Design of Flexible Fixture for Wing Structure of Aircraft Based on PLC
GAO Sheng1,WANG Xiyang2, HUANG Qi1
1. College of Aeronautical Manufacturing Engineering, Nanchang Hangkong University, Nanchang 330063, China;
2. College of Aircraft Engineering, Nanchang Hangkong University, Nanchang 330063, China
Aiming at the high speed milling of the wing structure in the aviation field, a fixture design scheme with small interference, high flexibility, fast changing and high automation is proposed in this paper. The composition, principle and PLC control program of the fixture system is discussed in detail. In order to solve the problem that the waste of raw materials in the traditional folder and interference between machine tool and fixture in processing, adjustable positioning plate positioning, rotary clamping cylinder clamping, the use of sensor perception, PLC control achieve the electromagnetic valve orderly action and the workpiece reliable clamping in this paper. Correspondingly, the PLC control program is edited successfully. The fixture design can be used in the actual production of the aircraft structural components and the design of the automatic control fixture.
基金资助:武装预研基金(AA201506033)。
引用本文:
高升,王细洋,黄琦. 基于PLC 的飞机翼类结构件柔性夹具设计[J]. 航空制造技术, 2019, 62(10): 93-97.
GAO Sheng,WANG Xiyang, HUANG Qi. Design of Flexible Fixture for Wing Structure of Aircraft Based on PLC. Aeronautical Manufacturing Technology, 2019, 62(10): 93-97.