Development of a high speed, high temperature, compressor discharge seal-Reference-Cited by-同舟云学术

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Development of a high speed, high temperature, compressor discharge seal

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Gardner James¹

Affiliation:

1. EG&G Engineered Products, Warwick, RI

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2684

Reference11 articles.

1. CompressorDischargeSeal0022,A&4-93-1997, (1997).

2. Development of Film Riding Face Seals for a Gas Turbine Engine

3. O'Brien, M. "Development of aShortLength SelfActing Seal0022,AVCO-Lycoming, NASACR-135159(1976).

4. O'Brien, M. "Development of Spiral-Groove Self-Acting FaceSeals0022,Avco Lycoming Report NASA-CR-135303,(1997).

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. 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

2. Investigation of Effective Groove Types for a Film Riding Seal;Journal of Engineering for Gas Turbines and Power;2017-02-14

3. Spiral-grooved gas face seal for steam turbine shroud tip leakage reduction: Performance and feasibility analysis;Tribology International;2016-06

4. Aeroelasticity Analysis of Air-Riding Seals for Aero-Engine Applications;Journal of Tribology;2002-05-31

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