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ENDLESS ORBITAL MOTION STRUCTURE FOR ELLIPTICAL ORBIT

机译:椭圆轨道的无轨道运动结构

摘要

PROBLEM TO BE SOLVED: To provide an endless orbital motion structure for enabling revolving circular motion greater than conventional one without changing a revolving range and a size.;SOLUTION: As shown in a B-B cross section, an elliptical frame (1) is constituted as the base of the structure with totally four semi-circles, namely, upper and lower radial circles (α) each having a greater radius and right and left radial circles (β) each having a smaller radius, where an elliptical smooth outer peripheral face (γ) is formed into a convex shape (ε). On the elliptical orbital face (γ) of the constituted elliptical frame (1), a link mechanism orbital body (4) having endless linkage is installed. A concave shape (δ) of the revolution face of such an orbit holding revolving body (19) that the elliptical orbital face (γ) is incorporated in the connection axis (6) of the link mechanism endless orbital body (4) is matched to the convex shape (ε) of the outer peripheral face (1) of the elliptical frame (1) to enable smooth elliptical endless orbital motion while avoiding the shift of an orbit during the endless orbital motion of the link mechanism endless orbital body (4).;COPYRIGHT: (C)2010,JPO&INPIT
机译:解决的问题:提供一种环形轨道运动结构,以使旋转圆周运动比常规旋转运动更大,而又不改变旋转范围和尺寸。解决方案:如BB截面所示,椭圆框架(1)构成为具有总共四个半圆的结构的底部,即,每个半径较大的上,下径向圆(α)和半径较小的左右径向圆(β),其中椭圆形光滑的外周面(γ)形成为凸形(ε)。在所构成的椭圆形框架(1)的椭圆形轨道面(γ)上,安装有具有环形连杆的连杆机构轨道体(4)。这样的轨道保持公转体(19)的公转面的凹面形状(δ)是椭圆形轨道面(γ)结合在连杆机构环形轨道体(4)的连接轴线(6)中。与椭圆形框架(1)的外周面(1)的凸形(epsi)匹配,以实现平滑的椭圆形无限循环运动,同时避免在连杆机构无限循环体进行无限循环运动时轨道发生位移(4).;版权:(C)2010,日本特许厅&INPIT

著录项

  • 公开/公告号JP2010155586A

    专利类型

  • 公开/公告日2010-07-15

    原文格式PDF

  • 申请/专利权人 YOKOI TAKAHIRO;

    申请/专利号JP20080336314

  • 发明设计人 YOKOI RAN;YOKOI TAKAHIRO;

    申请日2008-12-29

  • 分类号B62D55/20;B62B5/02;B62D55/075;B62D55/12;B62D55/14;B62M29/00;A01D34/83;

  • 国家 JP

  • 入库时间 2022-08-21 19:05:49

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