Multi-segment shaft joint rotor dynamic balance method for small aeroengine

The invention belongs to the technical field of dynamic balance, and particularly relates to a multi-segment shaft joint rotor dynamic balance method for a small aeroengine. According to the invention, based on a mechanical vibration test method, the vibration of a rotor is transferred to test on a...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: YUE HEQUN, DUO XINYU, SUN XUDONG, MIAO QINYU, LIU JIANING, LI XIA
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!