Aluminium profile 40x80 10mm slot black anodised

Reference 6-ASN-10-4080-SA

€34.90 Tax excluded

Quantity

126 bars of 4180 mm in stock - Usual processing time: 2 to 4 working days

Aluminium profile 40x80 10mm slot black anodised

Important information: the black anodized finish is very sensitive to scratches. For this reason, and despite all the precautions we take when handling them, it is possible that the product delivered has this type of defect.

Reference 6-ASN-10-4080-SA

Data sheet

Slot type: B Type
Second moment of inertia (x10^4 mm^4) (y axis): 72.6
Second moment of inertia (x10^4 mm^4) (x axis): 19.9
Linear mass density (kg/m): 2.79
Cross section (mm²): 1036
Cross section (mm): 40x80
Number of slots: 6
Size of slot: 10
Finish: Black anodised
Central hole diameter: 10,5 mm (for M12 thread)
Main material: Aluminium EN AW-6063-T5
Colour: Black
Sold by: Custom Length
Cutting tolerance: +/- 1 mm
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)

Maximum deformation recommended for your assembly:

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	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 2	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 3	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 4	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 5	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 6	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 7	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 8	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) in Kg
Mouting 9	Deformation δ (x axis): in mm Deformation δ (y axis): in mm	Max load (x axis) in Kg Max load (y axis) 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	Max load: in Kg
Assembly 2: for a recessed beam - movable recessed (along the vertical axis)	Max load: in Kg
Assembly 3: for a recessed-swivel beam	Max load: in Kg
Assembly 4: for a recessed-free beam	Max load: in Kg