Rotorcraft with a non-retractable wheel-type landing gear
AssigneesAirbus Helicopters Deutschland GmbH, Airbus Helicopters
InventorsAxel Fink, Aurelien Achard, Didier Bertin
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AssigneesAirbus Helicopters Deutschland GmbH, Airbus Helicopters
InventorsAxel Fink, Aurelien Achard, Didier Bertin
Estimating the term…
A rotorcraft with at least one non-retractable wheel-type landing gear and a fuselage comprising a lower shell, an inner floor, and at least one lower fuselage compartment arranged between the inner floor and the lower shell, wherein the at least one non-retractable wheel-type landing gear is rigidly attached in the at least one lower fuselage compartment and comprises: at least one wheel; a shock absorber connected to the at least one wheel and comprising a shock absorber tube and a shock absorber rod telescopically mounted to the shock absorber tube; at least two mounting arms extending laterally from the shock absorber tube; and a mounting pin device extending laterally from the shock absorber tube and comprising a mounting pin connected to a floor fitting provided at the inner floor.
A rotorcraft with a fuselage comprising a lower shell, an inner floor, and at least one lower fuselage compartment arranged between the inner floor and the lower shell, wherein the at least one lower fuselage compartment is equipped with a floor fitting provided at the inner floor and at least two lateral fittings, and wherein the at least one lower fuselage compartment is at least accessible via an opening formed in the lower shell, the rotorcraft comprising:
A rotorcraft with a fuselage comprising a lower shell, an inner floor, and a lower fuselage compartment arranged between the inner floor and the lower shell, wherein the lower fuselage compartment has a floor fitting at the inner floor and two lateral fittings, and wherein the lower fuselage compartment is accessible via an opening in the lower shell, the rotorcraft comprising:
Dependencies are inferred from the claim text.