2。2。 Dynamics of machine tools
This paper describes the FRFs and the stability lobe diagrams for chatter for the arch-type RMT at the y ¼ 01 and 451 reconfiguration position, to investigate variations
Fig。 1。 Final design for RMT with its finite element model。
328 J。 Dhupia et al。 / International Journal of Machine Tools & Manufacture 47 (2007) 326–334
Table 1
Modal data for final RMT design
Mode # Frequency (Hz) Comments
1 36 Mainly due to weak connection between the ram and the arch。
2 53 Mainly due to column/base structure
3 60 Mainly due to a combination of weak connection between the ram and the arch,
4
69 and stiffness of Y-axis
Mainly due to weak connection between the ram and the arch
5 72 Mainly due to a combination of weak connection between the ram and the arch,
and stiffness of Z-axis
These data are valid only for a position of the machine in which: (a) spindle is half the way extended, i。e。 250 m, (b) ram is positioned at 451 angle, and (c) arch is positioned at the middle of its 775 mm stroke。
Fig。 2。 Different pivot-type RMT design concepts。
Fig。 3。 Arch-type RMT。
in arch-type RMT dynamic performance。 While the FRF gives the description of structural vibrations and stiffness of the machine tool [21], the stability lobes for chatter can be used as a direct assessment of the expected machining quality and productivity。
The FRF matrix, also known as the receptance matrix for the relative workpiece-machine tool vibration,GðioÞ, is
the transfer function from the cutting force to the rela- tive workpiece–machine displacement。 GðioÞ ¼ GtðioÞ— GwðioÞ, where GtðioÞ and GwðioÞ are the FRF matrices of tool and workpiece, respectively。 Let the displacement of the tool be ut and that of the workpiece be uw。 The cutting forces acting on the tool ðftÞ and the workpiece ðfwÞ have the same magnitude but opposing directions (i。e。 ft ¼ —fw)。
J。 Dhupia et al。 / International Journal of Machine Tools & Manufacture 47 (2007) 326–334 329
10。15 10。2 10。25 10。3 10。35 10。4 10。45
Time, t [sec]
Fig。 4。 Experimental and estimated cutting forces at ap ¼ 3:3 mm, N ¼ 1700 RPM and f t ¼ 7:2 mm=s。
In this paper the workpiece is assumed rigid, and the this system is
assumption was verified by measuring the FRF of the
workpiece and measuring the vibrations displacement of
the workpiece during the cutting experiments。 Thus, the
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