Effects of tip clearance, number of teeth, and tooth front angle on the sealing performance of straight and stepped labyrinth seals-Reference-Cited by-同舟云学术

Effects of tip clearance, number of teeth, and tooth front angle on the sealing performance of straight and stepped labyrinth seals

Published:2021-03-24 Issue:4 Volume:35 Page:1539-1547
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Lee Soo In,Kang Young Jun,Kim Woo Jun,Kwak Jae Su,Kim Tong Seop,Kim Dong Hyun,Jung Il Young

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

https://link.springer.com/content/pdf/10.1007/s12206-021-0318-5.pdf

Reference22 articles.

1. R. E. Chupp, R. C. Hendricks, S. B. Lattime and B. M. Steinetz, Sealing in turbomachinery, NASA Technical Report, NASA/TM-2006-214341 (2006).

2. B. M. Steinetz, R. C. Hendricks and M. J. Braun, Turbomachine sealing and secondary flows, Part 1— Review of sealing performance, customer, engine designer, and research issues, NASA Technical Report, NASA/TM-2004-211991/Part1 (2004).

3. L. Bozzi, E. D’Angelo, B. Facchini, M. Micio and R. Da Soghe, Experimental investigation on leakage losses and heat transfer in a non conventional labyrinth seal, ASME Turbo Expo: Turbine Technical Conference and Exposition (2011) 955–965.

4. G. Vermes, A fluid mechanics approach to the labyrinth seal leakage problem, ASME Gas Turbine Power and Hydraulic Divisions Conference and Exhibi (1960) V001T02A012-V001T02A012.

5. H. M. Martin, Labyrinth packings, Engineering, 85 (1908) 35–36.

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