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Fixture for automatically machining aero-engine blade

A technology for aero-engines and blades, which is applied in the direction of metal processing machinery parts, manufacturing tools, metal processing equipment, etc., can solve the problems that the clamping state of each blade cannot be guaranteed and are completely consistent, and achieve stable and automatic processing. Effect

Pending Publication Date: 2022-08-09
CHENGDU AERONAUTIC POLYTECHNIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the deficiencies of the prior art, the present invention provides a fixture for automatic machining of aeroengine blades, which solves the problem that the clamping state of each blade cannot be guaranteed to be completely consistent when the blades are processed in batches

Method used

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  • Fixture for automatically machining aero-engine blade
  • Fixture for automatically machining aero-engine blade
  • Fixture for automatically machining aero-engine blade

Examples

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Embodiment Construction

[0021] In order to make the technical means, creative features, goals and effects realized by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments, but the following embodiments are only preferred embodiments of the present invention, not all. Based on the examples in the implementation manner, other examples obtained by those skilled in the art without creative work shall fall within the protection scope of the present invention. The experimental methods in the following examples are conventional methods unless otherwise specified, and the materials, reagents, etc. used in the following examples can be obtained from commercial sources unless otherwise specified.

[0022] Example:

[0023] like figure 1 and figure 2 As shown, the present invention provides a fixture for automatic processing of aero-engine blades, comprising a base plate 1, a base 2 and a tailstock 3 are respectively provided...

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PUM

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Abstract

The invention discloses a clamp for automatically machining aero-engine blades, which comprises a bottom plate, a base and a tailstock which are respectively arranged at the two ends of the upper side of the bottom plate, a tail ejection piece arranged at the upper end of the tailstock, a 3R base arranged at the upper end of the base, and a 3R positioning piece fixedly connected to one side of the 3R base, the other side of the 3R positioning sheet is sequentially connected with a flat plate, a concave plate, an L-shaped plate, a chuck mounting frame and a chuck mounted on the surface of the chuck mounting frame; the chuck mounting frame rotates around the Z axis, moves along the X axis and the Y axis, is in positioning connection with the L plate through bolts, rotates around the Y axis, moves along the Z axis and the X axis, is in positioning connection with the concave plate through bolts, rotates around the X axis, moves along the Z axis and the Y axis, and is in positioning connection with the flat plate through bolts, so that the adjustment of six degrees of freedom of the chuck is realized; the positions of the chucks can be conveniently adjusted according to the clamping states of the blades, so that the clamping states of all the blades are completely consistent, and stable automatic machining is guaranteed.

Description

technical field [0001] The invention relates to the field of aero-engine blade processing, in particular to a fixture for automatic processing of aero-engine blades. Background technique [0002] Aero-engine is a highly complex and sophisticated thermal machine. As the heart of an aircraft, it is not only the driving force for aircraft flight, but also an important driving force for the development of aviation. Every important change in the history of human aviation is related to the technological progress of aero-engines. It is inseparable, because the aero-engine blade processing equipment is very expensive, and the depreciation of the machine tool is lost every second, so it must be run 24 hours to be fully and effectively used for production, and the night is the human sleep biological clock time, on the one hand, workers do not They are willing to work night shifts. On the other hand, even if workers are willing to work night shifts, they are prone to make mistakes. The...

Claims

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Application Information

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IPC IPC(8): B23Q3/06B23B23/00
CPCB23Q3/062B23B23/00Y02P70/50
Inventor 何正琛林盛
Owner CHENGDU AERONAUTIC POLYTECHNIC
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