Cone-free neck flange intensity checking method
A strength check and flange technology, applied in the direction of strength characteristics, measuring devices, instruments, etc., to achieve the effect of solving inaccurate design
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specific Embodiment approach 1
[0030] Specific implementation mode one: combine figure 1 and figure 2 Describe this embodiment, a method for checking the strength of a flange without a taper neck in this embodiment, including the following steps:
[0031] Strength verification method for non-taper neck flanges without external loads:
[0032] According to the design method of the pressure vessel design standard GB150.3 flange, the thickness of the flange is initially estimated according to the calculation method of the integral flange, and then the strength of the dangerous section of the flange is checked according to the following steps.
[0033] Method for checking the strength of a-a section:
[0034] The aa section bears two-way stress, and the bending stress σ generated by the flange stud force W am and the shear stress τ due to the flange stud force W a
[0035] At this time, the bending stress of the a-a section has stress concentration due to the structural mutation, and its stress concentrat...
specific Embodiment approach 2
[0179] Specific embodiment two, combine figure 1 and figure 2 Describe this embodiment, this embodiment proposes a flange with external load (bending moment, torque, radial thrust, axial tension) without taper neck (see Figure 5 ) strength checking method
[0180] Explanation of the strength check and design method of the flange bearing external load:
[0181] 1. There are four types of external loads on the pipe flange: 1) Bending moment M; 2) Torque T; 3) Radial thrust V; 4) Axial force N.
[0182] 2. In the accompanying document Figure 5 For example, there are ±My, ±Mz for bending moment; ±Tx for torque; ±Vz, ±Vy for radial thrust; ±Nx for axial force.
[0183] 3. The above M and V external loads may have values in both directions. When both external load values are given, they can be combined for calculation, for example, Mx and My values are given. Then the composite M value is:
[0184] The thrust V is similar to this.
[0185] 4. Torque T and axial for...
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