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Numerical control machining clamp for control plane part

A technology of parts and rudder surfaces, which is applied in the field of CNC machining fixtures for rudder surface parts, can solve the problems of low clamping reliability, inconsistent clamping force, and low degree of automation of rudder surface parts, shorten the production cycle, and improve machining accuracy , the effect of high degree of automation

Inactive Publication Date: 2020-02-14
SHANGHAI JIAO TONG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the above-mentioned deficiencies in the prior art, the present invention proposes a numerical control machining fixture for rudder surface parts, which can realize effective and fast clamping of rudder surface parts, and solve the problem of low reliability of rudder surface parts clamping, inconsistent clamping force, Problems with long setup time and low degree of automation

Method used

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  • Numerical control machining clamp for control plane part
  • Numerical control machining clamp for control plane part
  • Numerical control machining clamp for control plane part

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Embodiment Construction

[0017] like figure 1 As shown, it is a CNC machining fixture for steering surface parts related to this embodiment, which includes: a base 8 and a positioning device 12, a clamping device 13 and an auxiliary device 14 arranged on the base 8, wherein: the workpiece 3 is arranged on The middle area of ​​the base 8 is fixed by the positioning device 12, the clamping device 13 is set on the pre-designed position on the base 8 to clamp the workpiece 3, and the auxiliary device 14 is set around the surface of the base 8 for connecting and fixing with the machine tool.

[0018] The positioning device 12 includes: a fixed support column 10, a floating support column 11, a side positioning column 6 and a tool positioning column 7, wherein: the fixed support column 10 and the floating support column 11 are arranged below the workpiece 3, and the side positioning column 6 is arranged on the side of the workpiece 3, and the tool positioning column 7 is arranged on the side of the base 8. ...

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Abstract

Disclosed is a numerical control machining clamp for a control plane part. The numerical control machining clamp comprises a base, and a positioning device, a clamping device and an auxiliary device which are arranged on the base. A workpiece is arranged in the middle region of the base and fixed by the positioning device, the clamping device is arranged at the periphery of the base and clamps theworkpiece, and the auxiliary device is arranged at the periphery of the surface of the base for being fixedly connected to a machine tool. The positioning device comprises a fixed supporting column,a floating supporting column, a side positioning column and a tool positioning column. The clamping device comprises a hydraulic power mechanism, a rotation compressing oil cylinder and a pressing head. The auxiliary device comprises a hanging ring screw for being connected with the machine tool and a connecting hole for being fixed to the machine tool. The control plane part can be effectively and rapidly clamped, the problems that the control plane part clamping reliability is low, and the clamping force is not consistent are solved, the production period is shortened, the machining precision is improved, the automatic degree is high, beneficial contributions are made to boosting of the overall progress of the control plane part, and the high technical content and the high economic valueare achieved.

Description

technical field [0001] The invention relates to a technology in the field of mechanical manufacturing, in particular to a numerically controlled machining fixture for rudder surface parts. Background technique [0002] As the main load-bearing components of missiles and other aircraft, the rudder surface parts are generally realized by high-strength titanium alloy rudder surface at this stage, but the processing performance of titanium alloy is poor, and the material removal rate is high during the rudder surface processing process. Easy to deform. Rudder surface parts mainly adopt the traditional clamping method of mechanical pressure plate clamping, which has many problems such as long clamping time, low clamping reliability, and unguaranteed clamping force and consistency. Contents of the invention [0003] Aiming at the above-mentioned deficiencies in the prior art, the present invention proposes a numerical control machining fixture for rudder surface parts, which ca...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23Q3/08
CPCB23Q3/082
Inventor 陈明邹凡安庆龙明伟伟郭国强
Owner SHANGHAI JIAO TONG UNIV