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Small Tension and Compression Load Cell 1kg/3kg/5kg/20kg/200kg

This time we will introduce a small load cell. It is a tension and compression load cell for force measurement, such as automobile braking force detection.
Small tension and compression load cell 1kg - 200kg
Load cell specification:
Model
ATO-S-LCC-DYMH-103
Weight
0.1kg
Capacity
1kg, 2kg, 3kg, 5kg, 10kg, 20kg, 30kg, 50kg, 100kg, 150kg, 200kg
Accuracy
0.03%F.S (linearity + hysteresis + repeatability)
Sensitivity
1.0~1.5mV/V
Creep
±0.05%F.S/30min
Zero output
±1%F.S
Temperature effect on zero
±0.05%F.S/10℃
Temperature effect on output
±0.05%F.S/10℃
Operating temperature
-30℃~+70℃
Input impedance
400±10Ω
Output impedance
350±10Ω
Insulation resistance
≥5000MΩ
Safety overload
150%F.S
Overload limit
200%F.S
Bridge voltage
DC 10-15V, suggest DC 10V
Material
Stainless steel
Protection class
IP67
Cable length
2m
Wiring
EXC+: Red, EXC-: Black, SIG+: Green, SIG-: White
Load cell dimension:
Capacity
M
5kg, 10kg, 15kg, 20kg, 30kg, 50kg
M5
60kg, 100kg
M6
200kg
M8
The elastic element of tension and compression load cell measure the bending stress of the circular plate. Elastic element of tension and compression load cellStructural and mechanical characteristics of load cell elastic elements:
  1. Simple and compact structure, small volume, low height, and light.
  2. Circular appearance, easy to ensure high processing precision of dimensions, form and position.
  3. Large transverse stiffness and strong resistance against eccentricity and lateral load.
  4. An integrated circular and symmetric circular plate. Consistent in different directions of thermal expansion. Low temperature coefficient.
  5. Simple theoretical computing. The maximum deflection, W, is far smaller than the circular-plate thickness, h, under the effect of the external load, so the thin-plate small deflection bending theory is applicable. Capable of being simplified into the surrounding fixed support.
The central convex plate is a circular plate suffers the concentrated force, P. Using Lobo formula, and the following equation can be obtained:
Maximum stress:
Maximum deflection:
Where, K and K1 are the stress and deflection computing coefficient. According to the ratio of the circular-plate elastic elements' supporting marginal radius, b, to the central loading convex platform radius, a, the convex platform circular-plate stress and deflection computing coefficient, K and K1, can be obtained.

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