Skin structure and skin installation and detachment methods
An installation method and skin technology, applied in the aerospace field, can solve the problems of high travel rate, difficult disassembly, complicated operation, etc., and achieve the effect of ensuring installation size, stable and reliable structure, and meeting strength requirements.
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[0040] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art.
[0041] figure 1 It is a schematic diagram of an assembled overall structure of an embodiment of the present invention. figure 2 for figure 1 Schematic diagram of the overall structure of the skin structure in the embodiment. image 3 for figure 1 Schematic diagram of the overall structure of the first part to be connected in the embodiment. Figure 4 for figure 1 Schematic diagram of the structure of the first positioning kit...
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