Method for calculating longitudinal damping force generated by upward raising of tail hook after cable hooking
A calculation method and technology of damping force, applied in the field of aeronautical engineering, can solve problems such as inability to guarantee the hook cable
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[0030] The parameters of a certain type of fixed-wing aircraft are as follows, see Table 1.
[0031] Table 1 Tail hook and cable parameters
[0032]
[0033] Substitute the data in Table 1 into the above equations ①②③④⑤⑥, and solve each equation within the time t equal to 0 to 3 seconds. When solving translation and rotation, refer to figure 1 , when solving the damping force equation, see figure 2 , image 3 . Use the SIMULINK module in the MATLAB software to solve the problem, see Figure 4 . Choose k=2×10 6 N / m, c=6×10 4 The calculation results at N·s / m are as follows, and the calculation results of the impact between the tail hook and the road surface are shown in Figure 5 . The maximum damping force of the longitudinal buffer is 285550N during the upward rotation of the tail hook, which shows that the longitudinal buffer has a certain tendency to inhibit the upward rotation of the hook.
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