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

Active Publication Date: 2015-07-15
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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Problems solved by technology

[0003] The loads of each mooring cable in the statically indeterminate mooring scheme are solved by the conventional finite element method. Since the flexible mooring cable can only bear the tensile load, but not the compressive load, when using the beam element and rod element FEM method to model and calculate, in the past, The trial and error method of manually adding or subtracting units is adopted, the solution efficiency is poor, and it is easy to miss the bearing unit
[0004] The mooring cable is extremely soft, but it is not a standard flexible body. It has the physical characteristics of only being able to bear tension, and is an energy dissipator, which brings certain difficulties to the establishment of the finite element model and simulation analysis.

Method used

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  • Airplane mooring load calculating method

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Embodiment Construction

[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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Abstract

The invention belongs to the technical field of aviation and in particular relates to load calculation of stationed mooring of airplane bodies and landing gears on a motion platform deck. An airplane mooring load calculating method is characterized by providing a non-linear GAP unit FEM calculation analyzing method which is high in universality and based on MSC. PATRAN/NASTRAN environment. External load (wind load and mass inertia force) is applied according to a full airplane mooring balance equation; the mooring load calculation situation is comprehensively and meticulously divided, so that the purpose of automatically screening and judging bearing mooring cables and the maximum mooring load is achieved on the premise of without changing the airplane and a motion platform deck model, and the work efficiency and the solving accuracy are improved.

Description

technical field [0001] The invention belongs to the technical field of aviation, and in particular relates to a method for calculating the mooring load of a fixed-wing aircraft. Background technique [0002] The aircraft must be moored and anchored on the flight deck of the motion platform and in the hangar to ensure safe stationing under the motion state of the platform at all levels of sea conditions. In the past, land-based aircraft usually did not have a special airport mooring device, and generally only fixed with wheel chocks; while the aircraft used for the service of the motion platform must be equipped with a special mooring device, and in order to ensure safety, a certain degree of redundancy is used. From the perspective of load strength calculation, the design scheme belongs to the multi-degree static indeterminate mooring scheme. [0003] The loads of each mooring cable in the statically indeterminate mooring scheme are solved by the conventional finite element...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 姚念奎曹奇凯隋福成邱涛
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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