Flexible adjusting and positioning device for aviation high-temperature guide pipe and new manufacturing process

Abstract

The invention provides a flexible adjusting and positioning device for an aviation high-temperature guide pipe and a new manufacturing process. According to the flexible adjusting and positioning device for the aviation high-temperature guide pipe and the new manufacturing process, a bottom plate is installed at the top of a mounting plate in a supported mode through a lifting adjusting mechanism, a transverse adjusting plate capable of transversely moving and adjusting is installed at the top of the bottom plate in a supported mode, and a longitudinal adjusting plate capable of longitudinally moving and adjusting is installed at the top of the transverse adjusting plate in a supported mode; a first arc-shaped seat is supported on the top of the longitudinal adjusting plate through a Z-axis rotating seat, an X-axis rotating seat is hinged to the first arc-shaped seat through a first rotating shaft, a second arc-shaped seat is fixed to the top of the X-axis rotating seat, a Y-axis rotating seat is hinged to the second arc-shaped seat through a second rotating shaft, and a positioning connecting assembly is installed on the Y-axis rotating seat. Through a pure mechanical manual adjusting mechanism, movement and rotation in all directions in a three-dimensional space are integrated on one adjusting device, adjusting positioning and locking of six degrees of freedom in the three-dimensional space can be quickly achieved, and the quick space positioning requirements of different mounting holes or mounting faces are met.

Description

technical field [0001] The invention relates to the field of aviation maintenance technology and equipment, in particular to an aviation high-temperature conduit flexible adjustment and positioning device and a new manufacturing process. Background technique [0002] In accordance with the requirements of the aircraft manufacturer's technical bulletin, during the process of new manufacturing and field refitting of aircraft engine high-temperature air ducts, it was found that the aero-engine high-temperature air ducts were different due to different aircraft sorties, large number of ducts, many troops involved, and wide distribution areas. , there are differences in the direction of the pipeline and the installation size on the machine. In addition, local deformation and misalignment will occur after long-term use, which adds difficulty to the new production and replacement of high-temperature conduits. and sampling to determine the direction of the pipeline, it is necessary ...

AI Technical Summary

Problems solved by technology

[0002] In accordance with the requirements of the aircraft manufacturer's technical bulletin, during the process of new manufacturing and field refitting of aircraft engine high-temperature air ducts, it was found that the aero-engine high-temperature air ducts were different due to different aircraft sorties, large number of ducts, many troops involved, and wide distribution areas. , there are differences in the direction of the pipeline and the installation size on the machine. In addition, local deformation and misalignment will occur after long-term use, which adds difficulty to the new production and replacement of high-temperature conduits. and sampling to determine the direction of the pipeline, it is necessary to determine the spatial position of the conduit interface through repeated physical inspections on the machine and gradual cutting and grinding on site. The duct cannot be installed on the aircraft or interferes with other parts

[0003] In addition, the aircraft cannot fly during the tube replacement process, and as the military training and various special tasks become more and more heavy, there will not be too much time for the tube replacement, and there will be no opportunities to disassemble the tube multiple times. It will affect the normal training and tasks of the troops

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