Micro aero-engine fuel manifold nozzle and oil mixing test method thereof

The invention discloses a micro aero-engine fuel manifold nozzle. The micro aero-engine fuel manifold nozzle comprises a nozzle base, a rotational flow core, an auxiliary nozzle and a main nozzle. The auxiliary nozzle is arranged in the main nozzle; after the main nozzle is installed on the nozzle b...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LENG BIN, HUANG SHAOQI, QIU SHUBIN, YIN SHENGGUANG, YANG LIYING, YANG JIN, AN YUEPING, TANG HUA, HUANG DEMIN, XIONG JIAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MEASURING MECHANICAL ENGINEERING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS
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