the multi-position support operation.
[0075] In this embodiment 1, multiple slide rails 34 are symmetrically and fixedly installed on the top surface and front and rear side walls of the base plate 1, and slide rails 34 are also fixedly installed on the left and right side walls of the mounting plate 2. Multiple slide grooves 35 are provided on the bottom surface of the mounting plate 2 and the front and rear inner walls of the movable frame 10, and slide grooves 35 are also provided on the left and right side walls of the movable plate 3. The slide rails 34 are slidably connected to the corresponding slide grooves 35.
[0076] In this embodiment 1, the mounting plate 2 is slidably connected to the slide rail 34 on the top surface of the base plate 1 through the slide groove 35 on the bottom surface, so that the mounting plate 2 can be slidably installed on the base plate 1, which is convenient for assembly and installation.
[0077] In this embodiment 1, the movable frame 10 is slidably connected to the slide rails 34 on the front and rear side walls of the base plate 1 through the slide grooves 35 on the front and rear inner side walls, so that the movable frame 10 can be slidably installed on the base plate 1, which is convenient for assembly and installation.
[0078] In this embodiment 1, the movable panel 3 is slidably connected to the slide rails 34 on the left and right side walls of the mounting plate 2 through the slide grooves 35 on the left and right side walls, so that the movable panel 3 can be slidably mounted on the mounting plate 2, which is convenient for assembly and installation.
[0079] In this embodiment 1, the sliding connection between the slide groove 35 and the corresponding slide rail 34 can also be used to support the mounting plate 2, the movable plate 3 and the movable frame 10 to perform stable movement, thereby improving the support stability and versatility of the test device for the micro gas turbine generator.
[0080] The present invention also provides a method for using a micro gas turbine generator set test device, based on the above-mentioned micro gas turbine generator set test device, comprising the following steps:
[0081] S1: First, the specification data of the micro gas turbine generator to be tested is collected, and then the test device is adaptively adjusted according to the collected data. An appropriate number of mounting plates 2 are slid onto the top surface of the base plate 1, and then the displacement assembly 9 is started to drive the mounting plates 2 to move on the base plate 1 to a position suitable for the support of the micro gas turbine generator.
[0082] In step S1, the working process of the displacement component 9 is: start the third motor 26, the third motor 26 drives the gear 27 to rotate through the rotating shaft 25, the gear 27 engages with the rack 28, and the mounting plate 2 moves on the base plate 1, so as to move the mounting plate 2 to a position suitable for the support of the micro gas turbine generator. After the adjustment is completed, the operation of the third motor 26 is turned off.
[0083] S2: Start the spacing adjustment component 4 to adjust the spacing between the two movable plates 3 to adapt to the width requirement of the micro gas turbine generator, and then start the height adjustment component 7 to adjust the height of the vertical plate 6 to adapt to the support height requirement of the micro gas turbine generator.
[0084] In step S2, the working process of the spacing adjustment component 4 is: start the first motor 14 to drive the first threaded rod 13 to rotate, the first threaded rod 13 engages the connecting block 15 to move, and the connecting block 15 drives the movable plate 3 to move on the mounting plate 2 to realize the adjustment operation of the spacing between the two movable plates 3.
[0085] In step S2, the working process of the height adjustment component 7 is: start the second motor 18 to drive the corresponding transmission rod 38 to rotate, and drive the other transmission rod 38 to rotate synchronously through the cooperation of the connecting rod 37 and the connecting groove 36. The rotation of the two transmission rods 38 drives the second threaded rod 16 to rotate through the transmission action of the worm 17 engaging the worm wheel 19. The second threaded rod 16 is threadedly connected to the threaded hole, so that the vertical plate 6 extends to a suitable height of the fixed shell 5, thereby realizing the height adjustment operation of the vertical plate 6.
[0086] S3: The micro gas turbine generator to be tested is placed between the support plates 20 by means of an external lifting device, so that the support plates 20 are used to support and place the micro gas turbine generator. Then, according to actual needs, the automatic telescopic rod 21 at the designated position is started, and the automatic telescopic rod 21 drives the positioning plate 22 to move, so that the positioning plate 22 is tightly pressed against the outer wall of the micro gas turbine generator, thereby realizing multi-point support operation for the micro gas turbine generator, effectively improving the stability during support placement and reducing the impact on the equipment.
[0087] S4: Install the detection module 33 used to test the micro gas turbine generator on the fixed frame 32 in the mounting shell 31, then push the mounting shell 31, and slide the connecting plate 29 on the movable frame 10, so that the mounting shell 31 drives the detection module 33 to move to the designated position corresponding to the micro gas turbine generator, and then lock the position of the mounting shell 31.
[0088] In step S4, the positioning bolt 30 is rotated so that one end of the positioning bolt 30 close to the movable frame 10 is in contact with the outer side surface of the movable frame 10, thereby positioning the position of the connecting plate 29 on the movable frame 10, and then locking and positioning the positions of the mounting shell 31 and the detection module 33 for easy use.
[0089] S5: Connect the input end of the detection module 33 to the micro gas turbine generator, connect the output end of the detection module 33 to the external data acquisition device, start the micro gas turbine generator, and make the micro gas turbine generator run under the specified working conditions. Start the detection module 33 to collect the operating data of the micro gas turbine generator under the specified working conditions and transmit the data to the external data acquisition device.
[0090] In steps S4-S5, the detection module 33 may adopt a gas composition acquisition sensor. The detection module 33 with the gas composition acquisition sensor is fixedly mounted on the fixing frame 32. Pipes are respectively installed at both ends of the mounting shell 31. One pipe is connected to the exhaust end of the micro gas turbine generator, and the other pipe is connected to the external gas processing equipment. Then, the micro gas turbine generator is operated to the specified working condition, and the gas composition acquisition sensor in the detection module 33 is started. At this time, the gas composition acquisition sensor collects data on the exhaust gas composition, and the detection module 33 transmits the gas composition data to the external equipment based on wired or wireless signal transmission. At this time, the external equipment is used to perform the exhaust test operation on the micro gas turbine generator, which is convenient to use.
[0091] S6: After completing the test data collection of the micro gas turbine generator, the micro gas turbine generator and the detection module 33 are turned off, and the operator further analyzes and processes the data of the micro gas turbine generator to perform the test operation of the micro gas turbine generator, and then removes the micro gas turbine generator from the test device.
[0092] Example 2: Please refer to Figure 8As shown, based on the above-mentioned embodiment 1, in this embodiment 2, the height adjustment component 7 can also adopt an automatic lifting telescopic rod 40, which is vertically arranged in the fixed shell 5, and the fixed end of the automatic lifting telescopic rod 40 is fixedly installed on the movable plate 3, and the telescopic end of the automatic lifting telescopic rod 40 is fixedly connected to the bottom end surface of the vertical plate 6. The automatic lifting telescopic rod 40 is used to drive the vertical plate 6 to move up and down in the fixed shell 5.
[0093] In this embodiment 2, the automatic telescopic rod 40 is an electric telescopic rod, a hydraulic cylinder, or a telescopic cylinder.
[0094] Example 3: Please refer to Figure 9-10 As shown, based on the above-mentioned embodiment 1, in this embodiment 3, the spacing adjustment component 4 can also adopt a bidirectional automatic telescopic rod 41; the bidirectional automatic telescopic rod 41 is arranged between the two movable plates 3, and the middle part of the bidirectional automatic telescopic rod 41 is fixedly mounted on the mounting plate 2 using a mounting frame, and the bidirectional automatic telescopic rod 41 and the transmission rod 38 are arranged in parallel. The bidirectional automatic telescopic rod 41 has two telescopic ends, and the two telescopic ends are respectively fixedly connected to the corresponding movable plates 3.
[0095] The two telescopic ends of the bidirectional automatic telescopic rod 41 are used to drive the two movable plates 3 to move toward or away from each other, thereby adjusting the distance between the two movable plates 3 for easy use.
[0096] When the two movable plates 3 move, the connecting rod 37 moves axially in the connecting groove 36, so that the two transmission rods 38 can adapt to the distance between the two movable plates 3, and the cooperation between the connecting rod 37 and the connecting groove 36 can ensure that the two transmission rods 38 are connected in transmission, which is convenient to use.
[0097] In this embodiment 3, the bidirectional automatic telescopic rod 41 adopts one of an electric bidirectional telescopic rod, a hydraulic bidirectional oil cylinder, and a bidirectional telescopic cylinder.
[0098] In this embodiment 3, the displacement component 9 is also Figure 9-10 In the structure shown, the displacement assembly 9 includes a displacement box 42 , which is fixedly mounted at a middle position on one side of the mounting plate 2 , and a through hole 43 is formed on the displacement box 42 .
[0099] A movable worm gear 44 is rotatably installed inside the displacement box 42. The movable worm gear 44 and the through hole 43 are coaxially arranged. A driving worm 45 is meshed and connected above the movable worm gear 44. Both ends of the driving worm 45 are rotatably installed on the inner wall of the displacement box 42. The third motor 26 is fixedly installed on the outer surface of the displacement box 42, and the power output end of the third motor 26 is transmission-connected to the driving worm 45.
[0100] In this embodiment 3, the axis of the movable worm gear 44 is arranged parallel to the moving direction of the mounting plate 2 , and both sides of the movable worm gear 44 are rotatably mounted on the inner surface of the displacement box 42 using support bearings.
[0101] A threaded drive hole 46 is coaxially defined in the middle of the movable worm wheel 44 . The inner diameter of the threaded drive hole 46 is smaller than the inner diameter of the through hole 43 . An internal thread is defined on the inner surface of the threaded drive hole 46 .
[0102] A mounting groove 47 is provided at the center of the top surface of the base plate 1 . The mounting groove 47 is provided along the moving direction of the mounting plate 2 . A movable threaded rod 48 is fixedly installed in the middle of the mounting groove 47 .
[0103] During assembly, the mounting plate 2 is slidably connected to the slide rail 34 on the top surface of the base plate 1 through the slide groove 35 on the bottom surface, so that the mounting plate 2 can be slidably installed on the base plate 1, which is convenient for assembly and installation. The displacement box 42 is slidably arranged in the mounting groove 47, and the threaded drive hole 46 on the movable worm gear 44 is threadedly connected to the movable threaded rod 48.
[0104] When the mounting plate 2 needs to be moved, the third motor 26 is used to drive the driving worm 45 to rotate, and the driving worm 45 engages the moving worm wheel 44 to rotate. The threaded driving hole 46 in the middle of the moving worm wheel 44 is threadedly connected to the moving threaded rod 48. At this time, the mounting plate 2 can be driven to slide on the base plate 1 through the cooperation of the threads, which is convenient to use.
[0105] The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the principles of the present invention. These improvements and modifications should also be regarded as within the scope of protection of the present invention.
Claims
1. A micro gas turbine generator set test device, comprising a base plate (1), characterized in that: The bottom plate (1) is slidably connected to a plurality of mounting plates (2), and each mounting plate (2) is symmetrically slidably connected to two movable plates (3), a spacing adjustment component (4) is provided between the two movable plates (3), a fixed shell (5) is fixedly connected to the movable plate (3), a vertical plate (6) is slidably connected in the fixed shell (5), and a height adjustment component (7) for adjusting the height position of the vertical plate (6) is provided in each of the two fixed shells (5), the upper end of the vertical plate (6) extends above the fixed shell (5) and is provided with a multi-point support component (8), and the multiple multi-point support components (8) on the left and right sides cooperate to support and place the gas turbine generator set to be tested, a displacement component (9) for adjusting the position of the mounting plate (2) is provided between the mounting plate (2) and the bottom plate (1), a movable frame (10) is slidably connected to the bottom plate (1), and a test component (11) is movably provided on the movable frame (10); The multi-point support assembly (8) includes a support plate (20), the support plate (20) is fixedly mounted on the top surface of the vertical plate (6), the support plate (20) is in the shape of an arc plate, and a plurality of automatic telescopic rods (21) are evenly distributed and fixedly mounted on the side wall of the support plate (20), the telescopic ends of the top-connected automatic telescopic rods (21) extend to the inner side of the support plate (20) and are fixedly connected to a positioning plate (22), and the plurality of positioning plates (22) are arranged in an arc shape at intervals; The movable frame (10) is an arc-shaped frame, and a sliding slot (39) is provided on the movable frame (10). The test assembly (11) includes a mounting shell (31) movably arranged in the sliding slot (39), and connecting plates (29) are fixedly installed on both sides of the mounting shell (31). The connecting plates (29) are respectively slidably connected to the movable frame (10). A fixing frame (32) is installed in the mounting shell (31), and a detection module (33) is installed on the fixing frame (32). The mounting shell (31) slides on the movable frame (10) via the connecting plate (29), so that the mounting shell (31) drives the detection module (33) to move to a designated position corresponding to the micro gas turbine generator.
2. A micro gas turbine generator set testing device according to claim 1, characterized in that: The height adjustment assembly (7) includes a second threaded rod (16), a threaded hole is vertically opened in the middle of each vertical plate (6), the second threaded rod (16) is threadedly connected in the threaded hole, the bottom end of the second threaded rod (16) is rotatably connected to the corresponding movable plate (3), and the second threaded rod (16) rotates and drives the vertical plate (6) to move up and down through the threaded engagement.
3. A micro gas turbine generator set testing device according to claim 2, characterized in that: A transmission rod (38) is rotatably installed in each of the two fixed shells (5). The transmission rod (38) and the second threaded rod (16) are arranged vertically. The ends of the two transmission rods (38) that are close to each other slide and are transmission-connected. The transmission rod (38) is transmission-connected to the second threaded rod (16). When the two movable plates (3) move relative to each other, the two transmission rods (38) are driven to extend and retract, and the rotation of the transmission rod (38) is used to drive the second threaded rod (16) to rotate.
4. A micro gas turbine generator set testing device according to claim 3, characterized in that: The spacing adjustment assembly (4) includes a first threaded rod (13), the first threaded rod (13) is rotatably mounted on the mounting plate (2), two connecting blocks (15) are threadedly connected to the first threaded rod (13), the connecting blocks (15) are fixedly connected to the corresponding movable plates (3), one end of the first threaded rod (13) is transmission-connected to a first motor (14), and the first motor (14) is started to drive the first threaded rod (13) to rotate, thereby driving the two connecting blocks (15) and the two movable plates (3) to move toward or away from each other.
5. A micro gas turbine generator set testing device according to claim 4, characterized in that: The displacement assembly (9) includes a third motor (26) fixedly mounted on the mounting plate (2), a gear (27) being transmission-connected to a power output end of the third motor (26), a rack (28) being fixedly mounted on the top surface of the base plate (1), the rack (28) being arranged along the moving direction of the mounting plate (2), and the gear (27) being meshedly connected to the rack (28).
6. A micro gas turbine generator set testing device according to claim 5, characterized in that: A connecting groove (36) is provided on one end of any one of the transmission rods (38) away from the fixed housing (5), and a connecting rod (37) is slidably and transmission-connected in the connecting groove (36), and an end of the connecting rod (37) away from the connecting groove (36) is coaxially and fixedly connected to the other transmission rod (38).
7. The micro gas turbine generator set testing device according to claim 1, characterized in that: The spacing adjustment assembly (4) comprises a bidirectional automatic telescopic rod (41) fixedly mounted on the mounting plate (2), wherein the two telescopic ends of the bidirectional automatic telescopic rod (41) are respectively fixedly connected to the corresponding movable plates (3); The displacement assembly (9) includes a displacement box (42) fixedly mounted at a middle position on one side of the mounting plate (2), and a through hole (43) is provided on the displacement box (42); a movable worm gear (44) is rotatably mounted inside the displacement box (42), and the movable worm gear (44) and the through hole (43) are coaxially arranged; a third motor (26) is fixedly mounted on the outer surface of the displacement box (42), and a driving worm (45) is transmission-connected to the power output end of the third motor (26), and the driving worm gear (45) is meshingly connected to the movable worm gear (44); A threaded drive hole (46) is coaxially opened in the middle of the movable worm wheel (44), a mounting groove (47) is opened at the center position of the top surface of the bottom plate (1), a movable threaded rod (48) is fixedly installed in the middle of the mounting groove (47), and the threaded drive hole (46) of the movable worm wheel (44) is threadedly connected to the movable threaded rod (48).
8. A method for using a micro gas turbine generator set test device, based on the micro gas turbine generator set test device according to claim 6, characterized in that: The following steps are involved: S1: First, the test device is adaptively adjusted according to the specification data of the micro gas turbine generator to be tested, and a suitable number of mounting plates (2) are slid onto the top surface of the base plate (1), and then the displacement assembly (9) is started to drive the mounting plates (2) to move on the base plate (1) to a position adapted to support the micro gas turbine generator; S2: starting the spacing adjustment component (4) to adjust the spacing between the two movable plates (3) to meet the width requirements of the micro gas turbine generator, and then starting the height adjustment component (7) to adjust the height of the vertical plate (6) to meet the support height requirements of the micro gas turbine generator; S3: The micro gas turbine generator to be tested is placed at a position between the support plates (20) by means of an external lifting device, and then the top-connected automatic telescopic rod (21) at the designated position is activated according to actual needs. The top-connected automatic telescopic rod (21) drives the positioning plate (22) to move and connect to the outer wall of the micro gas turbine generator, thereby realizing a multi-point support operation for the micro gas turbine generator; S4: Installing a detection module (33) for testing the micro gas turbine generator onto a fixed frame (32) in the mounting shell (31), then pushing the mounting shell (31), and sliding the connecting plate (29) on the movable frame (10), so that the mounting shell (31) drives the detection module (33) to move to a designated position corresponding to the micro gas turbine generator, and then locking the mounting shell (31) in position; S5: connecting the input end of the detection module (33) to the micro gas turbine generator, connecting the output end of the detection module (33) to the external data acquisition device, starting the micro gas turbine generator, and making the micro gas turbine generator run under the specified working condition, starting the detection module (33) to collect the operating data of the micro gas turbine generator under the specified working condition, and transmitting the data to the external data acquisition device; S6: After completing the test data collection of the micro gas turbine generator, the operator further analyzes and processes the data of the micro gas turbine generator, and then removes the micro gas turbine generator from the test device.
Citation Information
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Portable motor rotating speed detection tool convenient for rapid supporting and fixing
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