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

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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
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Zusammenfassung: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 connected with the guider rim, and the other end of each guider blade is fixedly connected with the sealing disc. One end of the guider blade is fixedly connected with the guider rim, the other end of the guider blade is fixedly connected with the sealing disc, an evaporation pipe connecting ring is arranged on the upper surface of the guider rim, a straight evaporation pipe is arranged on the evaporation pipe connecting ring, a nozzle is arranged on the straight evaporation pipe, a fixing thin plate is arranged on the guider rim, a bolt hole is formed in the fixing thin plate, and the other end of the guider blade is fixedly connected with the sealing disc. An integrated structure is achieved through the straight eva