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A design method and system for near-net-shape blade fixtures for aeroengines

An aero-engine and near-net-shaping technology, which is applied in design optimization/simulation, calculation, graphics and image conversion, etc., can solve the problems of large demand for fixtures and the inability to realize fixture design and layout optimization, and achieve low-cost effects

Active Publication Date: 2022-05-20
TSINGHUA UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, in the processing of blades, due to the large number of blades, the demand for fixtures is large, and it will be a very difficult job to design and analyze the corresponding fixtures for each type of blade
The existing technology cannot realize the computer-aided rapid design system and method for fixture design and layout optimization oriented to adaptive processing technology system

Method used

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  • A design method and system for near-net-shape blade fixtures for aeroengines
  • A design method and system for near-net-shape blade fixtures for aeroengines
  • A design method and system for near-net-shape blade fixtures for aeroengines

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Embodiment 1

[0086] refer to figure 1 In this embodiment, it is embodied as a function module developed based on MATLAB language, and its main functions are described as follows: the present invention can realize the task of tooling design for new blades, and match it with existing tooling cases similar to blades through algorithms, based on The blade mesh affine transformation method realizes the geometric mapping relationship between the case blade and the target blade, based on the geometric relationship between the two, the inheritance of the tooling information of the case blade is realized, and finally the fixture layout information and fixture structure characteristics of the target blade are formed. Specifically, the following steps are included:

[0087] 1) Refer to figure 2 , to establish a case blade tooling database.

[0088] 1.1) Import the scanning model of the near-net shape blade of the aeroengine into the CAD software;

[0089] 1.2) According to the production experien...

Embodiment 2

[0106] The present embodiment provides a design system for aero-engine near-net-shape blade fixtures, which includes: a database building module, used to establish a case blade tooling database; a similar case blade determination module, used to adopt a similarity matching method, from the construction Find the case blade similar to the target blade in the case blade tooling database; the mechanical structure 3D model determination module is used to determine the 3D model of the mechanical structure in the target blade fixture based on the optimal tooling fixture model corresponding to the similar case blade; the 3D layout point The determination module is used to perform spatial projection on similar case leaves and target leaves, obtain two-dimensional plan information of target leaves and similar case leaves, and perform affine transformation and Inverse transformation to obtain the layout of the three-dimensional positioning points and clamping points of the target blade; t...

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Abstract

The invention relates to a design method and system for a near-net-shape blade fixture of an aero-engine, which includes: 1) establishing a case blade tooling database; 2) finding a case blade similar to a target blade from the constructed case blade tooling database; 3) Determine the three-dimensional model of the mechanical structure of the target blade fixture based on the optimal tooling fixture model corresponding to the similar case blade; 4) Perform spatial projection on the similar case blade and the target blade to obtain the two-dimensional plan information of the target blade and the similar case blade , and perform affine transformation and inverse transformation on the meshes of the target blade and similar case blades in the two-dimensional plane to obtain the three-dimensional positioning points and clamping point layout of the target blade; 5) based on the three-dimensional model of the mechanical structure in the target blade fixture and The 3D positioning point and clamping point layout of the target blade is used to obtain the final 3D model of the target blade fixture. The invention can be widely used in the field of aero-engine manufacturing.

Description

technical field [0001] The invention relates to the technical field of machining and manufacturing of aero-engine blades, in particular to a design method and system for a near-net-shape blade fixture of an aero-engine. Background technique [0002] Near-net-shape blades (including precision forging blades without allowance, precision cast blades without allowance, etc.) have become an important development trend of future aero-engine blade technology. Blade tip and tenon require secondary machining. [0003] In the secondary processing of the blade tenon, the adaptive processing technology combined with the flexible tooling fixture is currently used. The flexible tooling uses flexible elements to contact the blade body to protect the blade from being damaged by clamping. The adaptive processing technology is used for Compensate for blade position changes caused by flexible tooling. However, in the blade adaptive machining process, there are not only the overall deformatio...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/17G06F30/20G06T17/00G06T3/00
CPCG06F30/17G06F30/20G06T17/00G06T3/02
Inventor 王辉吴动波裴润森余杰张丽丽梁嘉炜周峰陈海瑛
Owner TSINGHUA UNIV