| 摘要 |
The invention concerns a device for locking an engine on an aircraft pylon (10) comprising a main lock-on structure and a standby lock-on structure (52). The main lock-on structure comprises a bracket (16) fixed to the pylon (10), and at least two connecting rods (18, 20) on spherical mounting connecting the anchor fitting (16) to the engine. The standby lock-on structure (52), through which no effort is exerted when the main lock-on structure is operative, directly connects, with clearance, the pylon (10) to the engine. It comprises, for example, a yoke (54) integral with the pylon (10) and passing through a window formed in the anchor fitting (16), or a connecting rod articulated on the engine and on the pylon.
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