Hydrogen Compressor Seal Case Study - Utilizing HALO (Non-Contacting, Compliant) Inter-Stage, Impeller Eye, Buffer and Fail-Safe Seals

dc.contributor.other	Turbomachinery Symposium (42nd : 2013)
dc.creator	Justak, John
dc.date.accessioned	2017-10-04T19:33:59Z
dc.date.available	2017-10-04T19:33:59Z
dc.date.issued	2013
dc.identifier.uri	https://hdl.handle.net/1969.1/162933
dc.description	Case Study	en
dc.description.abstract	An end user of a hydrogen compressor in an oil refinery application has identified existing labyrinth seals as a source of compressor inefficiency and a potential cause of rotor- dynamic instability. The objective of this effort was to investigate the applicability of a compliant/non-contacting seal developed for aerospace applications in the 5-stage hydrogen centrifugal compressor. This effort identified the potential seal performance of the compliant seals in the hydrogen compressor application 4 primary locations (shaft seal, impeller eye seal, thrust balance seal and barrier/buffer gas seal).	en
dc.format.medium	Electronic	en
dc.format.mimetype	application/pdf
dc.language.iso	en
dc.publisher	Texas A&M University. Turbomachinery Laboratories
dc.relation.ispartof	Proceedings of the 42nd Turbomachinery Symposium	en
dc.subject.lcsh	Turbomachines	en
dc.title	Hydrogen Compressor Seal Case Study - Utilizing HALO (Non-Contacting, Compliant) Inter-Stage, Impeller Eye, Buffer and Fail-Safe Seals	en
dc.type.genre	Presentation	en
dc.type.material	Text	en
dc.identifier.doi	https://doi.org/10.21423/R1RP9D