公开(公告)号：EP4389598A1

公开(公告)日：2024-06-26

申请号：EP22215343.9

申请日：2022-12-21

申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

发明人： FINK, Axel ,  OIOLI-NETO, Reynaldo

IPC分类号： B64C25/06 ,  B64C25/34 ,  B64C25/60

CPC分类号： B64C25/06 ,  B64C25/34 ,  B64C25/60

摘要： A rotorcraft comprising a fuselage (2) forming at least one lower lateral fuselage compartment (2c) with at least a first fitting (10a), a second fitting (11c), and a third fitting (11d); and at least one non-retractable wheel-type landing gear (8) that comprises: at least one wheel (8a); a shock absorber (8b) with a shock absorber tube (8c) having an open end (8g) and an axially opposed closed end (8f), and a shock absorber rod (8d) telescopically mounted to the shock absorber tube via the open end; a first fixation (8p) provided close to the open end on the shock absorber tube and connected to the first fitting; a second fixation (8e) provided close to the closed end on the shock absorber tube and connected to the second fitting; and a third fixation (8i) provided close to the closed end on the shock absorber tube and connected to the third fitting.