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Curvature theory for the double flier eight-bar linkage

机译:双翼八连杆机构的曲率理论

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摘要

This paper presents a graphical technique to obtain the radius of curvature of the path traced by a coupler point of a planar, single-degree-of-freedom, indeterminate eight-bar linkage commonly referred to as the double flier linkage. The first step is to find the pole for the instantaneous motion of the coupler link; i.e., the point coincident with the absolute instant center of the coupler link. Since the double flier is a linkage with kinematic indeterminacy then the Aronhold-Kennedy theorem cannot locate this instant center. The paper, therefore, begins with a novel technique, which requires few geometric constructions, to locate this instant center. Then the paper focuses on the graphical technique to determine the radius of curvature of the path of an arbitrary coupler point for a given position of the input link. The technique begins by obtaining an equivalent five-bar linkage and four kinematic inversions of this linkage. A four-bar linkage is obtained from each inversion. Finally, the systematic procedure provides a four-bar linkage in which the motion of the coupler link is equivalent up to, and including, the second order properties of motion of the coupler of the original double flier linkage. The radius of curvature of the path traced by the coupler point is then obtained from the well-known Euler-Savary equation.
机译:本文提出了一种图形技术,以获取由平面,单自由度,不确定的八连杆机构(通常称为双翼连杆机构)的耦合器点耦合的轨迹的曲率半径。第一步是找到耦合器连杆瞬时运动的极点;即与耦合器链接的绝对瞬时中心重合的点。由于双飞行器是运动不确定性的联系,因此Aronhold-Kennedy定理无法定位此即时中心。因此,本文从一种新颖的技术开始,该技术只需很少的几何构造即可定位此即时中心。然后,本文重点关注图形技术,以确定输入链接的给定位置的任意耦合器点的路径的曲率半径。该技术从获得等效的五杆连杆机构和该连杆机构的四个运动学反转开始。从每个反演中获得四连杆机构。最后,该系统过程提供了一种四连杆机构,其中,连杆机构的运动在原始双飞行连杆机构的耦合器的运动的二阶特性(包括二阶运动特性)上并包括在内。然后从众所周知的Euler-Savary方程获得耦合点跟踪的路径的曲率半径。

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