发明名称 TURBINE ENGINE COMPRISING A DEVICE FOR BRAKING THE FAN ROTOR
摘要 The invention relates to a turbine engine comprising a fixed structure (7), a fan (1) rotor (3), having an axis (XX) of rotation, and emergency braking means (12, 13) of the rotor (3), in particular in the event of the loss of a blade of the fan (1), characterised in that said emergency braking means (12, 13) comprise a first (18) and a second (22) member supported by the fixed structure (7), said members (18, 22) respectively being configured so as to interact frictionally with a first (20) element which is complementary to the rotor (3), by forming a stop of the rotor (3) towards the rear along the axis (XX), and a second (24) element which is complementary to the rotor (3), by forming a stop of the rotor (3) towards the front along the axis (XX), when the emergency braking means (12, 13) are active.
申请公布号 US2016097298(A1) 申请公布日期 2016.04.07
申请号 US201514876585 申请日期 2015.10.06
申请人 SNECMA 发明人 Becoulet Julien Fabien Patrick;Tan-Kim Alexandre Jean-Marie
分类号 F01D21/04;F01D5/30;F01D5/12;F01D21/00;F01D5/02;F01D9/02 主分类号 F01D21/04
代理机构 代理人
主权项 1. Turbine engine comprising a fixed structure, a fan rotor having an axis of rotation, and emergency braking means of the rotor, said emergency braking means comprising a first and a second member supported by the fixed structure, said members respectively being configured so as to interact frictionally with a first element which is complementary to the rotor, by forming a stop of the rotor towards the rear along the axis, and a second element which is complementary to the rotor, by forming a stop of the rotor towards the front along the axis, when the emergency braking means are active, characterised in that it further comprises means which are arranged so as to release at least one of said members in translation relative to the fixed structure along the axis of rotation. in the direction opposite to that for which it forms a stop, when the emergency braking means are activated.
地址 Paris FR