A landing gear for an aircraft can include a skid tube having an inboard flat side wall and an outboard flat side wall, the skid tube having a skid tube centerline plane that is parallel to at least one of the outboard flat side wall and the inboard flat side wall, the skid tube being canted inboard at an angle The landing gear can include a forward cross tube having a straight horizontal portion, a first bend transitioning the straight horizontal portion into a straight angled portion, and a second bend transitioning the straight angled portion into a straight end portion.
HELICOPTER SKID LANDING GEAR
2016-08-25
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Helicopter skid landing gear falling collision simulation analysis method
Europäisches Patentamt | 2015
|