The present disclosure relates to a method of installing a modular water system in an aircraft (1), including installing a water backbone assembly (100) extending over a length of an aircraft section (10) and connecting a pump (155) with a standard water consumer (90). The water backbone assembly (100) comprises at least one backbone conduit (105) and can be provided with connection fittings (110, 112, 114), in order to fluidly connect one or more branch conduits (120, 122, 125) to the backbone conduit (105). Further disclosed are an aircraft section (10) and an aircraft (1) having such water system installed therein.
METHOD OF INSTALLING A MODULAR WATER SYSTEM IN AN AIRCRAFT SECTION, AND AIRCRAFT SECTION AS WELL AS AIRCRAFT COMPRISING SUCH WATER SYSTEM
VERFAHREN ZUR INSTALLATION EINES MODULAREN WASSERSYSTEMS IN EINEM FLUGZEUGABSCHNITT UND FLUGZEUGABSCHNITT SOWIE FLUGZEUG MIT SOLCH EINEM WASSERSYSTEM
PROCÉDÉ D'INSTALLATION D'UN SYSTÈME D'EAU MODULAIRE DANS UNE SECTION D'AÉRONEF, ET SECTION D'AÉRONEF AINSI QU'AÉRONEF COMPRENANT UN TEL SYSTÈME D'EAU
2025-04-30
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft having drinking water system and method for installing drinking water system in aircraft
European Patent Office | 2025
|Aircraft having drinking water system and method for installing drinking water system in aircraft
European Patent Office | 2025
|Aircraft nacelle section and aircraft having aircraft nacelle section
European Patent Office | 2022
|Interior aircraft section comprising cover and corresponding aircraft
European Patent Office | 2024
|