An Algorithm for Surface Spraying Trajectory of Gas Turbine Components
A technology for gas turbines and components, applied in manipulators, program-controlled manipulators, manufacturing tools, etc., can solve problems such as collision accidents, difficulty in guaranteeing, and inability to guarantee coating quality, and achieve the effects of improving quality, improving spraying efficiency, and uniform thickness
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0114] Such as Figure 1-3 As shown, a gas turbine component surface spray trajectory algorithm includes the following steps:
[0115] A, initial partition: such as image 3 Distance
[0116] (1), take any vertical vertical interception in an irregular surface, and take N points (P11-P1n) to the N-1 line segment on this intercept, take points to ensure the neighbor. The surface of the surface is close to the plane;
[0117] (2), the N points taken before the previous interception are the starting points to be divided into N-rooted interception, respectively, and each transverse interception is separately taken, and the starting point, closed curved surface. The starting point and the end point are the same point), split into M root line segment, and the lateral point is also guaranteed to ensure that the surface between the adjacent two points is close to the plane;
[0118] (3), to this, the surface is collected a total of N * M points (P11-PMN) to form an approximate planar region...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


