A kind of composite material prepreg for ultraviolet curing structure repair and preparation method thereof
A composite material and curing structure technology, applied in the field of materials, can solve the problems of limited curing thickness, incomplete curing and uneven curing of thicker products, and achieve the effect of facilitating promotion and improving light curing efficiency
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Embodiment 1
[0033] The composite material prepreg (about 4mm thick) for UV curing structure repair provided by this embodiment consists of resin mixture (①resin matrix, ②photoinitiator, ③photosensitization accelerator, ④thermal initiator) and reinforcing material (⑤ Alkali-free glass fiber grid cloth) is prepared according to a certain proportion. The proportion of these five raw materials is calculated in parts by weight, which is 100:2:0.5:1:(80-100).
[0034] The above-mentioned composite material prepreg for UV curing structure repair is prepared by the following method, and the steps include:
[0035] (1) Choose TH230 vinyl ester resin as the base material;
[0036] (2) Select Darocur1173 (2-hydroxyl-2-methyl-1-phenylacetone) as photoinitiator;
[0037] (3) Select stannous octoate matched with Darocur1173 as photosensitization accelerator;
[0038] (4) Select BPO (benzoyl peroxide) matched with Darocur1173 as thermal initiator;
[0039] (5) Blend the resin, select the non-alkali g...
Embodiment 2
[0043] The composite material prepreg (about 6 mm thick) for UV curing structure repair provided by this embodiment consists of resin mixture (①resin matrix, ②photoinitiator, ③photosensitization accelerator, ④thermal initiator) and reinforcing material (⑤ Alkali-free glass fiber grid cloth) is prepared according to a certain proportion. The proportion of these five raw materials is calculated in parts by weight, which is 100:2:0.5:1:(80-100).
[0044] The above-mentioned composite material prepreg for UV curing structure repair is prepared by the following method, and the steps include:
[0045] (1) Choose TH230 vinyl ester resin as the base material;
[0046] (2) Select Irgacure184 (1-hydroxycyclohexyl phenyl ketone) photoinitiator;
[0047] (3) Select stannous octoate matching Irgacure184 as photosensitizer;
[0048] (4) AIBN (azobisisobutyronitrile) matching with Irgacure184 is selected as thermal initiator;
[0049] (5) extract approximately 80% styrene in the original ...
Embodiment 3
[0054] The composite material prepreg (about 8mm thick) that this embodiment provides for UV-curable structural repair is made of resin mixture (①resin matrix, ②photoinitiator, ③photosensitization accelerator, ④thermal initiator A, ⑤thermal initiator B) and the reinforcing material (⑥ non-alkali glass fiber grid cloth) are prepared in a certain proportion. The proportions of these six raw materials are calculated in parts by weight, which are 100:2:0.8:1:1 in turn: (80-100).
[0055] The above-mentioned composite material prepreg for UV curing structure repair is prepared by the following method, and the steps include:
[0056] (1) Choose TH230 vinyl ester resin as the base material;
[0057] (2) Select Irgacure184 (1-hydroxycyclohexyl benzophenone) photoinitiator;
[0058] (3) select stannous octoate as photosensitizer;
[0059] (4) BPO (dibenzoyl peroxide) and MEKP (methyl ethyl ketone peroxide) are selected as thermal initiators A and B;
[0060] (5) extract approximate...
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