Fluid machinery checking method
A fluid machinery and calibration technology, applied in computer-aided design, instrumentation, geometric CAD, etc., can solve problems such as lack of calculation accuracy, and achieve the effect of reducing the number of iterations, optimizing design, and improving reliability
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Embodiment 1
[0179] According to a specific embodiment of the present invention, the fluid domain calculation method of the present invention will be described in detail below.
[0180] Import the fluid domain grid into the fluid dynamics calculation software for fluid domain calculation, and obtain the aerodynamic parameters of the fluid domain; wherein, the time for the rotor to rotate through a blade channel is divided into multiple discrete time steps;
[0181] The fluid domain calculation includes the following steps:
[0182] Preset the total pressure value and the total temperature value of the equipment inlet in the software;
[0183] Preset the static value of the outlet of the equipment in the software;
[0184] Set the working medium as water or gas;
[0185] Given the speed of different working conditions, the speed range is 30% to 120% of the design working conditions;
[0186] The turbulence model selects the RNGκ-ε model;
[0187] Using the three-dimensional compressible...
Embodiment 2
[0212] According to a specific embodiment of the present invention, the calculation method of the solid domain of the present invention will be described in detail below.
[0213] The solid domain grid is imported into the solid mechanics calculation software for solid domain calculation, and the rotational speed of different working conditions is given to obtain the centrifugal prestress distribution of the blade.
[0214] Solid domain calculation includes the following steps:
[0215] Set the shaft part as fixed;
[0216] Set the working speed;
[0217] Using the implicit dynamic analysis method, the finite element discrete method is used to solve the governing equations, and the centrifugal prestress distribution of the blade is calculated.
[0218] The calculation of blade bearing centrifugal prestress distribution includes the following steps:
[0219] The mass of the blade is obtained according to the geometric and physical three-dimensional model of the blade and the...
Embodiment 3
[0228] According to a specific embodiment of the present invention, the calculation method of the air flow alternating stress distribution of the blade of the present invention under the prestressed state will be described in detail below.
[0229] According to the amplitude distribution field P of the pulsating flow field corresponding to the K-order exciting force on the surface of each blade k (x, y, z) and phase distribution field and the centrifugal prestress distribution of the blade, and the air flow alternating stress distribution of the blade under the prestressed state is obtained,
[0230] Specifically include the following steps:
[0231] S7100: The aerodynamic load P obtained in the form of amplitude and phase of each node calculated in S500 k (x, y, z) and Written in the form of real and imaginary parts;
[0232] S7200: According to the centrifugal prestress distribution of the blades calculated in S600, the surface pressure of the fluid domain is mapped to...
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