发明名称 TURBINE ROTOR FOR A TURBOMACHINE
摘要 A turbine rotor for a turbomachine, including a disk containing slots for mounting vane roots, each slot being defined by two adjacent teeth of the disk, the vane roots including contact surfaces bearing on contact surfaces of the teeth of the disk. Foils are mounted on the teeth of the disk, each foil having a general U-shape including lateral bearing parts inserted between the corresponding contact surfaces of the vane roots and teeth of the disk, and a central part facing the peak of the corresponding tooth of the disk and defining a cavity between said peak and the foil. The turbine rotor also includes a device for supplying cooling air into said cavity.
申请公布号 US2015322796(A1) 申请公布日期 2015.11.12
申请号 US201314423536 申请日期 2013.08.29
申请人 SNECMA 发明人 ROUSSELY-ROUSSEAU Amaury;BURLET Guy;MAREIX Jean Pierre
分类号 F01D5/08;F01D5/30 主分类号 F01D5/08
代理机构 代理人
主权项 1. A turbine rotor for a turbomachine, comprising a disk containing slots for mounting vane roots, with each slot being defined by two adjacent teeth of the disk, with the vane roots comprising contact surfaces bearing on contact surfaces of the teeth of the disk, wherein foils are mounted on the teeth of the disk, with each foil having a general U-shape comprising lateral bearing parts inserted between the corresponding contact surfaces of the vane roots and the teeth of the disk, and a central part facing the peak of the corresponding tooth of the disk and defining a cavity between said peak and the foil, with the turbine rotor comprising a device for supplying cooling air into said cavity.
地址 Paris FR