发明名称 |
HYDRAULIC AIRCRAFT SYSTEM INCLUDING AT LEAST ONE SERVO, ASSOCIATED ROTOR AND AIRCRAFT |
摘要 |
A hydraulic system of an aircraft, the system comprising at least one servo-control, each servo-control comprising at least one cylinder together with a drive rod and a piston arranged in each cylinder. Between each cylinder of servo-control and the drive rod of that servo-control, at least one servo-control presents main sealing means with controlled leakage allowing a hydraulic fluid to leak out from the cylinder, the hydraulic system further comprising at least one enclosure, each cylinder of the servo-control being arranged inside the enclosure so that the fluid is collected in the enclosure. |
申请公布号 |
EP2933186(B1) |
申请公布日期 |
2016.07.06 |
申请号 |
EP20150000848 |
申请日期 |
2015.03.23 |
申请人 |
AIRBUS HELICOPTERS |
发明人 |
BIHEL, JEAN-ROMAIN;COÏC, CLÉMENT;MARGER, THIBAUT;COUDERC, GÉRARD |
分类号 |
B64C27/64;F15B15/14 |
主分类号 |
B64C27/64 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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