发明名称 DUAL PISTON ACTUATOR
摘要 <p>DUAL PISTON ACTUATOR A pair of axially aligned and nested pistons (20,30) are mounted in a pressure sealed arrangement within the bore of a pressure housing (12). A primary piston (20) is moved in response to increasing pressure to provide an actuating output force while a secondary piston (30) simultaneously moves to overcome a reverse bias on it by a tension spring (40) and adds to the actuating force by engaging the primary piston (20) only when the pressure exceeds a specific higher threshold. The primary and secondary pistons thereafter operate in conjunction under the influence of high pressure to provide the output actuating force.</p>
申请公布号 CA1183426(A) 申请公布日期 1985.03.05
申请号 CA19820418164 申请日期 1982.12.21
申请人 GOODYEAR AEROSPACE CORPORATION 发明人 HALL, JOHN M.;PANTIC, MILAN
分类号 F16D65/14;F16D65/54;(IPC1-7):F15B15/00 主分类号 F16D65/14
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