TCS-4500
Aircraft Weight and Center of Gravity Measurement System Solution
The aircraft weight and center of gravity measurement system is primarily used to accurately measure aircraft weight and center of gravity.
During operation, the aircraft is towed or pushed onto the system's weighing platform. Each weighing platform is equipped with high-precision load cells. The sensor signals are collected, converted, and processed by a high-performance digital module before being transmitted to a computer. Both wired and wireless transmission methods are available. The computer's weighing management software processes and calculates the received signals, displaying the weight of each wheel, the aircraft's gross weight, and the aircraft's center of gravity on the computer screen. During fuel dumping tests, a center of gravity curve can also be plotted.
a) Aircraft weight measurement;
b) Aircraft center of gravity calculation;
c) Plotting the aircraft's center of gravity change curve during the fuel dumping test;
d) Storage, query, and output of aircraft weight, center of gravity test data, and other parameters.
Table 1 System Components
The TCS-4500 aircraft weight and center of gravity measurement system consists of a front scale, a left scale, a right scale, a laptop computer (including measurement software), an approach bridge, a wheel blocker, and measurement accessories, as shown in Figure 1.
Figure 1 System Configuration
a) Input Power: 220 (1 ± 10%) VAC, 50 (1 ± 10%) Hz or lithium battery;
b) Capacity:
1) 4000 lb (front scale),
2) 4000 lb (left scale),
3) 4000 lb (right scale);
c) System Accuracy: Better than 0.1% FS;
d) Overload Capacity: Safe Overload 125%, Ultimate Overload 150%;
e) Display Mode: Kilograms and Pounds, Switchable;
f) Signal Transmission: Wireless (Wi-Fi);
g) Wireless Transmission Distance: 50m;
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