发明名称 HYDRAULIC FLUID CONTROL APPARATUS
摘要 <p>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.</p>
申请公布号 WO2005110828(A1) 申请公布日期 2005.11.24
申请号 WO2005GB01753 申请日期 2005.05.10
申请人 DUNLOP AEROSPACE LIMITED;MILLER, RICHARD, JOHN 发明人 MILLER, RICHARD, JOHN
分类号 B60T8/00;B60T8/32;B64C25/42;B64C25/46;(IPC1-7):B60T8/00 主分类号 B60T8/00
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