Nozzle insulation structure for thrust steering jet engines

The invention relates to a nozzle insulation structure for thrust steering jet engines. The structure is suitable for field of medium and small thrust aero-engines having thrust steering demands. Thestructure consists of 1 # heat shield (9), 2 # heat shield (8), 3 # heat shield (7), 4 # heat shield...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CHEN HAOMIN, WANG RONG, LIU ZHIHUA, LI GUILIN, PAN DAIFENG, GONG LIANGLIANG, ZHANG LUJUN, TIAN SHANLIN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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