The invention belongs to the technical field of helicopter fuel systems, and discloses a helicopter fuel pipeline integrated system. The system is composed of a first control valve, a second control valve, a third control valve, a fourth control valve, a fifth control valve, a sixth control valve, a seventh control valve, a transfer pump, a pressure oil filling port cover, a one-way valve, a booster pump, a pressure oil filling control valve, a first fuel tank, a second fuel tank, a first external oil tank and a second external oil tank. A set of pipeline is used for achieving the functions offuel oil transfer, pressure refueling and external oil tank oil transportation.
本发明属于直升机燃油系统技术领域,公开了一种直升机燃油管路集成系统。由第一控制阀、第二控制阀、第三控制阀、第四控制阀、第五控制阀、第六控制阀、第七控制阀、转输泵、压力加油口盖、单向阀、增压泵、压力加油控制阀、第一燃油箱、第二燃油箱、第一外挂油箱、第二外挂油箱组成。使用一套管路分别实现燃油转输、压力加油、外挂油箱输油功能。
Helicopter fuel pipeline integrated system
一种直升机燃油管路集成系统
2021-01-05
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
DISCHARGE METHOD AND BLEED MANIFOLD OF HELICOPTER FUEL PIPELINE
European Patent Office | 2017
|HELICOPTER SUBFLOOR-INTEGRATED FUEL-TANK CRASHWORTHINESS
British Library Conference Proceedings | 2006
|Helicopter FUEL Economy Evaluation
SAE Technical Papers | 1998