A feasibility study on the use of foil bearings in cryogenic turbopumps-Reference-Cited by-同舟云学术

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A feasibility study on the use of foil bearings in cryogenic turbopumps

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:27th Joint Propulsion Conference
language:
Short-container-title:

Author:

HESHMAT HOOSHANG¹

Affiliation:

1. Mechanical Technology, Inc., Latham, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-2103

Reference5 articles.

1. Analysis of compliant foil bearings with spatially variable stiffness

2. Heshmat, H. "lnvestigation of Foil Bearings for Use in High Thrust Liquid Rocket Engines," HTI Report 90TR58, prepared for NASA-LeRC, Conicact No. NAS3-25818, NASA Contractor Report, No. 187099, April 1991.

3. Research Center under NASA Contract No. NAS3-25818.

Cited by 10 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. Theoretical Evaluation of Lubrication Performance of Thrust-Type Foil Bearings in Liquid Nitrogen;Lubricants;2024-07-17

2. An Overview of Bearing Candidates for the Next Generation of Reusable Liquid Rocket Turbopumps;Chinese Journal of Mechanical Engineering;2020-03-17

3. Experimental Investigation of Prototype Water-Lubricated Compliant Foil Bearings;Key Engineering Materials;2011-09

4. Testing of a Small Turbocharger/Turbojet Sized Simulator Rotor Supported on Foil Bearings;Journal of Engineering for Gas Turbines and Power;2008-03-26

5. Principles of Gas Turbine Bearing Lubrication and Design;Handbook of Lubrication and Tribology;2006-04-06

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