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Forming method for semi-closed complex deep inner cavity of sealing disc

A forming method and a semi-closed technology, applied in the field of mechanical processing, can solve the problems of low machine stress, large machine chatter, and large machine stress, so as to improve the service life of anti-fatigue, solve the problem of large machine stress, and solve the problem of The effect of large processing deformation

Active Publication Date: 2021-06-15
AECC AVIATION POWER CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to provide a sealing plate cantilever installation side semi-closed complex deep inner cavity forming method, which solves the existing processing method of the cantilever installation side semi-closed complex deep cavity of the sealing plate made of powder superalloy FGH99 material The existing machine stress is large, the processing deformation is large, and the problem of large machine chatter occurs; therefore, the present invention provides a method for high temperature processing of difficult-to-process powders on the basis of low machine stress and small processing deformation. Forming and processing method of semi-closed complex deep inner cavity of alloy material sealing disc with large arc cantilever installation side

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  • Forming method for semi-closed complex deep inner cavity of sealing disc
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  • Forming method for semi-closed complex deep inner cavity of sealing disc

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Embodiment Construction

[0057] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0058] The invention is a forming processing method for semi-enclosed complex deep inner cavity of a large arc cantilever mounting side of a sealing plate of a powder superalloy material that is difficult to process on the basis of satisfying low machine stress and small processing deformation.

[0059] Such as Figure 1 to Figure 5 As shown, the present invention provides a method for forming a semi-closed complex deep inner cavity with a cantilever mounting side of the sealing plate, comprising the following steps:

[0060] Step 1. Divide the parts to be processed into five cutting areas, and select the cutting tools corresponding to the structures of each cutting area; The formed semi-closed and complex deep cavity 1 is divided into five cutting areas, namely, the face groove cutting area 2, the 45° concave cutting area 3, the 65° concave cutting area 4, ...

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Abstract

The invention provides a forming method for a semi-closed complex deep inner cavity of a sealing disc cantilever mounting edge. The forming method comprises the following steps that firstly, a to-be-machined part of a part is divided into five cutting areas, and cutters with structures corresponding to the cutting areas are selected, wherein the to-be-machined part of the part is the semi-closed complex deep inner cavity of the large arc cantilever mounting edge of the sealing disc; secondly, working procedures and cutting areas corresponding to the working procedures are formulated; and thirdly, a low-stress cutting path is planned, and cutting parameters are formulated. According to the forming method, the surface roughness of the part machined through the forming method reaches Ra1.6 microns-Ra2.3 microns, the surface appearance is good, meanwhile, the stress value of the part ranges from-45 Mpa to-82 Mpa, the stress is pressure stress, and the anti-fatigue service life of the part can be prolonged; and the deformation of the matching surface and the mounting surface of the part is controlled between -0.03 mm and +0.05 mm, and the deformation range from -0.05 mm to +0.1 mm allowed by the design is met.

Description

technical field [0001] The invention belongs to the field of mechanical processing, in particular to a sealing plate prepared from a powder superalloy FGH99 material, and relates to a forming method of a semi-closed complex deep inner cavity of the sealing plate. Background technique [0002] A new generation of domestic powder superalloy FGH99 was used for the first time as the material of a certain sealing plate. This material has a low machinability coefficient. Under the cutting conditions of the same specification and parameters, the cutting deformation of this powder superalloy is larger than that of ordinary superalloys (such as GH4169). . In terms of structure, compared with the previous models, the sealing plate has a semi-closed deep inner cavity structure formed by a large arc cantilever mounting edge and the sealing plate body at the front end. Due to the deep inner cavity and the structure Complexity and weak overall rigidity make it difficult to plan low-stres...

Claims

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Application Information

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IPC IPC(8): B23D79/00
CPCB23D79/00
Inventor 李林燊夏野鲁斌常广利俞树霆
Owner AECC AVIATION POWER CO LTD