| 摘要 |
PROBLEM TO BE SOLVED: To provide a novel braking structure for proposing an excellent compromise in terms of weight, performance, usability and reliability of the structure. SOLUTION: The hydraulic braking structure is provided for an aircraft having a plurality of wheels attached with a brake (102). In the braking structure, the respective brakes include two semi-cavities (102a and 102b), and the structure includes a first braking circuit (N1) including a plurality of servo valves (103), that is, the first braking circuit for supplying power to one or a plurality of semi-cavities of a separate brake by the respective servo valves, and a second braking circuit (N2) including a plurality of servo valves (104), that is, the second braking circuit for supplying power to the one or the plurality of semi-cavities of the separate brake by the respective servo valves. With respect to the respective brakes, the power is supplied to at least one semi-cavity by the servo valves for supplying the power only to the semi-cavities. COPYRIGHT: (C)2011,JPO&INPIT
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