Aircraft engine blade profile machining, clamping and positioning method

The invention provides a clamping and positioning method for aircraft engine blade profile machining. The clamping and positioning method comprises the following positioning steps that firstly, a tool is used for clamping and positioning a dovetail wedge head according to the positioning requirement...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: JEON YU-JIN, DU JIAYAN, HAN SHIXIN, WANG BO, YANG LIN, GONG YONGQING, MENG SHAOXUAN, ZHOU CHUHAO
Format: Patent
Sprache:chi ; eng
Schlagworte:
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