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Study, design and optimization of clearance seals used in high speed turbo-machinery operating in cryogenic fluids and vacuum conditions

Implementing Organization

CO-Principal Investigator
Shri. Paul P. George
Liquid Propulsion Systems Centre (LPSC), Valiamala

Project Overview

Clearance seals are used in cryogenic turbopumps which work in Liquid Hydrogen/Liquid Oxygen environment during chilling phase and in vacuum conditions during operation of turbopumps. The vibration, friction and wear characteristics of seal/runner combination play a vital role in the turbopump performance. Minimum wear and heat generation and maximum life are the desirable properties of clearance seals used in turbopumps. Detailed study in this area is required to optimize the existing seal designs/ configurations and material selection.
Funding Organization
Funding Organization
Department of Space (DoS)
Quick Information
Area of Research
Astronomy & Space Sciences
Focus Area
Cryogenic Turbopump
Status
Ongoing
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
N/A
Startup (If Any)
00
No. of Patents
Filed :00
Grant :00
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