The invention is related to a rotary wing aircraft with a fuselage and an at least partially non-retractable landing gear, wherein the at least partially non-retractable landing gear comprises at least three individual support legs, wherein at least one individual support leg (30) of the at least three individual support legs is mounted pivotally to the fuselage by means of an associated pivot bearing arrangement (35), wherein the at least one individual support leg (30) is further connected to the fuselage via at least one tension device (36) with a predetermined elastic range, and wherein the at least one tension device (36) is adapted to act, in the predetermined elastic range, as a tension spring, and, outside of the predetermined elastic range, as an energy absorber.
A ROTARY WING AIRCRAFT WITH AN AT LEAST PARTIALLY NON-RETRACTABLE LANDING GEAR
DREHFLÜGELFLUGZEUG MIT EINEM ZUMINDEST TEILWEISE NICHT EINZIEHBAREN FAHRWERK
AÉRONEF À VOILURE TOURNANTE ÉQUIPÉ D'UN TRAIN D'ATTERRISSAGE AU MOINS PARTIELLEMENT NON RÉTRACTABLE
01.11.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ROTARY WING AIRCRAFT WITH AN AT LEAST PARTIALLY NON-RETRACTABLE LANDING GEAR
Europäisches Patentamt | 2023
|A ROTARY WING AIRCRAFT WITH AN AT LEAST PARTIALLY NON-RETRACTABLE LANDING GEAR
Europäisches Patentamt | 2023
|