Heat-dissipation pump body structure of civil aviation engine

The invention discloses a heat-dissipation pump body structure of a civil aviation engine. The heat-dissipation pump body structure comprises a pump body and a pump cover arranged on the left side ofthe pump body; an inserting groove and an inserting hole are distributed in the edge of the left side...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	NING XUEMEI, YUAN YAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING HEATING LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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