Filtration device for aircraft with filter rotation stop

B - Operations – Transporting – 01 – D

Patent

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Details

B01D 35/30 (2006.01) B01D 27/08 (2006.01) F02C 7/06 (2006.01) F16N 39/06 (2006.01)

Patent

CA 2658066

The invention concerns a filtering device for aircraft has a hydraulic block made of titanium and receiving a removable filter, where the filter comprises a tank for receiving a filtering cartridge. An insert is screwed in an internal thread of the block by tightening. The insert has an internal thread, in which the tank is screwed. A rotation stopping unit is formed of a shoulder and a toothed tab for stopping rotation of the tank, once the tank is screwed in the insert.

L'invention concerne un dispositif de filtrage pour aéronef comprenant un bloc hydraulique adapté à recevoir un filtre amovible qui comporte une cuve recevant une cartouche. Conformément à l'invention, un insert est vissé avec serrage dans un taraudage du bloc hydraulique, l'insert comportant lui-même un taraudage dans lequel la cuve est vissée, le dispositif comportant en outre des moyens d'arrêt en rotation de la cuve une fois celle-ci vissée dans l'insert.

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