发明名称
摘要 There is described a transmission (6) for a helicopter (1), the transmission having a movable transmission member (7); a casing (8) housing the movable member (7); lubricated supporting means (9) for supporting the movable member (7) inside the casing (8) and for rotation about an axis (A); and feed means (11) for feeding a lubricating fluid to the supporting means (9); the transmission (6) also has storage means (25) permitting gradual release of the lubricating fluid, and which are connected fluidically to the feed means (11) and to the supporting means (9) to permit lubrication of the supporting means (9) in the event of breakdown of the feed means (11); and the storage means (25) are angularly integral with the movable member (7) and located radially inwards of the supporting means (9) to feed the lubricating fluid centrifugally to the supporting means (9).
申请公布号 JP5122092(B2) 申请公布日期 2013.01.16
申请号 JP20060169043 申请日期 2006.06.19
申请人 发明人
分类号 F16H57/04;B64C27/12 主分类号 F16H57/04
代理机构 代理人
主权项
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