Disclosed is a hydraulic system (300) for an aircraft. The hydraulic system (300) comprises a backup hydraulic pressure source (216) to provide hydraulic pressure to a brake (222) in the event of a failure condition of a primary hydraulic brake pressure source. The hydraulic system (300) also comprises a landing gear backup system to provide hydraulic pressure to enable extension and/or retraction of landing gear (100). The backup hydraulic pressure source (216) is arranged to provide hydraulic pressure to the landing gear backup system in the event of a failure condition of a primary landing gear hydraulic pressure source.
AIRCRAFT HYDRAULICS
FLUGZEUGHYDRAULIK
SYSTÈME HYDRAULIQUE D'AÉRONEF
2018-12-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
SLUB | 1957
SLUB | 1957
Engineering Index Backfile | 1943
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