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A multi-objective optimization method for brush seal structure

A multi-objective optimization and brush-type technology, applied in multi-objective optimization, genetic rules, prediction, etc., can solve the problems of reduced sealing performance and reduced wear resistance, and achieve small calculation load, high precision, and strong global search performance Effect

Inactive Publication Date: 2017-06-13
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the improvement of the sealing performance will be at the cost of reducing the wear resistance. For example, the increase of the diameter of the brush filament will reduce the wear, but it will cause the decline of the sealing performance. The increase of the number of brush filament layers will inhibit the leakage, but accelerate the wear

Method used

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  • A multi-objective optimization method for brush seal structure
  • A multi-objective optimization method for brush seal structure
  • A multi-objective optimization method for brush seal structure

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Experimental program
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Embodiment Construction

[0054] The brush seal multi-objective optimization method provided by the present invention will be described in detail below in conjunction with the figures and specific embodiments.

[0055] Step 1. Select the diameter of the brush filament, the number of layers of the brush filament, the protection height of the rear baffle, and the free height of the brush bundle as the parameters to be optimized for the sealing structure; determine the optimization range of the parameters to be optimized: the optimization range of the diameter of the brush filament is 0.09 to 0.2 mm, the optimal range of brush filament layers is 6-14 layers, the optimal range of tailgate height is 0.78-2.68 mm, and the optimal range of brush bundle free height is 2.64-15.14 mm.

[0056] Step 2, take the least leakage and the lowest wear as the optimization goals, give weights of 0.7 and 0.3 respectively, and construct the fitness function.

[0057] Step 3. According to the experimental scheme in Table 1, ...

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Abstract

The invention discloses a multi-objective optimization method of a brush seal structure. The multi-objective optimization method of the brush seal structure comprises the following steps: a to-be-optimized parameter of the seal structure is selected, and the optimization range of the to-be-optimized parameter is determined; a fitness function is constructed with the least leaking and the lowest wearing as optimization objectives; a variable working condition experiment is performed, and a data sample of a support vector machine is made; parameters of the support vector machine are trained on the basis of a training sample, and a support vector machine delegation model of the brush seal structure is established; the brush seal structure is optimized with a genetic algorithm, and the optimal value of the to-be-optimized parameter is determined. The multi-objective optimization method overcomes defects of existing single-objective optimization methods of the brush seal structure, the delegation model is high in precision, and the global optimization capacity is high, and the robustness is high.

Description

technical field [0001] The invention belongs to the technical field of brush seals, in particular to a multi-objective optimization method suitable for brush seal structures. Background technique [0002] Low fuel consumption, high thrust-to-weight ratio, high reliability and durability are the development trends of modern aviation gas turbine engines. However, the internal temperature and pressure ratio of the engine are increasing year by year, which makes the leakage problem of the internal flow system more and more serious. In order to reduce leakage loss and improve the overall performance of the engine, it is particularly important to use high-efficiency sealing devices. The brush seal technology has gradually developed and matured since the early 1980s. It is a new type of sealing technology with excellent performance. Under the same conditions, the leakage level of the brush seal is only 50% of the typical grate seal structure. Even 20-10%. Therefore, only changing...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50G06N3/12G06Q10/04
CPCG06F30/17G06F2111/06G06N3/126G06Q10/04
Inventor 王春华张靖周周君辉
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS