A fuel pump arrangement has multiple fuel pumps for fitting to aircraft fuel tanks and allowing maintenance of the pumps without requiring access from inside the tanks, particularly one having a housing with two fuel pumps for mounting in or adjacent a single aperture in the wall of a fuel tank, each pump being individually removable from the housing by withdrawal away from the tank. A sleeve is moveable also in the same direction as the pump to obstruct inlets in the housing and isolate the housing from the fuel in the tank so the tank need not be drained.
IMPROVEMENTS IN AND RELATING TO FUEL PUMP ARRANGEMENTS
2016-09-08
Patent
Electronic Resource
English
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile / 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 |