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    • 11. 发明授权
    • Hydraulic fluid control apparatus
    • 液压油控制装置
    • US08205830B2
    • 2012-06-26
    • US11568822
    • 2005-05-10
    • Richard John Miller
    • Richard John Miller
    • B60T8/32B64C25/46
    • B60T8/00B60T8/325
    • In the field of avionics, it is difficult to justify initiation of new aircraft programmes for replacement of small numbers of niche aircraft. Instead, in many cases, retrofitting existing aircraft is preferred for economic reasons. In this respect, upgrading existing braking systems to accommodate replacement of existing brake units employing sintered friction materials with brake units employing carbon-carbon composite friction materials is desirable. However, when upgrading the braking systems it is necessary to ensure that the integrity of the existing airframe is not compromised by the use of the new brake assemblies employing the carbon-carbon composite friction materials. Consequently, the present invention replaces existing pressure control valves of existing braking systems with an electronic control unit (126) coupled to a pressure control servovalve (128) thereby ensuring proper application of hydraulic pressure to brake assemblies (122). An advantage of this invention is that the pressure profile of the hydraulic fluid is controllable and hence the integrity of the airframe is maintained.
    • 在航空电子学领域,很难证明开始使用新的飞机方案来替代少量的利基飞机。 相反,在许多情况下,由于经济原因,改装现有飞机是首选的。 在这方面,期望升级现有的制动系统以适应使用具有使用碳 - 碳复合摩擦材料的制动单元的烧结摩擦材料的现有制动单元的更换。 然而,当升级制动系统时,有必要确保使用采用碳 - 碳复合材料摩擦材料的新的制动组件不影响现有机身的完整性。 因此,本发明用耦合到压力控制伺服阀(128)的电子控制单元(126)来代替现有制动系统的现有压力控制阀,从而确保对制动组件(122)的适当的液压施加。 本发明的一个优点是液压流体的压力分布是可控的,因此保持了机身的完整性。