| 摘要 |
A steering device (20) for an aircraft landing gear leg including a main fitting has a steering collar (16) for rotatably mounting on the outside of the main fitting, and an actuator (40,50) having an actuator body (42,52) and an actuator arm (43,53) arranged to move between an extended position and retracted position with respect to the actuator body (42,52). The actuator arm (43,53) is pivoted to the main fitting. A bracket (29) is pivotally connected to the main fitting at a first pivot location (36), to the actuator body (52) at a second pivot location (34), and to one end (28) of a steering arm (26) at a third pivot location (32). The steering arm (26) is pivoted at its other end (27) to the steering collar (16). Also, an aircraft landing gear with the steering device (20) and aircraft having the landing gear. |
