Fluorine-containing composite material for aerospace cable and use method of fluorine-containing composite material
A technology of aerospace and composite materials, which is applied in the field of fluorine-containing composite materials for aerospace cables, and can solve problems such as affecting lines and easy to generate heat.
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Embodiment 1
[0030] see Figure 1-6 , this embodiment provides a fluorine-containing composite material for aerospace cables and a method of using the same, including a main body 1 of a cable jacket, the main body 1 is arranged in multiples, and the outer side walls of the plurality of main bodies 1 are sleeved and installed with an integrated sleeve 2. The materials of the main body 1 and the integrated sleeve 2 include tetrafluoroethylene, sodium metabisulfite, polyvinyl chloride, chloroprene and tetraalkylmethylaminothiocarbonyl disulfide;
[0031] The weight ratio of each component is,
[0032]
[0033] In order to facilitate and promote the circulation of air flow inside the integrated sleeve 2, multiple integrated sleeves 2 are arranged, and a movable mechanism 4 is arranged between the multiple integrated sleeves 2.
[0034] In order to prevent that the main body 1 cannot be fully protected after the multi-segment integrated sleeve 2 is installed, a connecting piece 3 is fixedly...
Embodiment 2
[0047] see Figure 7-8 , the difference from Example 1 is:
[0048] The driven member 51 , the driving member 53 and the transmission member 54 are all configured as gears.
[0049] Among them, the transmission members 54 are arranged in multiples, and are rotatably installed in the through hole 32 and the sealing cover 522. The plurality of transmission members 54 are in-line engagement with each other, and the transmission members 54 at the most ends engage the driven member 51 and the driving member respectively. 53. The driven member 51 and the driving member 53 are linked by a plurality of transmission members 54, so that the driving member 53 rotates and then drives the driven member 51 to rotate.
Embodiment 3
[0051] see Figure 1-2 and Image 6 , further improvements made on the basis of Example 1:
[0052] In order to strengthen the structural stability of the integrated sleeve 2 and prevent the integrated sleeve 2 from contacting the rotating disk 41 after being bent, a connecting plate 44 is fixedly installed in the integrating sleeve 2 , and a support rod 441 is fixedly connected to the outer side wall of the connecting plate 44 .
[0053] Among them, the support rods 441 are set in the same number as the main body 1, are located between the main body 1 and the adjacent main body 1, and are evenly and fixedly connected to the outer side wall of the connecting plate 44 in a circular array. The supporting rod 441 supports the integration sleeve 2 and the main body. 1 to limit.
[0054] The connecting plate 44 is located at the end of the rotating plate 41 away from the connecting piece 3, the inner cavity wall of the bracket 43 is fixedly connected with the first connecting rod...
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