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    • 66. 发明申请
    • AEROPLANE CRUSHING DEVICE, AND AEROPLANE DEMOLITION METHOD
    • 飞机破碎装置和飞机拆卸方法
    • US20150007736A1
    • 2015-01-08
    • US14368486
    • 2013-09-03
    • KABUSHIKI KAISHA TOWANI
    • Yoshiaki Takakura
    • B30B9/00B30B15/00
    • B30B9/32B09B3/00B09B5/00B30B7/04B30B9/00B30B13/00B30B15/0023B30B15/062B30B15/30B64F5/00Y02P70/585
    • An aircraft collapsing device that collapses an aircraft fuselage inward includes: a gate-shaped shell which covers a circumference of both sides and an upper portion of a fuselage of an aircraft body from which horizontal wings and a vertical wing have been decoupled, a wedge-shaped pressing member that is mounted to an upper portion of the shell to press at least one portion of a circumference of at least one of annular frames juxtaposed in a longitudinal direction of the fuselage toward a center of the fuselage, a pair of sidewall pressing members that is mounted to both sides of the shell to press the fuselage simultaneously from two directions crossing a pressing direction of the wedge-shaped pressing member at the center of the fuselage after pressing by the wedge-shaped pressing member, and a moving unit that moves the fuselage of the aircraft and the shell relative to one another.
    • 将飞机机身向内折叠的飞机塌缩装置包括:覆盖飞机机身两侧的圆周和飞机主体的机身的上部的门形壳体,水平翼和垂直翼从该机体的机身脱离, 形状的按压构件,其安装到所述壳体的上部,以将沿机身的纵向方向并列设置的至少一个环形框架的圆周的至少一部分朝向机身的中心按压;一对侧壁按压构件 安装在壳体的两侧,同时从通过楔形按压部件按压之后的机身中心处的楔形按压部件的按压方向的两个方向按压机身;以及移动单元,其移动 飞机的机身和壳体相对于彼此。
    • 67. 发明授权
    • Punch, and rotary compression molding machine using the same
    • 冲压和旋转压缩成型机使用相同
    • US07581941B2
    • 2009-09-01
    • US11660325
    • 2005-08-24
    • Kenji HaradaFumiharu IkaiYuichi Ozeki
    • Kenji HaradaFumiharu IkaiYuichi Ozeki
    • B29C43/08
    • B30B11/08B30B11/34B30B15/0023B30B15/065Y10T83/391Y10T83/395
    • This invention provides a punch comprising: a center punch and an outer punch surrounding the outer periphery of the center punch, both of which being slidable and capable of compressing; and relative position restriction means for restricting a relative position of the center and outer punches, the relative position restriction means being configured to restrict a first position in which a punch tip of the center punch is protruded from a punch tip of the outer punch and a second position in which the punch tip of the center punch is substantially coincident with the punch tip of the outer punch, and being configured to fail to restrict a third position in which the punch tip of the center punch is retracted in the punch tip of the outer punch, as well as a rotary compression molding machine provided with the double-structured punch.
    • 本发明提供了一种冲头,其包括:中心冲头和围绕中心冲头的外周的外冲头,两者均可滑动并能够压缩; 以及用于限制中心和外部冲头的相对位置的相对位置限制装置,相对位置限制装置被构造成限制中心冲头的冲头顶端从外冲头的冲头顶端突出的第一位置和 第二位置,其中中心冲头的冲头尖部与外冲头的冲头顶端基本一致,并且构造成不能限制第三位置,其中中心冲头的冲头尖端在其中的冲头顶端缩回 外冲头,以及设置有双结构冲头的旋转压缩成型机。