发明名称 Reinigungsanlage für Flugzeuge.
摘要 The aircraft washing equipment comprises a sub-arm (15) that rotates at the tip of an ascendable and descendable arm (9) by means of a shaft (7) with a base perpendicular to the arm, and is movably controlled by a drive mechanism; a brush oscillating frame (32) rotated by a drive mechanism at the tip of the sub-arm, and which base rotates by means of a shaft (33 min ) perpendicular to the longitudinal direction of the sub-arm and a shaft at the tip of the arm; a brush swivelling frame (33) that is swivelled by a drive mechanism centering around the axis of the longitudinal direction of the brush oscillating frame; a brush arm (35, 36) attached to a hinge on both sides of the brush swivelling frame, disposed bendably in a plane which is parallel to the swivelling plane of the brush swivelling frame (33) and is bent by a drive mechanism; a center shaft of a rotating brush attached on brackets parallel to the brush swivelling frame and the brush arm (35, 36) mutually coupled with a universal joint, with their bases on the brush swivelling frame and the brush arm, and protruding perpendiculary to the swivelling plane of the brush swivelling frame; and a drive mechanism (34) to drive the rotating brush around the center axis.
申请公布号 DE69012228(D1) 申请公布日期 1994.10.13
申请号 DE1990612228 申请日期 1990.06.21
申请人 SUZUKI MECHANICAL ENGINEERING CO. LTD., TOKYO, JP 发明人 SUZUKI, TSUNEO, ,C/O SUZUKI MECHANICAL, KITA-KU, TOKYO, JP
分类号 B64F5/00 主分类号 B64F5/00
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