发明申请
US20150159486A1 INFLOW SEGMENT FOR A TURBOMACHINE 审中-公开
流量分配为涡轮机

INFLOW SEGMENT FOR A TURBOMACHINE
摘要:
A turbomachine is provided having an inflow segment which carries an inflow segment vane and bores, a partial mass flow arriving through these bores at a relief space and leading to a cooling system.
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