其中,在发动机风扇、压气机、涡轮上采用整体叶盘(Blisk)结构(包括整体叶轮、整体叶环等)是提高发动机性能、简化结构、降低重量、减少故障率、提高耐久性与可靠性的重要措施。
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涡轮整体叶盘 turbine blisk
It is urgent need to develop and manufacture the blisk of dissimilar materials due to rapid progress in high thrust-weight ratio aero-engines.
研究异种材料整体叶盘的制造技术是高推重比航空发动机发展的迫切要求。
参考来源 - 线性摩擦焊接过程有限元热力耦合分析·2,447,543篇论文数据，部分数据来源于NoteExpress
整体叶盘是高推比航空发动机采用的新结构。
Blisk is a new integrated structure of blades and disk actually used in the aero-engine of high thrust-weight ratio.
本文介绍了某高压涡轮整体叶盘破裂转速的计算方法和试验验证。
In this paper, the calculation method and experimental investigation of a HP turbine blisk burst speed has been introduced.
针对闭式整体叶盘通道开槽工艺问题，研究了叶盘通道五坐标开槽插铣加工方法。
With regard to the slot process of closed blisk, a 5-axis slot plunge milling method of closed blisk is studied.
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