AIRCRAFT FILTER DEVICE WITH THE FILTER BEING STOPPED IN ROTATION
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United States of America Patent
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Issued Date -
Sep 17, 2009
app pub date -
Mar 10, 2009
filing date -
Mar 14, 2008
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
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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