High pressure hydrogen storage bottle made of PBO fiber and carbon fiber mixed composite material and preparation method
A composite material and carbon fiber technology, applied in fixed capacity gas storage tanks, gas/liquid distribution and storage, pressure vessels, etc., can solve problems such as poor safety, low hydrogen storage efficiency, and steel cylinder weight, and achieve structural optimization and high safety The effect of reliability and long service life
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specific Embodiment approach 1
[0014] Specific implementation mode one: combine figure 1 The present embodiment will be described. This embodiment consists of an aluminum alloy lining layer 1, an elastic adhesive transition layer 2, a carbon fiber composite material inner structure layer 3, a PBO fiber composite material outer structure layer 4, and a glass fiber composite material outer protective layer 5. The layer 1 and the carbon fiber composite inner structure layer 2 are bonded by an elastic adhesive transition layer 2, and the inner surface of the PBO fiber composite material outer structure layer 4 is wound on the outer surface of the carbon fiber composite material inner structure layer 3, on the PBO The outer surface of the outer structural layer 4 of fiber composite material is wound with an outer protective layer 5 of fiber composite material.
specific Embodiment approach 2
[0015] Specific embodiment two: the preparation method of this embodiment adopts the following steps:
[0016] Step 1. First, evenly paint a layer of elastic interface adhesive layer 2 on the outer surface of the aluminum alloy inner lining layer 1; the aluminum alloy inner lining layer 1 is made of 6061 aluminum alloy, which has outstanding hydrogen corrosion resistance , will not produce hydrogen embrittlement cracks. The thickness of the aluminum alloy lining layer 1 is 3mm-6mm, and the thickness of the elastic adhesive layer 2 is 0.5mm-0.7mm. The aluminum alloy lining layer 1 adopts a seamless columnar structure formed by integral spinning technology, which avoids fatigue failure caused by welding seams.
[0017] Step 2: On the outer surface of the adhesive layer 2, the carbon fiber composite inner structure layer 3 is produced by using a fiber wet winding process, and the first to second layer of spiral winding, the second layer of hoop winding, the first to the second l...
specific Embodiment approach 3
[0024] Embodiment 3: The difference between this embodiment and Embodiment 2 is that the coating thickness of the elastic adhesive layer 2 in step 1 is 0.6 mm; in step 2, one layer of spiral winding and two layers of hoop winding are performed in sequence. , one layer of spiral winding, one layer of hoop winding, one layer of helical winding and one layer of hoop winding, the winding angle of helical winding is 15.5°, the thickness of each winding layer is 0.6mm, and the inner structure layer of carbon fiber composite material 3 The thickness is 4.2mm; in step 3, one layer of helical winding, one layer of hoop winding, two layers of helical winding and one layer of hoop winding are used successively, the winding angle of helical winding is 16°, and the thickness of each winding layer is 0.4mm, and the winding thickness of the PBO fiber composite material outer structure layer 4 is 2mm; in step 4, the second layer of helical winding and the second layer of glass fiber composite ...
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