| 摘要 |
A landing gear (1, 1") for an aircraft (2), having mounting means (5, 57) fitted to the fuselage (3) of the aircraft (2); at least one wheel (6); and at least one supporting arm (7, 7") having a first end portion (8, 8") connected to the mounting means (5, 57), and a second end portion (9, 9") opposite the first end portion (8, 8"), and to which the wheel (6) is suspended. The first end portion (8, 8") of the supporting arm (7, 7") has a seating portion (16, 60) fitted in rotary manner to a pin (10, 56) connected to the mounting means (5, 57) and extending crosswise to the supporting arm (7, 7"); and an electrically controlled actuator (20, 20") is fitted to the seating portion (16, 60), and is activated selectively to rotate the supporting arm (7, 7"), about the pin (10, 56), between a first and second operating position defining a stowed in-flight configuration and a lowered landing configuration of the landing gear (1, 1") respectively. |
