发明名称 |
Brake force transducer for electric brakes |
摘要 |
An electric brake actuator for the brake system of an aircraft is presented. A brake actuator includes a piston driven by a cylindrical nut and screw arrangement, driven by an appropriate motor of the actuator. Application of brake force results in a reactionary force that deflects the top cover of the actuator. The axial component of this deflection correlates directly with the brake force applied. A beam is interposed between this cover and a top cap, such that deflection of the beam correlates to applied brake face. Piezo-resistive devices are connected to the beam and, through a whetstone bridge, provide an electrical output signal correlating to applied brake force.
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申请公布号 |
US7565953(B2) |
申请公布日期 |
2009.07.28 |
申请号 |
US20060433020 |
申请日期 |
2006.05.11 |
申请人 |
MEGGITT AIRCRAFT BRAKING SYSTEMS |
发明人 |
DALTON KEVIN M.;BURKHALTER KURT;OSBURN MICHAEL P.;BOOHER HAROLD R. |
分类号 |
B60T17/22;F16D65/18;F16D51/00 |
主分类号 |
B60T17/22 |
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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