Tail nozzle structure suitable for double-duct turbofan engine

The invention discloses an exhaust nozzle structure suitable for a double-duct turbofan engine, relates to the technical field of aero-engines, and aims to reduce the difficulty of stable connection of an exhaust nozzle on the double-duct engine. An exhaust nozzle structure suitable for a double-duc...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	TONG YINGDONG, PAN QINGWEI, REN QUANLONG, CAO HAOBO, YANG XIAOJIE, YANG JINHU, CONG BINGYU, HUANG ANQI, LIU YUAN, LAN JIAZHE, LI SHIJIE, PAN WUYI, SHI HONGHAO, ZHANG WEI, CHENG JIAN, LI SHANCHENG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!