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Standard profile D28
P28-01A
€5.90
Tax excluded
Standard profile D28
Standard profile D28
P28-01A
Data sheet
- Second moment of inertia (x10^4 mm^4) (y axis)
- 1.18
- Second moment of inertia (x10^4 mm^4) (x axis)
- 1.18
- Linear mass density (kg/m)
- 0.414
- Cross section (mm²)
- 148.75
- Finish
- Transparent grey anodised
- Main material
- Aluminium EN AW-6063-T5
- Sold by
- Custom Length
- Cutting tolerance
- +/- 1 mm
- Manufacturing tolerances
- According to EN 755-9
- Customs Code
- 76042100
The results are given for information only and Systéal declines any responsibility concerning the use of this module.
Please note: this simulator currently only works with aluminum profiles. Do not use it for other materials and for plates.
Step 1: Fill in your data
| Load (P) | in Kg | Distance a | in mm |
| Length L | in mm | Length (m) | in mm |
| Young's modulus | N/mm² |
Step 2: Calculate the result (don't forget to update after each change in value)
Step 3: Determine your assembly and its admissible load
The recommended maximum load is the load corresponding to the maximum deformation recommended by the manufacturer (1 / 1000th of the length of the beam)
| in mm |
How to read the results? :
your mounting is not recommended because the deformation will be too high. Reduce the load or improve your assembly. the deformation is less than the maximum load. Your assembly is correct.
Mouting 1 |
in mm in mm | in Kg in Kg |
Mouting 2 |
in mm in mm | in Kg in Kg |
Mouting 3 |
in mm in mm | in Kg in Kg |
Mouting 4 |
in mm in mm | in Kg in Kg |
Mouting 5 |
in mm in mm | in Kg in Kg |
Mouting 6 |
in mm in mm | in Kg in Kg |
Mouting 7 |
in mm in mm | in Kg in Kg |
Mouting 8 |
in mm in mm | in Kg in Kg |
Mouting 9 |
in mm in mm | in Kg in Kg |
The results are given for information only and Systéal declines any responsibility concerning the use of this module.
Please note: this simulator currently only works with aluminum profiles. Do not use it for other materials and for plates.
Step 1: Fill in your data
| Load (P) | in Kg | Length (L) | in mm |
| Young's modulus | N/mm² |
Step 2: Calculate the result (don't forget to update after each change in value)
Step 3: Determine your assembly and its admissible load
The critical buckling load (= maximum load) is calculated using Euler's formula.
More information here.
How to read the results? :
your mounting is not recommended because the critical buckling load has been exceeded. Reduce the load or improve your assembly. the critical load is not exceeded. Your assembly is correct.Assembly 1: for a swivel beam at both ends |
in Kg |
Assembly 2: for a recessed beam - movable recessed (along the vertical axis) |
in Kg |
Assembly 3: for a recessed-swivel beam |
in Kg |
Assembly 4: for a recessed-free beam |
in Kg |
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