Aircraft refuelling device including a fuel circulation pipe of which the downstream end is equipped with a wing coupling for connecting it to an inlet orifice of a fuel tank of the aircraft. The wing coupling includes a body which defines a fuel circulation duct at the end of the pipe, a sensor for measuring the value of a parameter indicative of a flow of fuel passing through the wing coupling, and at least one battery electrically powering the sensor. The sensor and the electrical power supply battery are housed in two half-shells mounted together around the body of the wing coupling.
УСТРОЙСТВО ДЛЯ ЗАПРАВКИ ЛЕТАТЕЛЬНОГО АППАРАТА И СПОСОБ ИЗГОТОВЛЕНИЯ КРЫЛЬЕВОГО РАЗЪЕМА ДЛЯ ТАКОГО УСТРОЙСТВА
2022-03-04
Patent
Electronic Resource
Russian
IPC: | 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 |
European Patent Office | 2022
ДВИЖИТЕЛЬНОЕ УСТРОЙСТВО ДЛЯ ЛЕТАТЕЛЬНОГО АППАРАТА, ТАКОГО КАК ТУРБОВИНТОВОЙ САМОЛЕТ
European Patent Office | 2020
УЗЕЛ ШАССИ ЛЕТАТЕЛЬНОГО АППАРАТА И СПОСОБ СБОРКИ ТАКОГО УЗЛА
European Patent Office | 2019
СПОСОБ И ОСНАСТКА ДЛЯ ИЗГОТОВЛЕНИЯ КОМПОЗИТНОЙ РАМЫ ИЛЛЮМИНАТОРА ЛЕТАТЕЛЬНОГО АППАРАТА
European Patent Office | 2022