An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within the aft fuselage. burst zone is defined about the turbine engine and a tail is disposed at least partially with the burst zone. The tail includes primary control surfaces and sacrificial control surfaces. The sacrificial control surfaces can break away in a defined manner to maintain integrity of the primary control surfaces outside of the burst zone.
STABILIZER SACRIFICIAL SURFACES
17.09.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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