| 摘要 |
<p>The invention relates to a blade (11) for a turbine, comprising a foot (13) enabling it to be protracted into a honeycomb element (14) of a disk (12) of said turbine, provided with an internal air cooling circuit comprising means for admitting air (15) disposed on the foot of the blade opposite the honeycomb element, and means for discharging air. The foot (13) of the blade is provided with means (20) for homogenizing the pressure and temperature of the cooling air entering the means for admitting air.</p> |
