Air compressor rotor detection device
Patent Information
- Application Number
- CN202522709775.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-12-22
- Publication Date
- 2026-09-18
- Estimated Expiration
- 2035-12-22
AI Technical Summary
[0004]为了弥补以上不足,本实用新型提供了一种空压机转子检测装置,旨在解决现有技术中夹持装置结构复杂,装夹操作繁琐,需要人工多次调整才能确保转子轴线与旋转中心重合,导致检测准备时间长、效率低的问题
[0015] 1. In this utility model, the first and second support wheels arranged symmetrically in a V-shape in the support mechanism, together with the pressure wheel driven by the first hydraulic cylinder, simplify the complex structure of the traditional clamp. Only the rotor shaft end needs to be placed between the V-shaped wheels, and the hydraulic drive can automatically complete the clamping and positioning. The self-centering characteristic of the V-shaped structure makes the rotor axis automatically coincide with the rotation center, eliminating the need for repeated manual adjustments, shortening the test preparation time and improving the test efficiency.
Smart Images

Figure CN224772982U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of rotor testing technology, and in particular to an air compressor rotor testing device. Background Technology
[0002] In existing technologies, flaw detection and testing of screw air compressor rotors mainly employs magnetic particle testing or ultrasonic testing. Ultrasonic testing can detect extremely small defects inside the screw air compressor rotor, such as cracks, pores, and inclusions. Generally, it can detect defects at the millimeter level or even smaller, which is crucial for the early detection of potential safety hazards in the rotor. At the same time, the propagation time and reflection position of ultrasonic waves in the rotor can accurately determine the location, depth, and size of defects. This helps maintenance personnel accurately assess the condition of defects and provides a reliable basis for subsequent repair or replacement work.
[0003] Currently, air compressor rotor flaw detection typically uses a rotatable special fixture to clamp and fix the rotor shaft end, and a motor drives the fixture to rotate the rotor, which in turn scans surface defects with the detection probe. However, existing clamping devices are complex in structure and cumbersome in operation, requiring multiple manual adjustments to ensure that the rotor axis coincides with the center of rotation, resulting in long preparation time and low efficiency. Therefore, an air compressor rotor detection device is proposed to solve the above problems. Utility Model Content
[0004] To overcome the above shortcomings, this utility model provides an air compressor rotor testing device, which aims to solve the problems of complex clamping device structure, cumbersome clamping operation, and the need for multiple manual adjustments to ensure that the rotor axis coincides with the rotation center in the existing technology, resulting in long test preparation time and low efficiency.
[0005] To achieve the above objectives, the present invention adopts the following technical solution: an air compressor rotor testing device, comprising a machine base, a support mechanism provided on the upper surface of the machine base, and a testing frame fixedly connected to the upper surface of the machine base;
[0006] The support mechanism includes a first support base, a first motor is provided on the right wall of the first support base, a first synchronous pulley is fixedly connected to the output end of the first motor, a first support wheel is rotatably connected to the inner wall of the first support base through a bearing, a second synchronous pulley is fixedly connected to the right end of the axle of the first support wheel, a synchronous belt is drivenly connected to the outer wall of the second synchronous pulley, the lower end of the synchronous belt is drivenly connected to the outer wall of the first synchronous pulley, and the second support wheel is rotatably connected to the inner wall of the first support base through a bearing.
[0007] A fixing frame is fixedly connected to the upper surface of the first support base, and a first hydraulic cylinder is fixedly connected to the inner wall of the fixing frame. A wheel frame is fixedly connected to the telescopic end of the first hydraulic cylinder.
[0008] As a further description of the above technical solution: the inner wall of the wheel frame is rotatably connected to a pressure wheel via a bearing, the right wall of the wheel frame is fixedly connected to a limiting plate, and the rear end of the limiting plate is slidably connected to the right wall of the fixed frame.
[0009] As a further description of the above technical solution: a second support base is fixedly connected to the left end of the upper surface of the machine base, a support plate is fixedly connected to the right wall of the first support base, and the bottom of the first motor is fixedly connected to the upper surface of the support plate.
[0010] As a further description of the above technical solution: a second motor is fixedly connected to the right wall of the testing frame, a lead screw is fixedly connected to the output end of the second motor, a movable seat is slidably connected to the inner wall of the testing frame, and the inner wall of the movable seat is threadedly connected to the outer wall of the lead screw.
[0011] As a further description of the above technical solution: a mounting bracket is fixedly connected to the front of the movable seat, and a detection probe is fixedly connected to the inner wall of the mounting bracket.
[0012] As a further description of the above technical solution: the upper surface of the machine tool is provided with an adjustment mechanism, the adjustment mechanism includes an adjustment groove, the adjustment groove is opened on the upper surface of the machine tool, and the upper surface of the machine tool is provided with an installation groove.
[0013] As a further description of the above technical solution: a guide rod is fixedly connected to the inner wall of the adjusting groove, an adjusting seat is slidably connected to the outer wall of the guide rod, the top of the adjusting seat is fixedly connected to the bottom of the first support seat, a second hydraulic cylinder is fixedly connected to the inner wall of the mounting groove, and the telescopic end of the second hydraulic cylinder is fixedly connected to the right wall of the adjusting seat.
[0014] This utility model has the following beneficial effects:
[0015] 1. In this utility model, the first and second support wheels arranged symmetrically in a V-shape in the support mechanism, together with the pressure wheel driven by the first hydraulic cylinder, simplify the complex structure of the traditional clamp. Only the rotor shaft end needs to be placed between the V-shaped wheels, and the hydraulic drive can automatically complete the clamping and positioning. The self-centering characteristic of the V-shaped structure makes the rotor axis automatically coincide with the rotation center, eliminating the need for repeated manual adjustments, shortening the test preparation time and improving the test efficiency.
[0016] 2. In this utility model, the adjustment seat is driven to slide along the guide rod by the second hydraulic cylinder in the adjustment mechanism, thereby realizing the automatic adjustment of the distance between the first support seat and the second support seat. This enables the detection device to be compatible with air compressor rotors of different lengths and improves the versatility of the equipment. Attached Figure Description
[0017] Figure 1 This is a front view of an air compressor rotor detection device proposed in this utility model;
[0018] Figure 2 This is a schematic diagram of the first support base structure of an air compressor rotor detection device proposed in this utility model;
[0019] Figure 3 This is a schematic diagram of the testing frame structure of an air compressor rotor testing device proposed in this utility model;
[0020] Figure 4 This is a schematic diagram of the adjustment mechanism of an air compressor rotor detection device proposed in this utility model.
[0021] Legend:
[0022] 1. Machine base; 2. Support mechanism; 201. First support seat; 202. First motor; 203. First synchronous pulley; 204. Synchronous belt; 205. First support wheel; 206. Second synchronous pulley; 207. Second support wheel; 208. Fixed frame; 209. First hydraulic cylinder; 210. Wheel frame; 211. Pressure roller; 212. Limiting plate; 213. Support plate; 214. Second support seat; 3. Adjustment mechanism; 301. Adjustment groove; 302. Guide rod; 303. Adjustment seat; 304. Mounting groove; 305. Second hydraulic cylinder; 4. Detection frame; 5. Second motor; 6. Lead screw; 7. Moving seat; 8. Mounting frame; 9. Detection probe. Detailed Implementation
[0023] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.
[0024] Reference Figure 1 The present invention provides an embodiment of an air compressor rotor testing device, comprising a machine base 1, a support mechanism 2 provided on the upper surface of the machine base 1, and a testing frame 4 fixedly connected to the upper surface of the machine base 1. The support mechanism 2 is used to support and limit the shaft end of the rotor.
[0025] Reference Figure 2 The support mechanism 2 includes a first support base 201. A first motor 202 is provided on the right wall of the first support base 201. A first synchronous pulley 203 is fixedly connected to the output end of the first motor 202. A first support wheel 205 is rotatably connected to the inner wall of the first support base 201 through a bearing. A second synchronous pulley 206 is fixedly connected to the right end of the axle of the first support wheel 205. A synchronous belt 204 is rotatably connected to the outer wall of the second synchronous pulley 206. The lower end of the synchronous belt 204 is rotatably connected to the outer wall of the first synchronous pulley 203. When the first motor 202 is started, it can drive the first support wheel 205 to rotate through the synchronous pulley and the synchronous belt 204. A second support wheel 207 is rotatably connected to the inner wall of the first support base 201 through a bearing. The first support wheel 205 and the second support wheel 207 are symmetrically arranged front and back. The right shaft end of the rotor can be placed between the first support wheel 205 and the second support wheel 207. The first support wheel 205 and the second support wheel 207 can provide V-shaped limiting support for the rotor shaft end.
[0026] A fixed frame 208 is fixedly connected to the upper surface of the first support base 201. A first hydraulic cylinder 209 is fixedly connected to the inner wall of the fixed frame 208. A wheel frame 210 is fixedly connected to the telescopic end of the first hydraulic cylinder 209. The position and height of the wheel frame 210 can be adjusted by starting the first hydraulic cylinder 209.
[0027] The inner wall of the wheel frame 210 is rotatably connected to a pressure roller 211 via a bearing. A limit plate 212 is fixedly connected to the right wall of the wheel frame 210. The rear end of the limit plate 212 is slidably connected to the right wall of the fixed frame 208. The limit plate 212 can limit and guide the wheel frame 210. When the wheel frame 210 moves down, its pressure roller 211 can press the shaft end of the rotor against the first support roller 205 and the second support roller 207.
[0028] A second support base 214 is fixedly connected to the left end of the upper surface of the machine base 1. A support plate 213 is fixedly connected to the right wall of the first support base 201. The support plate 213 facilitates the installation and fixation of the first motor 202. The bottom of the first motor 202 is fixedly connected to the upper surface of the support plate 213. The second support base 214 can support the left end of the rotor.
[0029] Reference Figure 3 A second motor 5 is fixedly connected to the right wall of the testing frame 4. A lead screw 6 is fixedly connected to the output end of the second motor 5. A movable seat 7 is slidably connected to the inner wall of the testing frame 4. The inner wall of the movable seat 7 is threadedly connected to the outer wall of the lead screw 6. By starting the second motor 5, the lead screw 6 is driven to rotate, thereby achieving the purpose of adjusting the left and right position of the movable seat 7.
[0030] A mounting bracket 8 is fixedly connected to the front of the movable seat 7, and a detection probe 9 is fixedly connected to the inner wall of the mounting bracket 8. The detection probe 9 performs flaw detection on the rotor during the movement of the movable seat 7.
[0031] Reference Figure 1 - Figure 2 , Figure 4 An adjustment mechanism 3 is provided on the upper surface of the machine base 1. The adjustment mechanism 3 includes an adjustment groove 301, which is formed on the upper surface of the machine base 1. An installation groove 304 is formed on the upper surface of the machine base 1. A guide rod 302 is fixedly connected to the inner wall of the adjustment groove 301. An adjustment seat 303 is slidably connected to the outer wall of the guide rod 302. The guide rod 302 can limit and guide the adjustment seat 303. The top of the adjustment seat 303 is fixedly connected to the bottom of the first support seat 201. A second hydraulic cylinder 305 is fixedly connected to the inner wall of the installation groove 304. The telescopic end of the second hydraulic cylinder 305 is fixedly connected to the right wall of the adjustment seat 303. By activating the second hydraulic cylinder 305, the adjustment seat 303 can be moved, so that the position of the first support seat 201 on the adjustment seat 303 can be adjusted, thereby facilitating the support of rotors of different lengths.
[0032] Working principle: During testing, the right shaft end of the air compressor rotor to be tested is placed between the first support wheel 205 and the second support wheel 207. The first support wheel 205 and the second support wheel 207 are arranged in a V-shape to provide stable support for the rotor shaft end. The first hydraulic cylinder 209 is activated, and its telescopic end drives the wheel frame 210 to move downward. The limiting plate 212 slides along the right wall of the fixed frame 208 to guide the rotor shaft end, so that the pressure wheel 211 presses and fixes the rotor shaft end between the first support wheel 205 and the second support wheel 207. The left shaft end of the rotor is supported by the second support seat 214. The first motor 202 is activated, and the output end of the first motor 202 drives the first synchronous wheel 203 to rotate. Through the synchronous belt 204, the second synchronous wheel 206 is driven to rotate, which in turn drives the first support wheel 205 and the second support wheel 207 to rotate synchronously, causing the rotor to rotate at a constant speed around its axis. The second motor 5 is started, and the output end of the second motor 5 drives the lead screw 6 to rotate. The lead screw 6 is threaded with the inner wall of the movable seat 7, so that the movable seat 7 slides left and right along the inner wall of the detection frame 4, which drives the detection probe 9 on the mounting frame 8 to continuously scan and detect the surface of the rotating rotor. When it is necessary to detect rotors of different lengths, the second hydraulic cylinder 305 is started. Its telescopic end pushes the adjusting seat 303 to slide along the guide rod 302 in the adjusting groove 301. The adjusting seat 303 drives the first support seat 201 to move horizontally, thereby adjusting the distance between the first support seat 201 and the second support seat 214 to achieve support and positioning of rotors of different lengths.
Claims
1. An air compressor rotor detection device, comprising a machine table (1), characterized in that: The upper surface of the machine base (1) is provided with a support mechanism (2), and a testing frame (4) is fixedly connected to the upper surface of the machine base (1). The support mechanism (2) includes a first support base (201), a first motor (202) is provided on the right wall of the first support base (201), a first synchronous pulley (203) is fixedly connected to the output end of the first motor (202), a first support wheel (205) is rotatably connected to the inner wall of the first support base (201) through a bearing, a second synchronous pulley (206) is fixedly connected to the right end of the axle of the first support wheel (205), a synchronous belt (204) is rotatably connected to the outer wall of the second synchronous pulley (206), the lower end of the synchronous belt (204) is rotatably connected to the outer wall of the first synchronous pulley (203), and a second support wheel (207) is rotatably connected to the inner wall of the first support base (201) through a bearing. A fixed frame (208) is fixedly connected to the upper surface of the first support base (201). A first hydraulic cylinder (209) is fixedly connected to the inner wall of the fixed frame (208). A wheel frame (210) is fixedly connected to the telescopic end of the first hydraulic cylinder (209). A pressure wheel (211) is rotatably connected to the inner wall of the wheel frame (210) through a bearing.
2. The air compressor rotor inspection apparatus of claim 1, wherein: A limiting plate (212) is fixedly connected to the right wall of the wheel frame (210), and the rear end of the limiting plate (212) is slidably connected to the right wall of the fixed frame (208).
3. The air compressor rotor detection device of claim 1, wherein: The upper surface of the machine base (1) is fixedly connected to the left end of the second support base (214), the right wall of the first support base (201) is fixedly connected to the support plate (213), and the bottom of the first motor (202) is fixedly connected to the upper surface of the support plate (213).
4. The air compressor rotor detection device of claim 1, wherein: The right wall of the testing frame (4) is fixedly connected to a second motor (5), and the output end of the second motor (5) is fixedly connected to a lead screw (6). The inner wall of the testing frame (4) is slidably connected to a movable seat (7), and the inner wall of the movable seat (7) is threadedly connected to the outer wall of the lead screw (6).
5. The air compressor rotor detection apparatus of claim 4, wherein: The front of the movable seat (7) is fixedly connected to a mounting bracket (8), and the inner wall of the mounting bracket (8) is fixedly connected to a detection probe (9).
6. The air compressor rotor inspection apparatus of claim 1, wherein: The upper surface of the machine base (1) is provided with an adjustment mechanism (3), the adjustment mechanism (3) includes an adjustment groove (301), the adjustment groove (301) is opened on the upper surface of the machine base (1), and the upper surface of the machine base (1) is provided with an installation groove (304).
7. The air compressor rotor detection apparatus of claim 6, wherein: The inner wall of the adjustment groove (301) is fixedly connected to a guide rod (302), and the outer wall of the guide rod (302) is slidably connected to an adjustment seat (303). The top of the adjustment seat (303) is fixedly connected to the bottom of the first support seat (201). The inner wall of the mounting groove (304) is fixedly connected to a second hydraulic cylinder (305), and the telescopic end of the second hydraulic cylinder (305) is fixedly connected to the right wall of the adjustment seat (303).