Invention Grant
US08127525B2 System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine 有权
在燃气涡轮发动机中涡轮轴断裂的情况下耗散能量的系统

System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine
Abstract:
A device for, in a gas turbine engine, braking a turbine including a rotor, having at least one disk with a rim driving a shaft and capable of rotating with respect to a stator, is disclosed. The device is for the event of the shaft breaking and includes a first braking member, secured to the rim and provided with at least one cutting element, and a second braking member secured to the stator downstream of the rim and including a ring-shaped element made of a material that can be cut by the cutting element. The two braking members coming into contact with one another through axial displacement of the rotor once the shaft has broken. The cutting element of the first braking member cuts the ring-shaped element of the second braking member.
Information query
Patent Agency Ranking
0/0