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Gasutaabinenjinyoenshinkonpuretsusa

机译:加斯特·阿比(Gaster Abi)年度雌猴新作系列

摘要

A centrifugal compressor assembly for a gas turbine engine includes an inducer section and an impeller section mounted for rotation about an axis. Because leading edges of the impeller blades are cambered, damper pads, extending perpendicular to the low pressure sides thereof also extend axially forward. Blades of the inducer section are indexed rotationally rearward of the impeller blades to improve the distribution of compression gases through the impeller section and high pressure surfaces of the inducer blades mate near their leading edges with outward surfaces of the damper pads. Because the pads and inducer blades vibrate at different frequencies, inducer blade vibrations that might otherwise cause fatigue are attenuated by contact with the damper pads. The damper pad arrangement thus permits the damping of vibrations in the inducer blades notwithstanding the indexed relationship between the inducer section and the impeller section.
机译:用于燃气涡轮发动机的离心压缩机组件包括安装成可绕轴线旋转的吸入器部分和叶轮部分。因为叶轮叶片的前缘是弧形的,所以垂直于其低压侧延伸的阻尼垫也轴向向前延伸。诱导器部分的叶片在叶轮叶片的旋转方向上向后转位,以改善通过叶轮部分的压缩气体的分布,并且诱导器叶片的高压表面在其前缘附近与减震垫的外表面配合。由于垫板和诱导叶片以不同的频率振动,因此与阻尼垫接触会减弱原本可能导致疲劳的诱导叶片振动。因此,尽管在诱导器部分和叶轮部分之间存在分度关系,但是阻尼垫装置允许阻尼在诱导器叶片中的振动。

著录项

  • 公开/公告号JPS5187609A

    专利类型

  • 公开/公告日1976-07-31

    原文格式PDF

  • 申请/专利权人 DEERE & CO;

    申请/专利号JP19750136789

  • 发明设计人 HOOMAA JETSUSE UTSUDO;

    申请日1975-11-13

  • 分类号F04D29/44;F01D5/04;F02C3/06;F02C3/08;F04D29/28;

  • 国家 JP

  • 入库时间 2022-08-23 03:12:09

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