| 摘要 |
A landing gear (30) includes a trunnion (40) that has at least one principal pivot point (42). The principal pivot point (42) is adapted to be pivotably coupled to an airframe (12) to allow the trunnion (40) to pivot about a principal trunnion pivot axis (45). The trunnion (40) is operable to move between a deployed position and a stowed position by pivoting about the principal trunnion pivot axis (45). The landing gear (30) also includes a wheel (60) rotatably coupled to the trunnion (40). The wheel (60) has a rolling axis (68) and a center, which is located forward of the principal pivot point (42) when the trunnion (40) is in the deployed position.
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