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Turbine Bearing And Seal Removal Fixture For Industrial Gas Turbine

Abstract: The Fixture has been designed to overcome the frequent puller lip failure of OEM suggested tool. This fixture is used to push the bearing and labyrinth seal out from turbine shaft in place of using puller lip tool to pull the seals. This fixture gives the benefit of repetitive use without any failure. This tool can be easily be mounted on the turbine rear side and by applying force on the tool bearing will be pushed out. This applies equal pressure on inner race thus prevents any localized damage to component.

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Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
03 April 2023
Publication Number
40/2024
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

HINDUSTAN AERONAUTICS LIMITED
CV RAMAN NAGAR, BANGALORE, KARNATAKA, INDIA, 560093.

Inventors

1. Mr. SANTOSH KUMAR
HINDUSTAN AERONAUTICS LIMITED, CV RAMAN NAGAR, BANGALORE, KARNATAKA, INDIA, 560093.
2. Mr. SATHISHA M
HINDUSTAN AERONAUTICS LIMITED, CV RAMAN NAGAR, BANGALORE, KARNATAKA, INDIA, 560093.
3. Mr BALRAM SING B P
HINDUSTAN AERONAUTICS LIMITED, CV RAMAN NAGAR, BANGALORE, KARNATAKA, INDIA, 560093.

Specification

1 Title of the Invention

Turbine bearing and seal removal fixture for Industrial gas turbine.

2 Field of the Invention

The present invention relates to manufacturing, repair, overhaul of Gas Turbines.

3 Background of the Invention

Tool/fixture suggested by OEM for removal of the turbine front bearing and labyrinth seal is having frequent problem with failure of puller lips / damage of engine components during strip of the engine. This resulting in frequent repair of tools and replacement of damaged components. There was need for tool which can remove the items without damage.

4 Brief Summary of the Invention

The Fixture has been manufactured to overcome the frequent puller lip failure of OEM suggested tool. This fixture is used to push the bearing and labyrinth seal out from turbine shaft in place of using puller lip tool to pull the seals. This fixture gives the benefit of repetitive use without any failure.

This tool can be easily be mounted on the turbine rear side and by applying force on the tool bearing will be pushed out. This applies equal pressure on eight locations on real and inner race thus prevents any localized damage to components.

5 Detail Description of the Drawings

FIG-1 Schematically illustrates the parts of the fixture.
6 Detail Description of the Invention Construction:

support plate (1) is rigidly fixed (welded) with guide pins (2) to provide a rigid fixture to withstand the applied load during removal of the bearing race. This also provide equal distribution of the applied force on the periphery to prevent any local damage of engine components.

Function :

This tool can be easily be mounted on the turbine rear side and by applying force on the tool, bearing will be pushed out. This applies equal pressure on eight locations on real and inner race thus prevents any localized damage to components.

Documents

Application Documents

# Name Date
1 202341025200-Form5_As Filed_03-04-2023.pdf 2023-04-03
2 202341025200-Form3_As Filed_03-04-2023.pdf 2023-04-03
3 202341025200-Form-2 (Title Page)_Complete_03-04-2023.pdf 2023-04-03
4 202341025200-Form-1_As Filed_03-04-2023.pdf 2023-04-03
5 202341025200-Drawing_As Filed_03-04-2023.pdf 2023-04-03
6 202341025200-Description Complete_As Filed_03-04-2023.pdf 2023-04-03
7 202341025200-Correspondence_As Filed_03-04-2023.pdf 2023-04-03
8 202341025200-Claims_As Filed_03-04-2023.pdf 2023-04-03
9 202341025200-Abstract_As Filed_03-04-2023.pdf 2023-04-03