A Method for Static Balance Correction of Aviation Tire
An aviation tire and calibration method technology, applied in static/dynamic balance testing, measuring devices, instruments, etc., can solve the problems of damage to the tire inner layer, time-consuming, labor-consuming, material, safety accidents, etc., and achieve the effect of easy operation.
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[0031] as attached figure 1 , attached figure 2 , attached image 3 , attached Figure 4 As shown, the tire specification is H44.5×16.5-21, the tire inflation diameter D=111.75cm, the inflation section width W=40.9cm, the rubber density d=1.1g / cm 3 . According to the calculation formula M=0.00383D2 (N.cm), it is calculated that the tire of this specification allows the maximum static balance difference Mmax=47.83N.cm, and the maximum allowable static unbalance weight Gmax=87.3g.
[0032] Use the aviation tire static balance testing machine to measure the "light spot" position A of the tire, the static balance difference M = 54.75N.cm, measure or calculate the static unbalanced weight G = 100g, at the measured "light spot" Mark the light point mark L near the bead. The point of symmetry between the "light point" position A and the tire axis O is the "key point" B of the tire.
[0033] The difference between the measured or calculated static unbalanced weight and the maxi...
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