System and Method for Automatic Mesh Division of Steam Turbine Rotor
A steam turbine rotor, automatic division technology, applied in the direction of instrument, geometric CAD, design optimization/simulation, etc., to meet the requirements of rotor strength design, good calculation accuracy, and easy for secondary development.
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specific Embodiment approach 1
[0056] Turbine rotor mesh automatic division system, including:
[0057] The rotor model feature acquisition module automatically collects and imports the feature information of the rotor model, including the coordinates of each end point of the rotor model, the length and angle of each feature side, and other feature information;
[0058] The eigenvalue analysis module numbers each characteristic edge and characteristic node and classifies the characteristic edges according to the characteristic coordinates, and at the same time obtains the length information of each characteristic edge, and compares the length n of each characteristic edge with the length n of the preceding characteristic edge 2 , the length of the rear feature side n 3 Compare to get the pre-feature ratio post feature ratio
[0059] Feature side distribution module, the pre-feature ratio R 1 and post-characteristic ratio R 2 Enter the logic library to find the most suitable seeding method, and contro...
specific Embodiment approach 2
[0076] The method for automatically dividing the grid of the steam turbine rotor includes the following steps:
[0077] Step 1. Apply modeling software such as UG to establish a rotor model;
[0078] Rotor models with different properties can be established according to the rotor form. For T-shaped blade roots and double-T-shaped blade roots, a two-dimensional axisymmetric model can be established, and for a palm-shaped leaf root, a three-dimensional circular symmetric model can be established; the established The rotor model is stored in stp format and imported into the steam turbine rotor mesh automatic division system;
[0079] Step 2, feature classification and feature value analysis:
[0080] Step 2.1, automatically collect the characteristic information of the imported rotor model, including the coordinates of each end point of the rotor model, the length of each characteristic side, angle and other characteristic information;
[0081] Step 2.2. Number each characteris...
specific Embodiment approach 3
[0103] The limiting maximum deviation factor described in step 2 of this embodiment is 0.1.
[0104] Other steps and parameters are the same as in the second embodiment.
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