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Aero-engine low-pressure turbine shaft-disk component assembling method, involves rotating turbine shaft supporting rod, supporting turbine shaft by fastening bolt at connecting disk, and retracting tightening system to turbine shaft. 专利
申请日期: 2018-01-01, 公开日期: 2018-05-18
作者:  GAO H ZHOU T
收藏  |  浏览/下载:9/0  |  提交时间:2019/12/02
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. 专利
申请日期: 2018-01-01, 公开日期: 2018-05-15
作者:  GAO H ZHOU T
收藏  |  浏览/下载:6/0  |  提交时间:2019/12/02
Cylinder-based contact-type displacement sensor group aero-engine low-pressure turbine shaft disk fastening force detection method, involves determining deviation value according to relationship between difference and pre-tightening force. 专利
申请日期: 2016-01-01, 公开日期: 2016-12-21
作者:  MA Y HUANG W JIANG Y SUN W SUN Q ZH
收藏  |  浏览/下载:3/0  |  提交时间:2019/12/09


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