发明名称 Fuselage structure for helicopter
摘要 The invention relates to a helicopter fuselage of the type including a central structure to which are linked a front structure, a rear structure and a landing gear, and which supports a transmission gearbox, a main rotor and at least one engine (50), and of the type in which the central structure includes a skeleton (16) fitted with covering elements which define the external shape of the fuselage. According to the invention, the skeleton (16) of the central structure exhibits substantially the shape of a regular hexahedron consisting of skeleton panels (28, 30, 32, 34, 36, 38) assembled together. The invention finds an application especially for producing light helicopters.
申请公布号 US5562264(A) 申请公布日期 1996.10.08
申请号 US19950392296 申请日期 1995.02.21
申请人 EUROCOPTER FRANCE 发明人 BIETENHADER, CLAUDE
分类号 B64C1/12;B64C1/00;B64C1/06;B64C27/00;B64C27/04;(IPC1-7):B64C1/06;B64C1/22 主分类号 B64C1/12
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