A stiffener skeleton that is configured to be mounted to an upper deck of a rotary wing aircraft in a maintenance phase, comprising an upper stiffening structure with a plurality of supporting arms for providing upside stiffening support, and a lateral stiffening structure with a plurality of supporting legs for providing lateral stiffening support, wherein the plurality of supporting arms and the plurality of supporting legs form a self-supporting frame structure.
STIFFENER SKELETON FOR A FIREWALL ARRANGEMENT OF A ROTARY WING AIRCRAFT
2022-05-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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