发明名称 Reconstitution of composite with surface- or deeper defect, including foam structures normally heated with difficulty
摘要 To heat the replaced section (2) a single radiant (6) emits infra red, the bandwidth ranging over wavelengths 1-10 mu m. It is located to heat the defect area, by irradiating the evacuation hood over the piece replaced, and other added layers, which are compressed. Preferred features: The radiant (6) is a catalytic burner (7). The evacuation hood is transparent to its infra red radiation. It is placed directly opposite the textile gas-venting layer (3). The sealing film (8) facing the plastic material is inserted between the hood and the venting fabric. A non-adherent film (9) facing the replacement section, is inserted between it and venting fabric. A variant based on the foregoing principles, forming a composite object, is also described.
申请公布号 FR2777496(A1) 申请公布日期 1999.10.22
申请号 FR19980005052 申请日期 1998.04.17
申请人 SUNKISS AERONAUTIQUE 发明人 CHARMES MICHEL;COMOGLIO BRUNO
分类号 B29C73/14;B29C70/44;B29C73/04;B29C73/32;B29K105/00;B29L31/30;B32B1/06;B32B37/00;(IPC1-7):B29C73/34 主分类号 B29C73/14
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