2009
DOI: 10.1590/s1516-14392009000100014
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Thermal and microestructural characterization of epoxy-infiltrated hydroxyapatite composite

Abstract: In this work, hydroxyapatite (HAp) obtained from the deorganification of bovine bones using hot NaOH solution was used to synthesize a HAp/epoxy infiltrated composite. Infiltration was carried out by vacuum assisted immersion in hot epoxy resin. The resulting composite was characterized regarding polymer content, morphological aspects and flexural strength. The infiltration method used resulted in thorough infiltration of the HAp but some residual porosity remained. Although the epoxy resin showed good interac… Show more

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Cited by 8 publications
(5 citation statements)
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“…At 870 C, the contents of the scaffold bioactive layer (hydroxyapatite and silica) were $10.7, 50.5, 59.2 and 86.9% for M-CA, M-CAS-1, M-CAS-2 and M-CAS-3, respectively. TGA data for bovine cortical bone from Roese et al 30 are also shown. Interestingly, the M-CAS-2 scaffold showed decomposition behaviour similar to natural bone.…”
Section: Tga Resultsmentioning
confidence: 94%
“…At 870 C, the contents of the scaffold bioactive layer (hydroxyapatite and silica) were $10.7, 50.5, 59.2 and 86.9% for M-CA, M-CAS-1, M-CAS-2 and M-CAS-3, respectively. TGA data for bovine cortical bone from Roese et al 30 are also shown. Interestingly, the M-CAS-2 scaffold showed decomposition behaviour similar to natural bone.…”
Section: Tga Resultsmentioning
confidence: 94%
“…Stage I is attributed to the loss of adsorbed water and the initial burning of wax in the temperature range of 90–350 °C. Further weight loss in the range of 350–415 and 415–670 °C can be attributed to the combustion of the pore former and the removal of lattice water, respectively. , Figure b is associated with a total weight loss of 21%, with wheat flour as a pore former. Stage I with a temperature range of 80–330 °C corresponds to the evaporation of adsorbed water and the burning of the pore former.…”
Section: Resultsmentioning
confidence: 97%
“…Figure 7 shows that the T g value of neat epoxy was 162°C, whereas for varying weight percentages of reinforced (10,20,30, and 40 wt.%) composites the T g value was 164°C, 168°C, 170°C, and 173°C, respectively. The higher values of T g may be attributed to the introduction of MWCNT-coated aramid fibers, which interacted with the matrix to restrict the mobility of the epoxy network.…”
Section: Dsc Studymentioning
confidence: 99%
“…A two-stage curing process is used to form epoxy/single-walled CNT (SWCNT) composites at 80°C for 2 h up to 150°C for 2 h [19]. In another attempt, epoxy-infiltrated hydroxyapatite composites were prepared [20]. A monoglycidyl etherbased epoxy resin and an Epodur 231 curing agent with a 100:27.5 ratio (wt/wt) were used.…”
Section: Introductionmentioning
confidence: 99%