Turbine interstage outer flow channel stator piece connecting structure

The invention provides a turbine interstage outer flow channel stator part connecting structure, and belongs to the technical field of aero-engines. The rear mounting edge of the low-pressure turbine guide vane is inserted into a casing rear hook of the low-pressure turbine casing, and axial positio...

Full description

Saved in:
Bibliographic Details
Main Authors MA SHIYAN, LI HONGLEI, LIU WENDONG, LIU MEI, YUAN CHANG, TIAN JING, CAO MAOGUO, ZHAN YUEXIN, CHENG RONGHUI
Format Patent
LanguageChinese
English
Published 15.03.2024
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:The invention provides a turbine interstage outer flow channel stator part connecting structure, and belongs to the technical field of aero-engines. The rear mounting edge of the low-pressure turbine guide vane is inserted into a casing rear hook of the low-pressure turbine casing, and axial positioning is achieved through a check block assembled in a groove in the rear side of the casing rear hook; the high-pressure outer ring mounting ring is connected to the low-pressure turbine case, and a mounting ring front mounting structure and a mounting ring rear hook are arranged on the inner side of the high-pressure outer ring mounting ring; the high-voltage outer ring is provided with a matching installation structure and a rear groove, the matching installation structure is matched with the installation ring front installation structure and the installation ring rear hook, and the high-voltage outer ring and the high-voltage outer ring installation ring are installed in a matched mode to form a high-voltage out
Bibliography:Application Number: CN202410167400