Monocoque helicopter fuselage with integral tail boom

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United States of America Patent

PATENT NO 9932123
SERIAL NO

14124247

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Abstract

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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.

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Patent Owner(s)

Patent OwnerAddress
INNOVA HELICOPTERS TECHNOLOGY HOLDINGS NZ LIMITED48 BAWDEN ROAD RD 2 ALBANY 0792

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Heatley, Nina Auckland, NZ 1 10
Maloney, Peter Auckland, NZ 5 32

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