发明名称 HELICOPTER
摘要 A composite structure forming a load bearing composite shell for a helicopter, with a shell which defines the exterior of a fuselage and includes a central fuselage section and tail boom, a fuselage which is adapted house an engine or drive train, a layered composite crashworthy seat and support structure and a fastening and a method of fastening by providing an adhesive between two layers which is allowed to flow through opposing holes in the layers to provide a chemical and mechanical attachment between the layers.
申请公布号 US2014197271(A1) 申请公布日期 2014.07.17
申请号 US201214124247 申请日期 2012.06.07
申请人 Maloney Peter;Heatley Nina 发明人 Maloney Peter;Heatley Nina
分类号 B64C27/04;B64D11/06;B64C1/00;B64C27/82;B64D37/04 主分类号 B64C27/04
代理机构 代理人
主权项 1. A primary flight structure comprising: a load bearing composite shell defining at least the exterior of a helicopter fuselage, the fuselage defining at least a central fuselage section and tail boom, wherein the central fuselage section is adapted enclose at least one of an engine or drive train.
地址 Auckland NZ