Evaporating pipe guider integrated structure of turbojet engine

The invention discloses an evaporation pipe guider integrated structure of a turbojet engine, which comprises a guider rim, guider blades and a sealing disc, the guider blades are arranged in an annular cavity formed by the guider rim and the sealing disc, one end of each guider blade is fixedly con...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SONG GUANGRUI, SONG CHAO, HU XIAO'AN, ZHU YANPING, LIU JINLONG, WANG SHUYA, TENG XUEFENG, SHEN JIE, XIE YIFAN, YUAN JINCHENG, QU SHUAIBIN, HE HAIYAN, HUANG YINGJING, JIN JINLONG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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