A rotorcraft provided with a rotary wing and a skid landing gear, the landing gear being provided with a first skid and a second skid and with a first cross-member and a second cross-member. The first cross-member is connected to an airframe of the rotorcraft only by two fastenings. The second cross-member is only carried during flight by two supports fastened to the airframe and traversed by the second cross-member. Each support comprises a hole delimited by a stop surface, the second cross-member always being separated from each stop surface by a clearance. A median supporting member is arranged transversely between the two supports and above the second cross-member.
GIRAVION MUNI D'UNE CELLULE PORTÉE PAR UN TRAIN D'ATTERRISSAGE À PATINS À ZONES DE REPRISE D'EFFORTS VARIABLES
ROTORCRAFT PROVIDED WITH A CELL SUPPORTED BY A LANDING GEAR WITH SKIDS WITH VARIABLE STRESS-RELIEVING ZONES
DREHFLÜGELFLUGZEUG, DAS MIT EINER DURCH EIN KUFENFAHRWERK GETRAGENEN ZELLE MIT ZONEN ZUR AUFNAHME VARIABLER KRÄFTE AUSGESTATTET IST
29.01.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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