Integrated Measurement of Center of Gravity and moment of inertia of Aeroengine

La description

Engine adaptation weight range: **0g****0kg;
The error of weight measurement was ±(1kg FS/0.5kg FS);
distance: ±(3.0mm/2.0mm);
the comprehensive accuracy of weight and center of gravity was better than 1 ‰ (according to HB******4);
System safety overload capacity: **5;
system limit overload capacity: **0;
maximum load of turntable (kg): ********0;
range of measurement (kg.m2): **0m****0;
measuring accuracy: ±0.5;
Pretwist mode: electric / manual;
turntable preset size (φ × H): φ **0 × *0;
power supply: AC **0V ±*0);
environmental temperature: **0 ℃ ~ + *5 ℃;
environmental humidity: ≤ *0RH;
Test engine diameter range: **0~***0mm (adjustable);
5 front, rear support (Wnl/Wnr, Wml/Wmr) lateral maximum movement range: left and right **0mm (preset);
The maximum longitudinal movement range of front / rear brace is **0~***0mm (preset), and the external dimension of platform (L × W × H): ***0 × ***0 × **0mm). *3