| 摘要 |
The present disclosure relates to isolation and reconfiguration schemes, architectures and methods for use in aircraft hydraulic systems (100). The main hydraulic system (104) of each hydraulic section (102a, 102b) of the aircraft hydraulic system (100) can be isolated from one or more consumers (110) in the event of a leak without the use pressure from the backup system (108). Further, in some embodiments, the main hydraulic system (104) of each hydraulic section (102a, 102b) of the aircraft hydraulic system (104) can be isolated from one or more consumers (110) in the event of a leak without the use pressure from the backup system (108) and the main system (104). |
