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Simulation-based parameter optimizing method for precise casting process of single crystal turbine blade

A technology of process parameter optimization and turbine blades, which is applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of poor optimization effect and achieve the effect of improving the optimization effect

Inactive Publication Date: 2012-12-12
NORTHWESTERN POLYTECHNICAL UNIV
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AI Technical Summary

Problems solved by technology

[0005] In order to overcome the disadvantages of poor optimization effect of existing single crystal turbine blade precision casting process parameter optimization methods, the present invention provides a simulation-based single crystal turbine blade precision casting process parameter optimization method

Method used

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  • Simulation-based parameter optimizing method for precise casting process of single crystal turbine blade
  • Simulation-based parameter optimizing method for precise casting process of single crystal turbine blade
  • Simulation-based parameter optimizing method for precise casting process of single crystal turbine blade

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Embodiment Construction

[0033] The following examples refer to Figure 1-7 .

[0034] Step 1: Use a certain type of turbine power blade, the main parameters of which are blade body length 106.10mm, maximum chord length 56.21mm, maximum inscribed circle radius 5.7mm, leading edge radius 4.12mm, and trailing edge radius 1.25mm. The blade is made of the second generation single crystal superalloy DD6, and the mold shell is made of silica sand. According to casting feeding theory and actual production experience, the blade casting process and gating system are designed for power blades, using top injection, 2 pieces in a set.

[0035] Step 2: Use commercial finite element pre-processing software Hypermesh (product of Altair, USA) to divide the model into units based on non-uniform mesh division technology. First, import the gating system model into Hypermesh and discretize it into tetrahedral units. The quality meets the quality requirements of general enterprise finite element analysis. In this embodi...

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Abstract

The invention discloses a simulation-based parameter optimizing method for a precise casting process of a single crystal turbine blade. According to the simulation-based parameter optimizing method, the technical problem of poor optimization effect of the precise casting process of the single crystal turbine blade is solved. The technical scheme provided by the invention is that the simulation-based parameter optimizing method comprises the following steps of: designing a casting system model of the single crystal turbine blade; carrying out unit division on the casting system model by adopting a finite element analysis method; obtaining a precise casting process parameter and a reasonable parameter change range which have greater influence on the dimensional precision of a precise casting blade molded surface by extracting and identifying precise casting process parameters through a single factor process test; carrying out numerical simulation on the casting process according to the established test table; estimating the deformation condition of a casting relative to the designed model by processing and analyzing the data; and gradually narrowing the search range of the parameter optimization of the precise casting process by establishing a BP (Back propagation) neural network model and adopting a small-step searching method. The optimization effect of the parameter optimization method for the precise casting process of the single crystal turbine blade is improved.

Description

technical field [0001] The present invention relates to a single crystal turbine blade precision casting process parameter optimization method, in particular to a single crystal turbine blade precision casting process parameter optimization method based on simulation. Background technique [0002] The complex hollow turbine blade is the core technology of the high thrust-to-weight ratio engine, the core component of the engine, and the easily broken and failed parts. Its performance level, especially its ability to withstand high temperatures, is an important symbol of the advanced level of a type of engine, and in a certain sense, it is also a significant symbol of the level of a country's aviation industry. Due to its complex internal cooling structure, high requirements for aerodynamic shape and dimensional accuracy, and long-term service under conditions of strong thermal shock and complex cyclic thermal stress, the structural design and manufacturing technology of hollo...

Claims

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Application Information

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IPC IPC(8): G06F17/50G06N3/02
Inventor 傅将威陈晨卜昆周丽敏乔燕董一巍邱飞高斌王鲁丁肖艺
Owner NORTHWESTERN POLYTECHNICAL UNIV
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