V-SLOT Aluminium profile C-BEAM 40x80 6mm slot

Reference C-BEAM-4080-VSLOT

€21.90 Tax excluded

Quantity

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

V-SLOT Aluminium profile C-BEAM 40x80 6mm slot

Warning: on this product, the tapping option adds 4 tapped holes on the selected side. This makes it possible to fix the end plate reference C-BEAM-END-PLATE

Reference C-BEAM-4080-VSLOT

Data sheet

Second moment of inertia (x10^4 mm^4) (y axis): 53.16
Second moment of inertia (x10^4 mm^4) (x axis): 11.22
Linear mass density (kg/m): 2.00
Cross section (mm²): 742
Cross section (mm): 40x80
Number of slots: 12
Size of slot: 6 mm (V-SLOT)
Finish: Transparent grey anodised
Rounded: No
Central hole diameter: 4,2 mm (for M5 thread)
Main material: Aluminium EN AW-6063-T5
Colour: Grey
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)

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