A landing gear of an aircraft of the present invention, includes a core section with a honeycomb structure, including a plurality of cell walls and a plurality of cell holes defined by the plurality of cell walls; a cover section which covers the core section; and a hole provided in the core section to absorb an impact, the hole having a diameter larger than that of the plurality of cell holes and extending in an extending direction of the plurality of cell holes.
LANDING GEAR OF AIRCRAFT AND AIRCRAFT COMPRISING LANDING GEAR
2018-03-15
Patent
Electronic Resource
English
Landing gear of aircraft and aircraft comprising landing gear
European Patent Office | 2021
|Landing gear, aircraft comprising landing gear and method of distributing load of landing gear
European Patent Office | 2023
|