SU1496989A1 - Conveying device for transfer line - Google Patents

Abstract

The invention relates to the automation of transport operations during machining and assembly on multi-position automatic lines. The purpose of the invention is to expand the technological capabilities of the lines by providing the possibility of transporting satellites in steps other than the main one. The device contains satellites 1-4 with longitudinal guide rails, support and guide rails for satellites, a pusher of a hydraulic cylinder 9 for moving satellites along guide rails, a mechanism for moving satellites in steps other than the main one. The insert 13 is installed with the possibility of rotation and displacement from the drives on an axis parallel to the direction of movement in the satellite movement section with a step different from the main one. 6 Il.

Description

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The invention relates to the automation of transport operations during machining and assembly on multi-station automatic lines.

The aim of the invention is to expand the technological capabilities of the line by providing the possibility of transporting satellites with a step other than the main O1.

On fpg. 1 schematically shows a transport device in the initial position; FIG. 2 is a section A-A in FIG. one; in fig. 3 - the transport device after the satellites are moved step; in fig. 4 the same, at the beginning of the cycle of the movement of the satellites in increments other than the main one; in fig. 5 - section bb pa. Fig 4; in fig. 6 - the transport device after the end of the movement of the satellite with

The transport device contains satellites 1-4 with longitudinal guides L-shaped strips 5 and b, support-guide bars 7 and 8, a mechanism for moving satellites in the form of a hydraulic cylinder 9 pusher, Mexai-movement of satellites in section B with a step different from the main one, in the form of a sump conveyor with a round rod 10 with flags 11 located on rollers 12 with the possibility of rotation around the axis of the rod and longitudinal movement along the axis from the drives (not shown), insert 13 installed rotatably around axis 14 from hydrocyl Idra 15 and movements along it in section B from the hydraulic cylinder 16. There are fasteners 17 on the satellites on both sides to create a gap between the satellite bodies when placed close to each other. Longitudinal movement of the insert is limited by the stops 18 and 19.

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In the initial position, the insert 13 from the hydraulic cylinder 15 is inserted between the stops 17 of satellites at the beginning of section B. From the hydraulic cylinder 9, the satellites with the insert move close to each other along rails 7 and 8 to step L equal to the length of the satellite (Fig. 3). After movement, the insert is lowered by the cylinder 15 below the satellites and the hydraulic cylinder 16 returns along axis 14 to the stop 18 (Fig. 4).

Claims (2)

By rotating the rod 10, the flags 11 are engaged with the satellite 2, and by the longitudinal movement of the rod 10, the satellite 2 is successively moved to steps different from the main one in section B. In the final position, the satellite 2 is brought to the contact by the stops 17 with the stop 3, and the rotation rods 10 flags 11 disengaged from the satellite 2. An insert is inserted between the satellites at the beginning of section B by the cylinder 15, a satellite is fed from the return conveyor (not shown) to the beginning of the transport device and a new movement cycle is carried out from the cylinder 9. Invention Formula An automatic line transport device containing support-guiding strips for satellites, a mechanism for moving satellites along the arrays, characterized in that, in order to expand technological capabilities, it is provided with an insert mounted on the axis with its translational movement along this axis, with This latter is parallel and stationary relative to the support-guide bars for the satellites, and the insert is mounted on the axis with the possibility of rotation from the additionally introduced drive and ontaktirovani satellites. ten 12/5 Lj / .sixteen 13 Фцг.З h 3 // 6  / .Tg-rr W Uh 1496989 / 1- / I 13 Pj H / iff fi &. 2 / 18 /15 Ir Jl t-g-rr W A 7 T Fog. p ya AT 6 13 15 FIG. five