Transactions of Nanjing University of Aeronautics & Astronautics
Methods for Reducing Interface Aperture Inconsistency During NC Orbital Milling of Aircraft Laminates with Coarse Pitch
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Abstract:
The methods for reducing interface aperture inconsistency are studied in NC orbital milling (NCOM) of CFRP/Ti6Al4V laminates with coarse pitch. Comparative experiments show burr, aperture inconsistency and error are typical interface defects. Meanwhile, aperture inconsistency and error are more serious than burr in NCOM with coarse pitch. As one of the major causes of interface defects, axial force and radial force are intensively studied. Based upon the machining principle of orbital milling (OM) and the actual hole-making condition in laminated structures, NCOM experiments with coarse pitch are conducted on CFRP/Ti6Al4V laminates under different cutting conditions. Then, the effects of interlayer clamping, minimal quantity lubrication (MQL), twice milling instead of reaming, and interlayer speed change on interface aperture are analyzed. Research shows that interlayer clamping, interlayer speed change and MQL can effectively reduce out-of-tolerance of interface aperture. When making holes of different diameters with one cutter, axial feed has a greater effect on interface aperture precision than tangential feed. When making holes of the same diameter with different cutters, small diameter cutter will reduce interface aperture precision in a single processing. But the method of “twice milling instead of reaming” can improve the aperture precision effectively.
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Clc Number:
TG146.23
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