Investigation of Effective Groove Types for a Film Riding Seal
Author:
Affiliation:
1. GE Power, Newbold Road, Rugby CV21 2NH, UK e-mail:
2. Centre for Power Engineering, Cranfield University, College Road, Cranfield, Bedfordshire MK43 0AL, UK
3. GE Power, Newbold Road, Rugby CV21 2NH, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4035601/6175168/gtp_139_07_072503.pdf
Reference41 articles.
1. Development of Film Riding Seals for a Gas Turbine Engine;Tribol. Trans.,1992
2. Advanced Seal Technology Role in Meeting Next Generation Turbine Engine Goals,1998
3. Testing of a High Performance Compressor Discharge Seal,1993
4. Development of Non-Contacting, Low-Leakage, Large-Diameter Air Seal,2008
5. Development of Mainshaft Seals for Advanced Air Breathing Propulsion Systems,1973
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2. Steady-State Characteristics of Spiral Groove Floating Ring Gas-film Seal Considering Temperature-Viscosity Effect;Journal of Applied Fluid Mechanics;2023-04-01
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4. Performance analysis of compliant cylindrical intershaft seal;Science Progress;2020-07
5. Detailed Study on Stiffness and Load Characteristics of Film-Riding Groove Types Using Design of Experiments;Journal of Engineering for Gas Turbines and Power;2017-04-11
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