Checking element 4 (upper tie rod) with MDESIGN

In the steps below, 🖱 means a left mouse click and → leads to the next action. Labels in the screenshots are those of the MDESIGN interface.

1. Calculation model and input data

Analysis model

Input data (Sec.3.2, Ex.3.2)

Forces: F_X = 1500 N, F_Y = 300 N, F_Z = 700 N.

Moments: M_X4 = 21000 Nmm, M_Y4 = 105000 Nmm.

Geometric parameters: X₁ = 80 mm; b₄ = 60 mm; h₄ = 15 mm.

Material: S235, weldable general-purpose steel.

Operating constraints: temperature T = (−30…40) °C.

Forces and moments in the MDESIGN xyz coordinate system

Forces: F_x = F_X = 1500 N, F_y = F_Y = 300 N, F_z = −F_Z = −700 N.

Moments: T_x = −M_X4 = −21000 Nmm, M_y = M_Y4 = 10500 Nmm.

2. Entering the data in MDESIGN (Annex.MD.1)

2.1 Launching the application

Launching the Beam module

🖱

→

🖱

→

🖱

Resetting the data of the automatically loaded application

🖱 → [🖱 select the command ] → [🖱 select the option ].

Saving the application

🖱 (, ) → : [ select the folder where the application will be saved],

[ enter the file name Element 4], [: ], 🖱.

Opening the application (if it was created and saved earlier)

🖱 → [🖱 select the command ] → [select the folder where the application is saved] → 🖱.

Note. While working, save intermediate versions regularly for safety (the system may freeze), using 🖱 or F10.

2.2 Selecting the Input window and general settings (Annex.MD.1)

Selecting the language

[🖱 select from the list the option ].

Selecting the Input page

Notes.

– the option is selected to view the results obtained after solving;

– the option is selected to view the input data.

General settings (selected from the attached lists)

2.3 Entering the geometric, technological, loading and material data (Annex.MD.1)

Entering data in the Beam geometry table

: 🖱 → 🖱 () → : select from the list 🖱, 🖱 → : 🖱 select from the list , 🖱 (data on the chosen section appear automatically in row 1) → : enter the bar length in the box , e.g. 80.

3D graphic view of the bar

🖱 ().

Note. The model can be manipulated with: 🖱 (, plane projection, 2D; , perspective view, 3D); 🖱 + 🖱 (to zoom in) or (to zoom out); 🖱 + drag to pan; + drag to rotate.

Entering the support data in the Bearings table

: 🖱, [enter the x value in the box , e.g. 0] → 🖱 () → : [🖱 select the icon for a fixed (clamped) support] →

🖱 ().

Entering the axial-force loading in the Axial Forces F_ax table

: 🖱, [enter the values in the boxes (the position, e.g. 0)], (the value, with a + sign in the direction of the x axis, e.g. 1500), (the radius, i.e. the distance from the X axis, e.g. 0), (the angle in the YZ plane, measured from the Y axis, e.g. 0).

🖱 ().

Entering the radial-force loading in the Radial Forces F_r table

: 🖱, [enter the values in the boxes (the position, e.g. 0)], (the value, with a − sign, opposite to the axis, e.g. −700/−300), (the angle in the XY plane, measured from the Z axis, e.g. 0/90).

🖱 ().

Entering the bending-moment loading in the Bending moments M_b table

: 🖱, [enter the values in the boxes (the position, e.g. 0)], (the value, with the appropriate sign, e.g. 10500), (the angle in the YZ plane, measured from the Z axis, e.g. 0).

🖱 ().

Entering the torsional-moment loading in the Torsion table

: 🖱, [enter the values in the boxes (the position), (the value of the torsional moment, e.g. −21000)] → (the length, e.g. 0)].

🖱 ().

Entering the material data

[select from the list 🖱 (the MDESIGN database)]

🖱 → : [select the row with the material ()], 🖱.

Entering the working temperature ()

[enter the value in the box , e.g. 40].

Entering the semi-finished product option ()

[select from the list , 🖱 ].

Meaning

T – Temperature (maximum working temperature); Material, surface hardened; Loads mainly crosswise to the preferred direction of machining (rolling).

3. Solving the model and saving the results

🖱

or 🖱 or F10

→

Correct any inconsistencies or errors in the input data (only if warning windows appear)

→

🖱

or 🖱 or F10

→ 🖱

→

Element 4.pdf

→ 🖱

4. Input data and results obtained (Annex.MD.3.6_4)

Selecting the Output page

Geometry data

Meaning

l_g – total length of the beam; m – total mass of the beam; x_s – position of the centre of gravity on the X axis; I_y – moment of inertia about the y axis; I_z – moment of inertia about the z axis; W_t – torsional section modulus; W_y – section modulus about the y axis; W_z – section modulus about the z axis; S_y – first moment of area about the y axis; S_z – first moment of area about the z axis.

Loading data

Axial-force loading

Radial-force loading

Bending-moment loading

Torsional-moment loading

Material data

Meaning

R_pN – yield strength; R_mN – ultimate tensile strength.

Support reactions

Meaning

Rigid Clamping – the fixed support; Position x – the position on the x axis; R_y – reaction force in the fixed support along the y axis; R_z – reaction force along the z axis; R – resultant reaction force in the transverse yz plane; R_x – reaction force along the x axis; Calculation results for point – the results calculated at point x; M_y – bending moment about the y axis; M_z – bending moment about the z axis; M_b – resultant maximum bending moment.

Bending moment values and diagrams

Note. The maximum bending moments are those at the support reaction (see above).

Meaning

Bending moment development (X–Y plane) – bending moment diagram in the XY plane; Bending moment development (X–Z plane) – diagram in the XZ plane; Bending moment development (resultant) – resultant bending moment diagram; Max. bending moment – the maximum bending moments; M_ymax – maximum bending moment about the y axis; M_zmax – maximum bending moment about the z axis; M_bmax – resulting maximum bending moment; Position; Amount (value).

Normal stress diagrams and maximum values

Bending stress diagrams

Maximum normal stress values

Maximum value of the normal stress

Meaning

Bending stress development (X–Y plane) – bending stress diagram in the XY plane; Bending stress development (X–Z plane) – diagram in the XZ plane; Bending stress development (resultant) – resultant bending stress diagram; Salient point – characteristic point of the section; Tension-pressure stress – tensile/compressive stress; Bending stress in consequence of M_ymax – bending stress due to M_ymax; Bending stress in consequence of M_zmax – bending stress due to M_zmax; σ_res – combined (resultant) normal stress; Stress of axial force F_X – stress due to the axial force F_X; Stress of bending moment M_Y – stress due to M_Y; Stress of bending moment M_Z – stress due to M_Z; σ_resmax – maximum resultant normal stress; Position; Amount (value).

Shear stress diagrams and maximum values

Shear stress diagrams

Shear stress values

Maximum value of the shear stress

Meaning

Shear stress development (X–Y plane) – shear stress diagram in the XY plane; Shear stress development (X–Z plane) – diagram in the XZ plane; Shear stress development (resultant) – resultant shear stress diagram; Salient point – characteristic point of the section; τ_z – shear stress due to F_Z; τ_y – shear stress due to F_Y; τ – stress due to the torsional moment; σ_res – combined (resultant) shear stress; Stress of radial force F_Y – stress due to the radial force F_Y; Stress of radial force F_Z – stress due to the radial force F_Z; Stress of torsion moment T_X – stress due to the torsional moment T_X; τ_resmax – maximum resultant shear stress; Position; Amount (value).

Equivalent stress and safety factor: values and diagrams

Meaning

σ_vx – equivalent stress development (resultant); σ_vxmax – maximum equivalent stress; S_F – safety against the yield point; S_Fmin – minimum safety factor against yielding.

Transverse displacements (deflections) and rotations: values and diagrams

Meaning

v – resultant transverse deflection; θ – resultant inclination (rotation); v_max – maximum resultant deflection; θ_max – maximum rotation (angle of the maximum deflection).

5. Checks

Check under combined loading

The check under combined loading aims to prevent permanent plastic deformation of the bar, based either on stresses,

σ_vmax ≤ σ_a,

or on safety factors,

c ≥ c_a,

where σ_vmax is the maximum equivalent stress, σ_a = σ₀₂/c_a the allowable stress against yielding (plastic deformation), σ₀₂ the yield strength and c_a the allowable (minimum) safety factor, which may be taken as c_a = 1.5…2.5; c = σ₀₂/σ_vmax is the minimum safety factor.

Applying the combined-loading check

σ_vmax ≤ σ_a; 35.073 < 117.5 MPa (satisfied),

or

S_Fmin ≥ c_a; 6.7 > 2 (satisfied).

Notes.

– Yield strength σ₀₂ = 235 MPa (see above, the Material Data section); the allowable safety factor was taken as c_a = 2.

– If the check is not satisfied, the cross-sectional dimensions of the segments must be increased.

Check of bending deformations (stiffness)

The deformation check is carried out to prevent linear and angular displacements that are unacceptable from a functional point of view, by comparing the maximum deflections and rotations with the allowable values:

v_max ≤ v_a,

θ_max ≤ θ_a,

where v_a is the allowable deflection and θ_a the allowable rotation. The allowable deformations recommended in the literature are v_a ≤ (0.002…0.03)l_max (l_max being the maximum length of the bar) for linear deformations, and θ_a = (0.5…1.5)° for angular deformations.

Applying the deformation (stiffness) checks

Linear deformations (deflections)

v_max ≤ v_a; 0.043 ≤ 1 mm (satisfied).

Angular deformations (rotations)

θ_max ≤ θ_a; 0.0496 ≤ 1° (satisfied).

Note. The allowable displacements were taken as v_a = 1 mm and θ_a = 1°.