Auxiliary recognition method for gas turbine hole inspection component based on virtual reality technology

A technology of virtual reality technology and recognition method, which is applied in the field of non-destructive testing, and can solve problems such as the inability to quickly identify component structures and assembly features

Pending Publication Date: 2022-02-22
HUANENG POWER INTERNATIONAL +1
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0006] The purpose of the present invention is to provide an auxiliary identification method for gas turbine hole inspection parts based on virtual reality technology in order to solve the problem that the component structure and assembly features cannot be quickly identified during the gas turbine hole inspection.

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  • Auxiliary recognition method for gas turbine hole inspection component based on virtual reality technology
  • Auxiliary recognition method for gas turbine hole inspection component based on virtual reality technology
  • Auxiliary recognition method for gas turbine hole inspection component based on virtual reality technology

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Embodiment Construction

[0026] In order to make the objects, technical solutions, and advantages of the present invention, the present invention will be further described in detail below with reference to the accompanying drawings.

[0027] Refer to the attachment figure 1 A flow chart of a auxiliary identification method provided by a virtual reality technique of a virtual reality technology, wherein the characteristics are processed in the following steps:

[0028] Step 1: Generate the original model library in the shape and assembly data of the combustion engine component and assembly of the forward design or reverse mapping;

[0029] Step 2: Import analysis module in real-time pylo image data when the actual aperture inspection of the combustion engine is introduced;

[0030] Step 3: Characteristic analysis and extraction of components in the analysis module, generate digital characteristics;

[0031] Step 4: According to the digital characteristics, the corresponding model map is matched from the or...

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Abstract

The invention discloses an auxiliary recognition method for a gas turbine hole inspection component based on a virtual reality technology. The method comprises the following steps of: 1, generating an original model library by using the shape and assembly data of a gas turbine component subjected to forward design or reverse surveying and mapping; 2, importing real-time hole inspection image data of the component of the gas turbine during actual hole inspection inspection into an analysis module; 3, performing feature analysis and extraction on the real-time hole inspection image of the component in an analysis module to generate a digital feature map; 4, matching a corresponding model map from the original model library according to the digital feature map, and generating a virtual three-dimensional image of the component; and 5, superposing a virtual three-dimensional image on the real-time hole inspection image, and attaching auxiliary prompt information such as component names, assembly and orientation features. According to the method, the problem that the component structure and the assembly characteristics cannot be quickly identified during hole inspection of the gas turbine at present is solved, the hole inspection efficiency of the gas turbine component is greatly improved, the reliability of the result is ensured, and technical support is provided for safe operation of a unit.

Description

Technical field [0001] The present invention belongs to the technical field of non-destructive detection, and is specifically a virtual reality technology, auxiliary recognition method based on a virtual reality technology. Background technique [0002] The aperture inspection refers to the use of specialized aperture equipment, and enters the relevant components inside the combustion engine by the reserved hole detection, and effectively mastered and evaluate the combustion engine through the reserved hole detection. Service quality and health status of each component. Regularly controlling the regularity of the combustion machine is a must-have means of safeguarding the security of the unit, and is one of the key links of the daily operation and maintenance of the combustion engine. [0003] Since the number of components in the internal parts of the combustion engine is complicated, when the assembly structure is complicated, there is a case where the structural characteristic...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06T7/00G06T19/00G06F30/17G06F30/20
CPCG06T7/001G06T19/006G06F30/17G06F30/20G06T2207/10068G06T2207/30164
Inventor 李永君肖俊峰张炯高斯峰唐文书南晴高松
Owner HUANENG POWER INTERNATIONAL
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