CN207050684U - A kind of small aero bent axle circle bounce, system for detecting roundness - Google Patents

Abstract

The utility model discloses a kind of bounce of small aero bent axle circle, system for detecting roundness；The stationary center of detection means and rolling center are fixed on the both ends of platform in detecting system, are moved by the handle of rolling center, make rolling center and stationary center and crankshaft two end centralized positioning clamping bent axle.Two U-shaped piece is fixed between stationary center and rolling center, and U-shaped piece is respectively supported at main bearing journal.It is located in three detection arms equipped with detector on platform, detector is adjusted and keeps being horizontally oriented measurement with measured workpiece automatically in short transverse, and each detector corresponds to the corresponding test point of measured workpiece.Sampled value is simultaneously transferred to industrial computer by detector gathered data, and industrial computer receives data and carries out calculation process, and testing result is shown by display.Detecting system also has data record, tracking and function of statistic analysis, is convenient for Quality Control Analysis；Improve the reliability of tractor crankshaft efficiency and testing result.

Description

A small aeroengine crankshaft circular runout and roundness detection system

technical field

The utility model relates to the technical field of mechanical measurement, in particular to a small aeroengine crankshaft circle runout and roundness detection system.

Background technique

The crankshaft is the core moving part of a small aero piston engine. Compared with other engines, the dimensional accuracy and behavioral tolerance of the aeroengine crankshaft are higher. The traditional measurement method of crankshaft runout and roundness is: use the top holes at both ends of the workbench to locate and supplement with special process equipment, use a dial indicator to measure each rotary surface separately, and draw a detection conclusion. The traditional detection method relies too much on personal Technology, less efficient.

In the patent CN2727691Y, "a comprehensive detection device for engine crankshaft" is disclosed. On the inspection tool base, the detection head is a sensor detection head; the inspection tool base is also equipped with two sets of top devices against the central holes at both ends of the crankshaft. Through the connection, the signals detected by the detection head are transmitted to the same electronic beam display and displayed separately. During detection, two sets of top devices position the crankshaft to be inspected, and after tightening it appropriately, the crankshaft is manually rotated for one circle, and each sensor detection head detects each corresponding part of the crankshaft at the same time. The detected signals are transmitted to the electronic light column display through the connected sensor detection heads and displayed separately. The difference between the maximum value and the minimum value of each display bar deviated from the zero position is the runout value of the surface to be tested, refer to Figure 1. This detection device has the following deficiencies:

a. The detection device adopts a relative measurement method, and the result obtained is a relative result, that is, it can only determine whether the parts are qualified but cannot detect specific values, and cannot be used for grouping engine parts. The application of this detection device has great limitations;

b. The detection device has high requirements on the manufacturing precision of the standard sample, and the state of the standard part directly affects the measurement result of the part;

c. The detection device does not have the functions of data recording, tracking and statistical analysis, and can only be used for the inspection of whether the workpiece is qualified, which is not convenient for quality control analysis.

Utility model content

In order to avoid the deficiencies in the prior art, the utility model proposes a small aero-engine crankshaft circle runout and roundness detection system.

The technical scheme adopted by the utility model to solve its technical problems is: comprising platform, fixed top, movable top, U-shaped block, detection arm, detection head, detection button, display, industrial computer and base, and described platform is fixed on the base On the seat, the central axis of the platform and the central axis of the base are in the same vertical plane, the industrial computer is installed in the base, the display and the detection button are respectively fixed on the side ends of the platform above the base, the display and the detection button are connected to the industrial computer through wires connect;

The fixed top and the movable top are respectively fixed on the two ends of the platform, and a handle is installed at one end of the movable top, and the movable top, the fixed top and the center blind holes at both ends of the crankshaft are positioned and clamped to the crankshaft by moving the handle; two U-shaped The block is fixed on the platform between the fixed top and the movable top, and the two U-shaped blocks are respectively supported at the main journal of the crankshaft;

There are three detection arms, and the detection arms are fixed on the platform, wherein two detection arms are located at the side of the U-shaped block at the front of the movable top, and the other detection arm is located at the side of the U-shaped block at the front of the fixed top. The detection head is installed on the top, and it is automatically adjusted in the height direction and kept in the horizontal direction with the measured workpiece for measurement. Each detection head corresponds to the corresponding detection point of the measured workpiece; press the start detection button, the detection head collects data and transmits the sampled value It is processed by the industrial computer, and the industrial computer receives the data and performs calculation processing, and the detection result is displayed in real time on the display.

The movable top, U-shaped block and fixed top are coaxially installed.

Beneficial effect

The utility model proposes a small aero-engine crankshaft circular runout and roundness detection system; the detection device in the detection system has its fixed top and the movable top fixed at both ends of the platform, and the movable top is equipped with a handle, which can be moved and moved by the handle. The top, so that the movable top and the fixed top are positioned with the central blind holes at both ends of the crankshaft to clamp the crankshaft; two U-shaped blocks are fixed between the fixed top and the movable top, and the U-shaped blocks are respectively supported on the main journal of the crankshaft. There are three detection arms, and each detection arm is equipped with a detection head. The detection head of the detection arm is automatically adjusted in the height direction and kept in a horizontal direction with the measured workpiece. Each detection head corresponds to the corresponding detection point of the measured workpiece. Press the start detection button, the detection head collects data and transmits the sampling value to the industrial computer, the industrial computer receives the collected data and performs calculation processing, and the detection result displays in real time through the display whether the tested workpiece is qualified.

The utility model also has the functions of data recording, tracking and statistical analysis, which is convenient for quality control analysis, and improves the crankshaft detection efficiency and the reliability of the detection results.

Description of drawings

A small aeroengine crankshaft circle runout and roundness detection system of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

Fig. 1 is a schematic diagram of an engine crankshaft comprehensive detection device in the prior art.

Fig. 2 is a schematic diagram of the installation parts of each component of the detection system of the present invention.

Figure 3 is a top view of the installation part of the measured workpiece.

Fig. 4 is a schematic diagram of the circular runout and roundness detection system of the small aeroengine crankshaft of the present invention.

In the picture:

1. Platform 2. Fixed top 3. Movable top 4. U-shaped block 5. Detection arm 6. Detection head 7. Workpiece under test 8. Detection button

detailed description

This embodiment is a small aeroengine crankshaft circular runout and roundness detection system.

Referring to Fig. 2, Fig. 3, Fig. 4, the present embodiment small aeroengine crankshaft circular runout, roundness detection system consists of platform 1, fixed top 2, movable top 3, U-shaped block 4, detection arm 5, detection head 6, detection The button 8, the workpiece 7 to be measured, the display, the industrial computer and the base are composed; wherein, the platform 1 is installed on the base, and the central axis of the platform 1 and the central axis of the base are located on the same vertical plane. The industrial computer is installed in the base, and the display and the detection button 8 are respectively installed on the base at the side end of the platform 1, and the display and the detection button 8 are connected with the industrial computer by wires. The fixed top 2 and the movable top 3 are respectively fixed on the two ends of the platform 1, and a handle is installed at one end of the movable top 3, and the movable top 3 is moved through the handle, so that the movable top 3, the fixed top 2 and the central blind hole positioning clips at both ends of the crankshaft Tighten the crankshaft. Two U-shaped blocks 4 are respectively fixed on the platform 1 and located between the fixed top 2 and the movable top 3, and the two U-shaped blocks 4 are respectively supported at the main journal of the crankshaft.

In this embodiment, three detection arms 5 are respectively fixed on the platform 1, wherein two detection arms 5 are installed beside the U-shaped block 4 at the front of the movable top 3, and the other detection arm 5 is installed at the front of the fixed top 2 Next to the U-shaped block 4; each detection arm 5 is equipped with a detection head 6, which corresponds to the workpiece 7 to be measured, and is automatically adjusted in the height direction and kept in a horizontal direction with the workpiece to be measured. The head 6 corresponds to the corresponding detection point of the workpiece 7 to be measured. Press the start detection button 8, the detection head 6 collects data and transmits the sampling value to the industrial computer for processing, the industrial computer receives the data and performs calculation processing, and the detection results are displayed in real time on the display.

When in use, each shift is calibrated first, the standard parts are put in first, the current shift calibration is completed, the system error and drift are eliminated, and the system enters the standby state.

When measuring, pull the handle of the movable center 3 to move the movable center 3, place the crankshaft between the fixed center 2 and the movable center 3, place the main journal of the crankshaft on two U-shaped blocks 4, and move the movable center 3 through the handle , so that the movable top 3 and the fixed top 2 are positioned with the central blind holes at both ends of the crankshaft to clamp the crankshaft. The detection heads 6 on the three detection arms 5 automatically contact the detected journal positions. Press the detection button 8 and manually rotate the crankshaft for one revolution. The crankshaft rotates one revolution based on the axis formed by the central blind holes at both ends. The detection head 6 continuously touches the workpiece to perform data sampling work. The industrial computer receives the data and performs calculation processing. The industrial computer can also set and modify the tolerance zone without reprocessing new standard parts; at the same time, set the relative zero position and absolute zero position when calibrating with standard parts, so as to measure the relative size and absolute size of the part, and measure The result is compared with the pre-set tolerance zone to draw a conclusion whether the part is qualified, and the test result is displayed in real time on the monitor.

Claims (2)

1. a small aero-engine crankshaft circle runout, roundness detection system, is characterized in that: comprise platform, fixed top, movable top, U-shaped block, detection arm, detection head, detection button, display, industrial computer and base, The platform is fixed on the base, the central axis of the platform and the central axis of the base are located on the same vertical plane, the industrial computer is installed in the base, the display and the detection button are respectively fixed on the side ends of the platform above the base, the display and the detection The button is connected with the industrial computer through wires; The fixed top and the movable top are respectively fixed on the two ends of the platform, and a handle is installed at one end of the movable top, and the movable top, the fixed top and the center blind holes at both ends of the crankshaft are positioned and clamped to the crankshaft by moving the handle; two U-shaped The block is fixed on the platform between the fixed top and the movable top, and the two U-shaped blocks are respectively supported at the main journal of the crankshaft; There are three detection arms, and the detection arms are fixed on the platform, wherein two detection arms are located at the side of the U-shaped block at the front of the movable top, and the other detection arm is located at the side of the U-shaped block at the front of the fixed top. The detection head is installed on the top, and it is automatically adjusted in the height direction and kept in the horizontal direction with the measured workpiece for measurement. Each detection head corresponds to the corresponding detection point of the measured workpiece; press the start detection button, the detection head collects data and transmits the sampled value It is processed by the industrial computer, and the industrial computer receives the data and performs calculation processing, and the detection result is displayed in real time on the display. 2. small aero-engine crankshaft circle runout according to claim 1, roundness detection system, is characterized in that: movable top, U-shaped block and fixed top coaxial installation.