发明名称 MODULAR POWER PLANT AND AN AIRCRAFT PROVIDED WITH A LIFT ROTOR
摘要 A power plant (10) having a main gearbox (20), a turbine engine (40), and a heat exchanger (60), the main gearbox (20) including a substantially vertical rotor mast (21). The main gearbox (20) comprises at least a rotary speed reduction stage arranged in a flat casing (22), and a pylon (23). The turbine engine (40) has an engine casing (42) with an outlet shaft projecting from said engine casing (42) and penetrating into said flat casing (22), said outlet shaft (41) being substantially parallel to the rotor mast (21), said engine casing (42) being offset longitudinally from the pylon (23) and not being in contact with the pylon (23). The heat exchanger (60) extends longitudinally behind said turbine engine (40), while, on the contrary, said rotor mast (21) is situated longitudinally in front of said turbine engine (40).
申请公布号 US2015284074(A1) 申请公布日期 2015.10.08
申请号 US201414330170 申请日期 2014.07.14
申请人 AIRBUS HELICOPTERS 发明人 HONNORAT Olivier
分类号 B64C27/12;F16H57/025;F02C7/36;B64C27/473;F02C7/12;F02C7/20 主分类号 B64C27/12
代理机构 代理人
主权项 1. A power plant having a main gearbox and a turbine engine, the main gearbox having a substantially vertical rotor mast suitable for rotating a hub of a rotor, the turbine engine having an outlet shaft for driving said main gearbox, said power plant having a heat exchanger fastened on said turbine engine, wherein: said main gearbox has at least one rotary speed reduction stage arranged in a flat casing and a pylon standing on a top face of said flat casing, said pylon having said rotor mast passing therethrough; said turbine engine includes an engine casing, said outlet shaft projecting from said engine casing, said outlet shaft penetrating into said flat casing when said engine casing is arranged on said top face, said outlet shaft being substantially parallel to the rotor mast, said engine casing being offset longitudinally relative to the pylon and not being in contact with the pylon; and said heat exchanger extends longitudinally behind said turbine engine, said rotor mast being situated on the contrary longitudinally in front of said turbine engine.
地址 Marignane FR