Aero-engine low-pressure turbine shaft-disk assembly assembling device, has turbine shaft position adjusting table mounted on turbine shaft position adjusting table pedestal, and tightening shaft fixed to circumferential of bolt. | |
GAO H ZHOU T | |
2018 | |
公开日期 | 2018-05-15 |
URL标识 | 查看原文 |
申请日期 | 2017-11-27 |
WOS记录号 | [DB:DC_IDENTIFIER_WOSID] |
内容类型 | 专利 |
URI标识 | http://www.corc.org.cn/handle/1471x/3262951 |
专题 | 大连理工大学 |
作者单位 | UNIV DALIAN TECHNOLOGY (UYDA-C |
推荐引用方式 GB/T 7714 | GAO H ZHOU T. Aero-engine low-pressure turbine shaft-disk assembly assembling device, has turbine shaft position adjusting table mounted on turbine shaft position adjusting table pedestal, and tightening shaft fixed to circumferential of bolt.. 2018-01-01. |
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