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公开(公告)号:US20120024211A1
公开(公告)日:2012-02-02
申请号:US13142592
申请日:2010-01-07
申请人: Garry Ronald Wiltse
发明人: Garry Ronald Wiltse
IPC分类号: B63B1/32 , B63H11/00 , B63H1/14 , B63B3/10 , B63B15/00 , B63B1/26 , B63H25/06 , B63B3/38 , B63H9/04
摘要: Stabilizers (14.1, 14.2) coupled to associated stanchions (20.1, 20.2) and associated linkage assemblies (16.1, 16.2) on both sides of a central hull (12) provide for piercing or cutting through waves (76′). Aerodynamic surfaces (18.1, 18.2, 112, 114, 116, 118) over the linkage assemblies (16.1, 16.2) provide lift, as may a central keel (68) on the central hull (12). In one embodiment, each stanchion (20.1, 20.2) is coupled to the central hull (12) with a four-bar linkage assembly (16.1′, 16.2′) incorporating pivot bushings (78, 80, 86, 88, 92, 94, 98, 100) depending from the central hull (12) and the associated stanchion (20.1, 20.2) in cooperation with two pairs of non-parallel hinge pins (82.1, 82.2, 82.3, 82.4), respectively, with associated wedge-shaped aerodynamic surfaces (112′, 114′, 116′, 118′) attached to the linkage assembly (16.1, 16.2). The height of the stabilizers (14.1, 14.2) relative to the central hull (12) is adjustable using associated actuators (42.1, 42.2) in cooperation with the linkage assemblies (16.1, 16.2) either providing for, or responsive to, different operating conditions. Dampers (42′) may be associated with or incorporated in the actuators (42.1, 42.2) to provide for dampening associated shock and vibration.
摘要翻译: 耦合到相关联的支柱(20.1,20.2)和在中心船体(12)的两侧上的相关连接组件(16.1,16.2)的稳定器(14.1,14.2)提供刺穿或切割波浪(76')。 连杆组件(16.1,16.2)上方的空气动力学表面(18.1,18.2,112,114,116,118)提供升力,如中央船体(12)上的中心龙骨(68)。 在一个实施例中,每个支柱(20.1,20.2)通过四个连杆组件(16.1',16.2')联接到中心船体(12),该连杆组件包括枢轴衬套(78,80,86,88,92,94, 分别与两对非平行铰链销(82.1,82.2,82.3,82.4)配合,从中央船体(12)和相关的支柱(20.1,20.2)中分别具有相关联的楔形空气动力学 附接到连杆组件(16.1,16.2)的表面(112',114',116',118')。 稳定器(14.1,14.2)相对于中心船体(12)的高度可以使用相关联的致动器(42.1,42.2)与联动组件(16.1,16.2)协调来调节,其提供或响应于不同的操作条件 。 阻尼器(42')可以与致动器(42.1,42.2)相关联或并入其中,以便抑制相关联的冲击和振动。