Airplane mooring load calculating method
A load calculation and mooring technology, applied in the aviation field, can solve the problems of difficult finite element model establishment and simulation analysis, easy omission of bearing units, poor solution efficiency, etc., to improve mooring efficiency, convenient and fast operation, and improve work efficiency. Effect
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[0023] The present invention will be described in further detail below through specific examples.
[0024] For a certain type of aircraft, according to the calculation method of this patent, the output results of various load conditions are obtained from the tethered load calculation model. The direction angle of each mooring cable is shown in Table 1, which is used as design input.
[0025] Table 1 Direction angle of each mooring line (measured value)
[0026]
[0027] Now select the output results of 4 cases, as an example as follows:
[0028] Case 1: Right side wind + right side inertial force, N Q =6, aircraft unfolded state, normal weather tethered load
[0029] T 1 = 0 N T 2 = 101600 N ...
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