Propelling system with large-range bypass ratio adjusting capacity

The invention belongs to the technical field of engine design, and particularly relates to a propelling system with the large-range bypass ratio adjusting capacity. The system comprises a turbofan engine used for generating main thrust; the generator is connected with the turbofan engine and is used...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SU GUIYING, XU XUE, HE JIAQIAN, RUI CHANGSHENG
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
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