Cavity pressure test structure for air system of aero-engine

The invention belongs to the technical field of aero-engine air system cavity pressure test design, and particularly relates to an aero-engine air system cavity pressure test structure comprising an air system side wall provided with a cavity pressure measuring hole; the air inlet end of the air pip...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PAN XINZHENG, ZHANG ZHIXUE, YE GUIMING, ZHANG YUXIN, ZHAO BIN, XIE FENGKUN, ZHANG ZEPENG, ZHANG YU, GAO JIAQI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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