An aircraft landing gear assembly including a structural load bearing beam arranged, in use, to react torsional loads applied to it. The beam has a tubular box section main body having four straight sidewall portions, adjacent sidewall portions being orthogonal to one another and connected by rounded corner portions. Each corner portion has a radius of between 10% and 40% of the width and/or height of the tubular box section main body.
AIRCRAFT LANDING GEAR ASSEMBLY
20.09.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |