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A method and device for grinding an end face in an eccentric cavity

A technology of inner end face and cavity, which is used in grinding/polishing equipment, machine tools suitable for grinding workpiece planes, grinding machines, etc. It can solve the problems of difficult forming and inability to process inner end faces, and achieve the effect of improving processing efficiency.

Active Publication Date: 2021-09-28
CHINA HANGFA SOUTH IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

But because the area of ​​the circular hole 102 is smaller than the area of ​​the inner end surface 103 (104) of the cavity 101, for example, when taking the axis of the circular hole 102 as a reference, the diameter of the circular hole 102 is Φ50mm, and The maximum diameter of the cavity 101 is Φ90mm, so when the grinding machine adopts the conventional grinding method, after the grinding wheel passes through the circular hole 102, it can only process the end face of the Φ50mm range based on the axis of the circular hole 102. The inner end faces at other positions cannot be machined
Therefore, in the existing processing method, it needs to go through multiple processes, and it is difficult to process and shape the inner end surface 103 (104) of the cavity 101 at one time.

Method used

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  • A method and device for grinding an end face in an eccentric cavity
  • A method and device for grinding an end face in an eccentric cavity
  • A method and device for grinding an end face in an eccentric cavity

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Embodiment Construction

[0024] In order to understand the technical features, objects, and effects of the present invention, specific embodiments of the present invention will be described with reference to the drawings. Wherein, the same components use the same reference numerals.

[0025] figure 1 Schematic diagram of stereoscopic structural schematic of a small and medium-sized aero-engine figure 2 A stereoscopic structure principle of an eccentric cavity in an eccentric cavity in an eccentric cavity in accordance with an embodiment of the present invention; image 3 for figure 2 Schematic diagram of the principle of stereo decomposition structure; Figure 4 for figure 2 Schematic of the principle of cross-sectional structure; Figure 5 for Figure 4 A partial cross-sectional configuration principle of the device in a direction. See Figure 1-5 As shown, the present invention provides an eccentric cavity inner end surface grinding method for the grinding of the cavity 101 in the axial end surface 103 (104...

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Abstract

A method for grinding an end face in an eccentric cavity, which includes the following steps, step A, providing a base with a cylindrical hollow structure, the base includes a bottom surface for contacting with the chuck of a grinding machine in the axial direction and a bottom surface for carrying the The top surface of the shaft-like parts, the top surface is provided with an eccentric hole, the shaft-like parts are assembled in the eccentric hole Step B, the base is installed on the chuck of the grinding machine, the type The two inner end faces of the cavity are ground. Step C, after completing the grinding process of the inner end surface of one cavity in step B, repeat the steps of step B to complete the grinding process of the inner end surface of the second cavity. In step D, the operations of step B and step C are repeated until the inner end faces of all the cavities are ground. The method for grinding the inner face of an eccentric cavity provided by the present invention greatly improves the processing efficiency. The present invention also provides a device used in the above method.

Description

Technical field [0001] The present invention relates to the field of machining, and in particular, to a method and apparatus for grinding the inner end surface of the eccentric cavity of the disk shaft. Background technique [0002] figure 1 Schematic diagram of stereoscopic structural schematic of a small and medium-sized aero-engine type part; see figure 1 As shown, the structure of the component 100 is a disk shaft type structure, and four radial penetration cavities 101 are disposed in the circumferential direction of the disc, and the cavity 101 has an axial direction in the axial side walls. The circular hole 102 is provided between the two adjacent two of the same radial plane, and is provided with an alleviation hole 105, i.etertering it, the disk body is all in both sides of the axial side. There are four mitigation holes 105, and the roughness of the two inner end faces 103 (104) of the axial direction of the cavity 101 is Ra0.4, and there is a verticality requirement ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B24B1/00B24B7/10
CPCB24B1/00B24B7/10
Inventor 鲁攀尹斯杰许小妮
Owner CHINA HANGFA SOUTH IND CO LTD