Impact of Material on the Sealing Behaviour of Radial Segmented Seals
Author:
Affiliation:
1. SAE: Safran Aircraft Engines
2. CETIM: Technical Centre of Mechanical Industries
3. Institut PPRIME, UPR CNRS 3346, Université de Poitiers, ISAE ENSMA
4. Laboratoire Génie de Production (LGP), Université de Toulouse, INP-ENIT
Publisher
Japanese Society of Tribologists
Link
https://www.jstage.jst.go.jp/article/trol/19/4/19_287/_pdf
Reference19 articles.
1. [1] Burcham RE. Liquid rocket engine turbopump rotating-shaft Seal. NASA S-8121. 1978.
2. [2] Allen GP. Comparison of analysis and experiment for self-acting seals for liquid-oxygen turbopumps. NASA. NASA TP-1443. 1979.
3. [3] Burcham RE. High-speed cryogenic self-acting shaft seals for liquid rocket turbopumps. NASA CR-168194. 1983.
4. [4] Nosaka M. Cryogenic tribology of high-speed bearings and shaft seals in liquid hydrogen. Tribology Online. 2011;6(2): 133-141.
5. [5] Oike M, Nosaka M, Watanabe Y, Kikuchi M, Kamijo K. Experimental study on high- pressure gas seals for a liquid oxygen turbopump. STLE Transactions. 1988;31(1): 91-97.
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