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.
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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 |
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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