SYSTEM AND METHOD FOR LOCAL SURFACE TREATMENT

The invention concerns a system for the local surface treatment of an aeronautical part (1) to be treated. Said system is characterised in that it comprises a plurality of reservoirs (18, 19, 20, 21} each comprising a treatment product (22, 23, 24, 25), at least one bath box (102a, 102b) suitable fo...

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Bibliographische Detailangaben
1. Verfasser:	RIVES, BERTRAND
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT APPARATUS FOR APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TOSURFACES, IN GENERAL APPARATUS THEREFOR APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TO SURFACES, IN GENERAL AVIATION CHEMISTRY COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTROFORMING ELECTROLYTIC OR ELECTROPHORETIC PROCESSES GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR METALLURGY PERFORMING OPERATIONS PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTIONOF COATINGS SPRAYING OR ATOMISING IN GENERAL TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention concerns a system for the local surface treatment of an aeronautical part (1) to be treated. Said system is characterised in that it comprises a plurality of reservoirs (18, 19, 20, 21} each comprising a treatment product (22, 23, 24, 25), at least one bath box (102a, 102b) suitable for delimiting a sealed space (26a, 26b) between said bath box (102a, 102b) and a portion (101a, 101b) of the part to be treated, and a controlled circuit (10) for supplying said sealed space (26a, 26b) with treatment product (22, 23, 24, 25) from the reservoirs (18, 19, 20, 21) linking at least said reservoir (18, 19, 20, 21) to said sealed space (26a, 26b) and comprising valves allowing the management of the supply of the sealed space by one or more reservoirs of the plurality of reservoirs. L'invention concerne un système de traitement local de surface d'une pièce (1) aéronautique à traiter. Ledit système est caractérisé en ce qu'il comprend une pluralité de réservoirs (18, 19, 20, 21} comprenant chacun un produit (22, 23, 24, 25) de traitement, au moins une boite (102a, 102b) à bain adaptée pour délimiter un espace (26a, 26b) étanche entre cette boite (102a, 102b) à bain et une partie (101a, 101b) de Sa pièce à traiter, et un circuit (10) commandé d'alimentation dudit espace (26a, 26b) étanche en produit (22, 23, 24, 25) de traitement les réservoirs (18, 19, 20, 21) reliant au moins ce réservoir (18, 19, 20, 21) audit espace (26a, 26b) étanche et comprenant des vannes permettant la gestion de l'alimentation de l'espace étanche par un ou plusieurs réservoirs de la pluralité de réservoirs.