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 |