发明名称 Manufacturing methods for machining spring ends parallel at loaded length
摘要 A first end surface of a coiled compression spring at its relaxed length is machined to a plane transverse to the spring axis. The spring is then placed in a press structure having first and second opposed planar support surfaces, with the machined spring end surface bearing against the first support surface, the unmachined spring end surface bearing against a planar first surface of a lateral force compensation member, and an opposite, generally spherically curved surface of the compensation member bearing against the second press structure support surface. The spring is then compressed generally to its loaded length, and a circumferentially spaced series of marks, lying in a plane parallel to the second press structure support surface, are formed on the spring coil on which the second spring end surface lies. The spring is then removed from the press structure, and the second spring end surface is machined to the mark plane. When the spring is subsequently compressed to its loaded length the precisely parallel relationship between the machined spring end surfaces substantially eliminates undesirable lateral deflection of the spring.
申请公布号 US5454150(A) 申请公布日期 1995.10.03
申请号 US19930149889 申请日期 1993.11.10
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 HINKE, PATRICK T.;BENSON, DWAYNE M.;ATKINS, DONALD J.
分类号 B21F35/00;B24B7/16;F16F1/12;(IPC1-7):B21F35/00;B21F3/00 主分类号 B21F35/00
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