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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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