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Control plane body milling tool

A milling and tooling technology, applied in the field of machining, can solve the problems of difficult to guarantee the machining accuracy of parts, difficult clamping of the middle groove and left bevel, and low efficiency, so as to broaden the processing limitations, easily adapt to production and processing, cost reduction effect

Inactive Publication Date: 2016-03-09
HARBIN JIANCHENG GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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specific Embodiment approach 1

[0007] Specific implementation mode one: combine Figure 1 to Figure 3 Describe this embodiment, a kind of rudder surface body milling tooling described in this embodiment includes a base plate 1, two pressure plates 4 and four M10 socket head bolts 3, the base plate 1 is a rectangular plate body, the base plate 1 is horizontally arranged, and the upper surface of the base plate 1 There is a rectangular groove 1-1 in the middle of the rectangular groove 1-1, a shoulder 1-2 is provided on one side of the rectangular groove 1-1, and two first screw holes 1-3 are provided on one side of the upper surface of the bottom plate 1 along the length direction. , the rectangular groove 1-1 is provided with two second screw holes 1-4 along the length direction, two mounting gaps 1-5 are opened on each side edge of the bottom plate 1, and the two pressure plates 4 pass through two M10 inner hexagon bolts 3 is installed in the two first screw holes 1-3, and the workpiece 5 is installed in t...

specific Embodiment approach 2

[0008] Specific implementation mode two: combination Figure 1 to Figure 3 To illustrate this embodiment, the rudder surface body milling tool described in this embodiment further includes two pads 2 , and one pad 2 is provided between the lower surface of each pressing plate 4 and the upper surface of the base 1 .

[0009] The technical effect of this embodiment is: with such arrangement, other components and connections are the same as those in the first embodiment.

specific Embodiment approach 3

[0010] Specific implementation mode three: combination Figure 1 to Figure 3 Describe this embodiment, the length of the bottom plate 1 of the steering surface body milling tool described in this embodiment is 340mm, the width of the bottom plate 1 is 240mm, and the thickness of the bottom plate 1 is 30mm. Other compositions and connections are the same as those in Embodiment 1 or 2.

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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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23Q3/00
Inventor 王智莉王学志张丹文化高伟马明礼姚飞
Owner HARBIN JIANCHENG GRP
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