| 摘要 |
The invention relates to an aircraft filter device comprising a hydraulic block (1) adapted to receive a removable filter (2) comprising a vessel (3) that receives a cartridge (4). In accordance with the invention, an insert (21) is screwed tightly into an internal thread (20) of the hydraulic block, the insert itself having an internal thread (22) into which the vessel is screwed, the device also including rotation-preventing means (23, 32) for preventing the vessel from moving in rotation once it has been screwed into the insert.
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