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...
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Main Authors | , , , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
15.03.2024
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Subjects | |
Online Access | Get full text |
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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 |
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Bibliography: | Application Number: CN202410167400 |