发明名称 Dual piston actuator
摘要 A pair of axially aligned and nested pistons are mounted in a pressure sealed arrangement within the bore of a pressure housing. A primary piston is moved in response to increasing pressure to provide an actuating output force while a secondary piston simultaneously moves to overcome a reverse bias on it by a tension spring and adds to the actuating force by engaging the primary piston 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.
申请公布号 US4496033(A) 申请公布日期 1985.01.29
申请号 US19810334707 申请日期 1981.12.28
申请人 GOODYEAR AEROSPACE CORPORATION 发明人 HALL, JOHN M.;PANTIC, MILAN
分类号 F16D65/14;(IPC1-7):B60T11/00;F01B7/20 主分类号 F16D65/14
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