Control plane body milling tool

Abstract

Provided is a control plane body milling tool, relating to a milling tool. The invention especially relates to the control plane body milling tool for the purpose of solving problems that a middle groove and a left inclined edge of a milled control plane body part are hard to clamp; efficiency is low, and part machining precision cannot be ensured. The control plane body milling tool comprises a bottom plate, two pressing plates and four M10 hexagon socket screws. The bottom plate is a rectangular and is horizontally arranged. A rectangular groove is formed in the middle of the upper surface of the bottom plate. A circular bead is arranged on one side in the rectangular groove. The size of the circular bead of the rectangular groove is matched with the relevant size of the part. Two first screw holes are formed in one side of the upper surface of the bottom plate in the length direction, two second screw holes are formed in the rectangular groove in the length direction. Two mounting gaps are formed in each side edge of the bottom plate. The two pressing plates are arranged in the two first screw holes through two M10 hexagon socket screws, and workpieces are arranged in the two second screw holes through the other two M10 hexagon socket screws. The control plane body milling tool is used for machining the control plane body workpieces.

Description

technical field [0001] The invention relates to a milling tool, in particular to a rudder surface milling tool, which belongs to the field of mechanical processing. Background technique [0002] In the processing of the existing rudder surface parts, the middle groove and the left hypotenuse are processed by slow wire cutting, which takes a long time and high processing cost; in order to reduce the cost, the milling method is used to process the two parts, but Clamping is difficult, efficiency is low, and the machining accuracy of parts is difficult to guarantee. Contents of the invention [0003] The invention aims to solve the problems of difficult clamping of the middle groove and the left hypotenuse of the milling process of the rudder surface body parts, low efficiency, and difficulty in ensuring the machining accuracy of the parts, and further designs the rudder surface body milling tooling. [0004] The technical scheme adopted by the present invention to solve the...

AI Technical Summary

Problems solved by technology

[0003] The present invention aims to solve the problems of difficult clamping of the middle groove and the left hypotenuse of the milling process of the rudder surface body parts, low efficiency, and difficulty in ensuring the machining accuracy of the parts, and further designs the rudder surface body milling tooling

[0005] The beneficial effects of the present invention are: the present invention improves the production efficiency of workpiece processing, reduces the cost, solves the processing limitations caused by the structure of the workpiece, and is easier to adapt to production and processing. Due to the processing characteristics of the variable bevel parts, the precision requirements of the parts themselves are used for positioning. Two clamping plates are used for main clamping and two bolts are used for auxiliary clamping to provide reliable clamping force and positioning accuracy. In addition, a smaller The cutting tool and the reasonable cutting parameters strive for the minimum cutting force for processing; the invention accurately positions the workpiece, and the workpiece does not need to be aligned and corrected for processing zero every time, thereby reducing the labor intensity of the staff and improving the processing efficiency; The invention adopts reasonable positioning and clamping, which broadens the processing limitations of parts, reduces processing costs and improves production efficiency

Images