Turbine blade interval damage tolerance analysis method

A technology of turbine blades and analysis methods, applied in the field of turbine blades, can solve problems such as lack of experimental data

Active Publication Date: 2019-08-02
HUNAN UNIV
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Problems solved by technology

Probabilistic damage tolerance can better make up for this defect, especially when it comes to the high-precision and high-cost structure of aero-engine turbine blades, but due to the lack of experimental data, it is usually difficult to construct an accurate probability density function of parameters for probabilistic damage tolerance analysis

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  • Turbine blade interval damage tolerance analysis method

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Embodiment Construction

[0056] Aiming at the lack of samples, the invention proposes an interval analysis method for the crack propagation life. Since in the crack structure, some parameters are correlated, such as two crack growth rate constants, while some parameters are independent parameters, such as load and crack size, etc., a novel parallelepiped model is introduced in the method to simultaneously contain It is measured when the relevant interval parameters contain independent interval parameters. Through the parallelepiped model, most of the relevant interval parameters will be unified and normalized into an independent standard hypercube. In this standard space, the upper and lower boundaries of the fatigue crack growth life of the turbine blade are predicted by using the subinterval analysis method.

[0057] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0058] Step 1: Firstly, a deterministic three-dimensional...

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Abstract

The invention relates to a turbine blade interval damage tolerance analysis method, and provides an interval analysis method for crack propagation life under the condition of sample shortage. In the crack structure, a novel parallelepiped model is introduced in the method to measure the situation that relevant interval parameters and independent interval parameters are contained at the same time due to the fact that part of the parameters are correlated, such as two crack growth rate constants, and part of the parameters are independent parameters, such as loads and crack sizes. Through the parallelepiped model, most relevant interval parameters are unified and normalized into an independent standard hypercube, and in the standard space, the upper and lower boundaries of the fatigue crackpropagation life of the turbine blade are predicted by adopting a subinterval analysis method. According to the method, independent and related interval variables can be considered at the same time, the problem of large uncertainty of parameters is solved, and engineering practicability of turbine blade damage tolerance uncertainty analysis is promoted.

Description

technical field [0001] The invention relates to a turbine blade of an aero-engine, in particular to a damage tolerance analysis method for a turbine blade section based on a sub-interval method. Background technique [0002] Turbine blades are the core components of aero-engines, gas turbines, etc. They rotate at high speed under the action of high-temperature and high-velocity gas. The turbine blades are subjected to strong gas thrust and bending stress. Repeated frequent start-stop and variable-condition operation make Turbine blades are prone to fatigue fractures in an alternating stress environment, and it is very important to conduct damage tolerance analysis to ensure their safe operation. In the service environment, the blade is usually affected by uncertain factors, and the crack growth life is no longer a definite value. These uncertain factors must be taken into account in the damage tolerance analysis to ensure the safety of the structure. Probabilistic damage to...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F2119/04G06F30/20Y02T90/00
Inventor 姜潮龙湘云刘凯李玮鹏
Owner HUNAN UNIV
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