发明名称 MANUFACTURE OF COMPOSITE MATERIAL PART CONSTITUTED BY CENTRAL BODY AND AUXILIARY WING AND MISSILE STRUCTURE OBTAINED BY SAID MANUFACTURE
摘要 PURPOSE: To provide a process for producing a composite material part having a central hollow body with ailerons fixed thereto. CONSTITUTION: Peripheral mandrels 1,... having two mutual contact faces 4, 6, a face 2 being fixed to a central hollow body, and two aileron fixing faces 3, 7 being fixed to the mutual contact faces 4, 6, respectively, are jointed while pairing the mutual contact faces 4, 6 such that the fixing faces themselves form a continuous face thus obtaining an assembly. A filament is then wound around the assembly and the winding 10 is cut off. Subsequently, the assembly is dismantled and the peripheral mandrels 1,... are pressed against a central mandrel 16 such that the aileron fixing faces 3, 7 face each other while being paired.
申请公布号 JPH07234099(A) 申请公布日期 1995.09.05
申请号 JP19940148232 申请日期 1994.06.29
申请人 AEROSPAT SOC NATL IND 发明人 JIYATSUKU FUAGE
分类号 F42B15/00;B29C53/58;B29C69/00;B29C70/06;B29C70/30;B29C70/54;B29D99/00;F42B10/06;(IPC1-7):F42B15/00;B29D31/00 主分类号 F42B15/00
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