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A method for automatic spraying of guide vane components by dual robots

A technology of guide vanes and automatic spraying, which is applied to the device, coating, spraying device and other directions for applying liquid to the surface. It can solve the problem of different parameters such as the moving speed of the spray gun and the spraying distance, and cannot guarantee the consistency of the coating quality of the blade. and other problems, to achieve the effect of good coating quality consistency, high efficiency and strong flexibility

Active Publication Date: 2018-01-16
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, manual spraying is affected by the experience and subjective initiative of the operator, and the parameters such as the moving speed of the spray gun and the spraying distance vary, and the quality and consistency of the coating of each blade cannot be guaranteed.

Method used

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  • A method for automatic spraying of guide vane components by dual robots
  • A method for automatic spraying of guide vane components by dual robots
  • A method for automatic spraying of guide vane components by dual robots

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Embodiment Construction

[0045] The method for automatic spraying of the guide vane assembly by dual robots proposed by the present invention comprises the following steps:

[0046] (1) See attached figure 1 and 2 , the spraying procedure of the guide vane is divided into three parts: the upper edge plate, the lower edge plate and the blade body;

[0047] See attached figure 1 , Division of the upper and lower edge plate areas: Since the upper and lower edge plate spraying areas are irregular surfaces, they are divided into five areas according to their structural characteristics and relevant requirements of the design drawing: ① The gap area between the two blade bodies, namely the rear The area surrounded by the blade basin edge of the left blade body, the blade back inlet edge of the right blade body when viewed from the back, the tangent line between the vertices of the inlet edges of the two blade bodies and the end of the blade back inlet edge of the right blade body when viewed from the rear,...

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Abstract

The invention provides a method for automatic spraying of a guide vane assembly by a double robot, which is characterized in that it comprises the following steps: dividing the spraying program of the guide vane into three parts: an upper edge plate, a lower edge plate and a blade body Part; upper and lower edge plate area division: because the upper and lower edge plate spraying area is an irregular surface, it is divided into five areas according to its structural characteristics and relevant requirements of the design drawing: ①The gap area between the two blade bodies, namely The area surrounded by the blade basin edge of the left blade body in rear view, the blade back inlet edge of the right blade body in rear view, the line connecting the vertices of the two blade body inlet edges and the tangent line at the end of the blade back inlet edge of the right blade body in rear view , ②The basin area of ​​the right leaf body as viewed from the rear, that is, the area surrounded by the extension line connecting the edge of the basin of the right leaf body and the vertices of the air inlet edges of the two blade bodies as viewed from the rear.

Description

Technical field: [0001] The invention belongs to the surface coating protection technology, and relates to a method for automatic spraying of a guide vane assembly by a double robot. Background technique: [0002] As the core component of the engine, the turbine guide vane assembly of the aero-engine is sprayed with NiCrAlY bonding layer and thermal barrier coating surface layer on its surface. The structure of the guide vane assembly is double-mounted blades, which are divided into upper edge plate, lower edge plate, rear-view left blade body and rear-view right blade body. The shape can be divided into the leaf pot and the leaf back. There is mutual interference and shielding between the left and right leaf bodies and the upper and lower edge plates, and the structure is very complicated. Restricted by the part structure, the factory has been spraying the NiCrAlY bonding layer by hand for a long time. However, manual spraying is affected by the experience and subjective ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B05D7/14B05B13/04
Inventor 胡江波王斌利张会盈姚妮彭露黄宝庆原红星李建军
Owner AECC AVIATION POWER CO LTD
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