CAJ | 학술논문

通过对数字化柔性装配技术的深入分析，结合某型号襟翼试验件研制，设计、制造了飞机内外前襟的数字化柔性工装，并完成了该柔性工装的安装、调试。该柔性工装由7个立柱式三坐标定位单元，各定位单元均能独立运动，由定位单元联合驱动实现内外前襟试验件4个部件的柔性装配。由应用结果可知：利用该工装提高了装配质量和效率，验证了内外前襟数字化柔性工装技术可行性。该工装的成功应用为后续类似结构的工装制造提供了成功案例。
통과대수자화유성장배기술적심입분석，결합모형호금익시험건연제，설계、제조료비궤내외전금적수자화유성공장，병완성료해유성공장적안장、조시。해유성공장유7개립주식삼좌표정위단원，각정위단원균능독립운동，유정위단원연합구동실현내외전금시험건4개부건적유성장배。유응용결과가지：이용해공장제고료장배질량화효솔，험증료내외전금수자화유성공장기술가행성。해공장적성공응용위후속유사결구적공장제조제공료성공안례。
Based on the analysis of digital, flexible assembly technology, a digital control and flexible tools is proposed for airplane flap assembly. The proposed tools have seven pillar-style positioners, which can move along x, y, z directions. The seven positioners control airplane flap pose during the assemble. Engineering application shows that the proposed tools can assemble different size airplane flaps on the basis of quality assurance, and the tools improve the assembly efficiency.