The invention provides a hydraulic system (14) for integrating in an aircraft (10) and for supplying hydraulic power to one or more hydraulic components (16) of the aircraft (10) by means of an operating fluid, the hydraulic system (14) comprising a system pumping device (26) for priming operating fluid from a system inlet (24) of the hydraulic system (14) and for pumping operating fluid thereinto.
HYDRAULIC SYSTEM FOR AN AIRCRAFT, HYDRAULIC ARRANGEMENT, AIRCRAFT, AIRCRAFT ARRANGEMENT, AND METHOD FOR TESTING SUCH HYDRAULIC SYSTEM
HYDRAULIKSYSTEM FÜR EIN FLUGZEUG, HYDRAULISCHE ANORDNUNG, FLUGZEUG, FLUGZEUGANORDNUNG UND VERFAHREN ZUM TESTEN SOLCH EINES HYDRAULIKSYSTEMS
SYSTÈME HYDRAULIQUE POUR UN AÉRONEF, AGENCEMENT HYDRAULIQUE, AÉRONEF, AGENCEMENT D'AÉRONEF ET PROCÉDÉ DE TEST D'UN TEL SYSTÈME HYDRAULIQUE
2025-05-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein |
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