发明名称 PROCEDE DE REALISATION D'ALVEOLES D'UN DISQUE DE TURBOMACHINE
摘要 A method for producing cavities in a turbomachine disk, the cavities extending between first and second lateral surfaces of the disk, the method including positioning a ring facing the first surface, the ring including an inner periphery including protrusions complementary in shape to the cavities that are to be produced; circulating an electrolyte close to the protrusions on the ring; activating a first translational movement of the ring towards the second surface; activating a rotation of the disk; generating an electric current pulse in the electrolyte when the ring is substantially at the first surface, the pulse resulting in the ionic dissolution of the disk at the protrusions; reducing the speed of rotation to a first reduced speed, when the ring is substantially at the first surface, for a first period of time; and stopping the first translation of the ring when the ring is beyond the second surface.
申请公布号 FR3006925(B1) 申请公布日期 2016.01.15
申请号 FR20130055647 申请日期 2013.06.17
申请人 SNECMA 发明人 LECOMTE JANVIER;BUELYHA JEAN-MICHEL;KRAFT JURI;ANDREAS GRUTZMACHER
分类号 B23H3/00;B23P15/00 主分类号 B23H3/00
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