| 摘要 |
The method involves detecting failure, where a portion of a fuel fluid of an engine (1) is tapped off to lubricate an engine element in response to the detection of the failure. The portion of the engine fuel fluid is directed into an enclosure (5) in the engine, where the enclosure is drained in order to prevent any overfilling. The engine is placed in a safety regime limiting a field of operation in response to the detection of the failure by a low- pressure sensor. A valve (17a) is used for tapping a pipe (8). Independent claims are also included for the following: (1) a standby lubrication device (2) an engine comprising a main lubrication system (3) a vehicle comprising a lubrication device (4) an aircraft comprising an engine. |
