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    • 3. 发明申请
    • LIGATING APPARATUS
    • 发光装置
    • US20110245855A1
    • 2011-10-06
    • US13017410
    • 2011-01-31
    • Yoshiaki MATSUOKAKoji ITOHMasayuki IWASAKARyosuke OSAKO
    • Yoshiaki MATSUOKAKoji ITOHMasayuki IWASAKARyosuke OSAKO
    • A61B17/08
    • A61B17/122A61B17/1227A61B17/1285
    • A ligating apparatus includes a clip, a clip connecting member, a clip holding member, an operating wire, an inner sheath member, an outer sheath member and first and second movement restricting portions. The clip ligates a body tissue with arm portions. The clip connecting member connects to a clip base portion. The clip connecting member is inserted through the clip holding member. The operating wire connects to the clip connecting member. The inner sheath member encloses the operating wire to support the clip holding member. The outer sheath member covers an outer periphery of the inner sheath member and freely advances and retreats. The outer sheath member advances and/or retreats to change the degree of opening of the arm portions. The first movement restricting portion restricts the inward movement of the clip holding member. The second movement restricting portion restricts the outward movement of the clip holding member.
    • 连接装置包括夹子,夹子连接构件,夹子保持构件,操作线,内部护套构件,外护套构件以及第一和第二移动限制部。 夹子将身体组织与臂部分结合。 夹子连接构件连接到夹子基部。 夹子连接构件插入穿过夹持件。 操作线连接到夹子连接构件。 内护套构件包围操作线以支撑夹持件。 外护套构件覆盖内护套构件的外周并自由前进和后退。 外鞘构件前进和/或后退以改变臂部分的开度。 第一移动限制部分限制夹子保持构件的向内运动。 第二移动限制部分限制夹子保持构件的向外移动。
    • 4. 发明申请
    • AIRCRAFT REACTION LINK
    • 飞机反应链接
    • US20110139938A1
    • 2011-06-16
    • US12954140
    • 2010-11-24
    • Koji ITOHToshiaki OGAWAMakoto NAGASHIMA
    • Koji ITOHToshiaki OGAWAMakoto NAGASHIMA
    • B64C13/40
    • B64C13/24Y02T50/44
    • An aircraft reaction link includes a pair of linear portions, a coupling portion that couples ends of the pair of linear portions on the same side to each other, a fulcrum shaft attachment portion, and a cylinder attachment portion. A metal frame that is made of a metallic material and that is provided so as to extend across the coupling portion and the pair of linear portions and a composite frame that is made of fiber-reinforced plastic and that is provided so as to extend at least in the pair of linear portions are bonded together, and thereby, the pair of linear portions and the coupling portion are formed. The metal frame is provided so as to extend from the fulcrum shaft attachment portion to the cylinder attachment portion.
    • 飞机反应连杆包括一对直线部分,将一对直线部分的端部彼此相对联接的联接部分,支点轴附接部分和气缸附接部分。 金属框架,其由金属材料制成,并且设置成跨越所述联接部分和所述一对直线部分,以及复合框架,所述复合框架由纤维增强塑料制成,并且被设置成至少延伸 在一对直线部分接合在一起,从而形成一对直线部分和联接部分。 金属框架设置成从支点轴附接部分延伸到气缸附接部分。