Laser precision de-weight system and method
A laser and precision technology, applied in laser welding equipment, welding equipment, metal processing equipment, etc., can solve problems such as affecting the service life of the rotor, affecting the working stability of the gyro instrument, and being unsuitable for the laser dynamic balance measurement method, to optimize the optical Structural design, reduce laser deduplication burr, the effect of the best deduplication effect
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2015-12-02
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention relates to a device that uses laser technology to complete the adjustment of the center of mass of the rotor so that it reaches a balanced state. Specifically, it relates to a laser precision weight removal system and method, which is mainly used to improve the balance precision of inertial navigation systems and jet engines. processing field. Background technique
[0002] With the continuous improvement of the precision and stability of the inertial gyro instrument, the accuracy and process requirements for the dynamic balance of the gyro rotor are also increased. The deweighting balance is actually completed by changing the mass distribution of the rotor. In all precision machinery and instruments with high-speed rotating parts such as gyro motors, electric motors, jet engine moving parts, etc., the functional errors (such as drift effects on gyroscopes) and disturbing swings are often caused by residues in the rotating parts. caused b...
Examples
Embodiment
[0081] Attached below figure 1 A specific example of the present invention is described:
[0082] This example is mainly aimed at the laser precision de-weighting system to realize the function of rotor balance, which is used to improve the balance accuracy of rotating parts such as inertial navigation systems and jet engines, and is suitable for the precision machining fields of aviation, aerospace and military.
[0083] The components and features included in the system are: the laser 110 and the visible light indicator 120 emit lasers with wavelengths of 1064nm and 632.8nm respectively, wherein the average power of the 1064nm laser is 30W, and the average power of the 632.8nm laser is 10mW on the same optical axis. The optical path transmitter 130 includes a beam combiner and a beam expander. One side of the beam combiner is coated with a 1064nm anti-reflection coating, and the other side is coated with a 45° 632.8nm high-reflection coating, which is used to reflect the ind...