Unterschiede
Hier werden die Unterschiede zwischen zwei Versionen angezeigt.
| Beide Seiten der vorigen RevisionVorhergehende ÜberarbeitungNächste Überarbeitung | Vorhergehende Überarbeitung | ||
| en:berechnungen:festigkeitsberechnung [2024/10/17 20:17] – [Strength calculation] neelest | en:berechnungen:festigkeitsberechnung [2025/09/03 12:27] (aktuell) – [Shear Stress] neelest | ||
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| - | ======Strength calculation====== | + | ======Stress Analysis====== |
| - | ===== Strength | + | -> [[..: |
| - | The strength calculation determines the maximum load of the screw with the shear | + | ===== Equivalent Stress===== |
| - | stress hypothesis according to TRESCA: | + | |
| + | The strength calculation determines the maximum load on the screw using the shear stress hypothesis according to TRESCA: | ||
| $$σ_v = \sqrt {(σ_x - σ_y)^2 + 4τ_{xy}^2}$$ | $$σ_v = \sqrt {(σ_x - σ_y)^2 + 4τ_{xy}^2}$$ | ||
| - | The screw fails above this stress. The hypothesis | + | Since the rotation of the screw represents a purely torsional load, the hypothesis |
| - | of the screw generates only torsion | + | As bending of the screw can also be neglected, the normal stress in the y-direction |
| - | therefore just shear stress | + | $\sigma_y$ may likewise be disregarded. |
| - | calculated | + | The normal stress in the x-direction $\sigma_x$ therefore results solely from the pressures at the inlet and outlet |
| + | |||
| + | $$σ_v = \sqrt {σ_x^2 + 4τ_{xy}^2}$$ | ||
| + | |||
| + | The screw' | ||
| + | |||
| + | ===== Normal Stress===== | ||
| + | |||
| + | The normal | ||
| + | |||
| + | $$\sigma_x = \sigma_{x, | ||
| + | $$\text{with}$$ | ||
| + | $$\sigma_{x, | ||
| + | $$\text{and}$$ | ||
| + | $$\sigma_{x, | ||
| + | |||
| + | With the outer diameter $D$ and the screw core diameter $d$.\\ | ||
| + | The acting force results from the pressure and the projected area on which the pressure acts. It is assumed that the compressive | ||
| + | |||
| + | ===== Shear Stress===== | ||
| + | |||
| + | The shear stress | ||
| + | |||
| + | $$\tau_{nominal} = \frac{M_t}{W_t} = \frac{M_t \cdot a_{max}}{I_p}$$ | ||
| + | |||
| + | with the torque $M_t$, the section modulus $W_t$, the polar moment of inertia $I_p$ and the maximum perpendicular distance from the outer fiber to the neutral (stress-free) fiber $a_{max}$. | ||
| + | |||
| + | Another influencing factor for calculating the screw strength is the radius that describes the transition from the screw core to the flight. For this geometric influence, a shape factor (stepped round bar under torsion, DIN 743-2) is defined as: | ||
| + | |||
| + | $$\alpha_{\tau} = 1+ \frac{1}{\sqrt{3, | ||
| - | $$τ_{max} | + | with the radius at the flight |
| - | Another influencing | + | From the shape factor, the notch effect factor $\beta_{\tau}$ (DIN 743-2) can be calculated as: |
| - | indicates | + | |
| - | defined for this geometric influence: | + | |
| - | $$K_{t,f} = 1+ \frac{1}{\sqrt{3, | + | $$\beta_{\tau} = \frac{\alpha_\tau}{n}$$ |
| + | $$\text{with}$$ | ||
| + | $$n=1+\sqrt{G' | ||
| + | $$\text{and}$$ | ||
| + | $$G'=\frac{1,15}{r}$$ | ||
| - | In combination with the notch sensitivity number | + | The total influence factor |
| - | $$q = \frac{1}{1+ \frac{8mm}{r} \cdot (1- \frac{R_{p0,2}}{R_m})^3}$$ | + | $$K_\tau |
| + | $$\text{with}$$ | ||
| + | $$K_2(d)=1-0,2 \frac{log(d/7,5\,mm)}{log(20)} \text{ with } K_2(d> | ||
| - | it is possible in according to THUM to calculate | + | as well as with the influence of surface roughness |
| - | equation describes | + | The values apply up to a diameter of 25 mm and decrease linearly beyond this value down to 1.0 at a diameter of 40 mm. For diameters above 40 mm, the value remains constant at 1.0. |
| - | $$K_f = 1+ (K_t-1) \cdot q$$ | + | The resulting shear stress, taking into account these influencing factors, is given by: |
| - | Finally, the shape number | + | $$\tau_{xy} = \tau_{max}=\tau_{nominal} \cdot K_\tau$$ |
| - | maximum stress or rather the characteristic value oft he screw strength. | + | |
| + | ===Further topics=== | ||
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