发明名称 POWER TRANSMISSION SYSTEM AND AN AIRCRAFT HAVING A ROTARY WING
摘要 A power transmission system having at least one inlet speed-reducing gear and a main speed-reducing gear, each inlet speed-reducing gear comprising an inlet pinion meshing with an inlet gearwheel. The inlet gearwheel is constrained to rotate with a main pinion of the main speed-reducing gear, the main pinion meshing with a main gearwheel. At least one inlet gearwheel is secured to reversible connection means in order to be capable of driving a first additional drivetrain connected to an additional rotor.
申请公布号 US2017073066(A1) 申请公布日期 2017.03.16
申请号 US201615265018 申请日期 2016.09.14
申请人 AIRBUS HELICOPTERS 发明人 DE MEERSCHMAN Olivier;BARAIS Olivier
分类号 B64C27/12;B64C27/06;B64C27/82;F16H1/28 主分类号 B64C27/12
代理机构 代理人
主权项 1. A power transmission system for a rotorcraft, the power transmission system having at least one inlet speed-reducing gear rotating a main speed-reducing gear, the main speed-reducing gear being for connecting mechanically to a rotor mast for driving a main rotor of the rotorcraft in rotation, the main rotor contributing at least in part to providing the rotorcraft with lift, each inlet speed-reducing gear comprising at least one inlet pinion meshing with an inlet gearwheel, each inlet pinion being for driving by an engine, the main speed-reducing gear having one main gearwheel per inlet speed-reducing gear, the main speed-reducing gear having one main gearwheel meshing with each main pinion, each main pinion being connected by a respective connection shaft to a respective inlet gearwheel, wherein at least one inlet gearwheel is constrained to rotate about an axis of rotation of the inlet gearwheel of reversible connection means, the reversible connection means being designed to be able to drive a first additional drivetrain connected to an additional rotor of the rotorcraft, the first additional drivetrain being an optional member that need not be mounted on the power transmission system.
地址 Marignane FR