A design and processing method suitable for extremely light mass delivery model
A model and quality technology, applied in the aviation field, can solve problems such as large influence of model design and processing quality experience, unstable quality control, time-consuming and labor-consuming, etc., to improve design and processing efficiency, low design limit requirements, and save design and the effect of processing time
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Embodiment 1
[0071] The flow sequence of the whole method is design module - part additive manufacturing - part assembly. The design module includes two subroutines, the quality characteristic calculation module and the quality characteristic design module.
[0072] The mass characteristic calculation module calculates the weight, center of gravity and moment of inertia of the model according to the model scaling and dynamic similarity criteria, and takes the calculated weight, center of gravity and moment of inertia as the target parameters of the mass characteristic design module.
[0073] The core idea of the mass characteristic calculation module is: hollow out the middle of the solid model to form a shell, and the hollowed out part is continuous. The basic thickness of the shell needs to be guaranteed, and its shape is not limited. The filling part is placed inside the hollowed part. The filling part can be made of materials of different densities. The filling part is continuous and...
Embodiment 2
[0083] A design and processing method suitable for an extremely light mass delivery model, characterized in that it includes design and processing steps, and is characterized in that it manages to include the following modules: a mass characteristic calculation module, a mass characteristic design module, component additive manufacturing, and model assembly, The design method steps are as follows:
[0084] (1) Parts are firstly divided, and the model entity without any operation is defined as a solid part, the cut-out part is defined as a hollow part, and the filled part is defined as a filled part;
[0085] (2) Then the cross-sectional profile and axial profile of the solid part are described by the profile formed by point Ai and the profile formed by point a respectively, and the cross-sectional profile and axial profile of the hollowed-out part are described by the profile formed by point Bi and point b respectively The formed contour description, the cross-sectional contou...
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