Show simple item record

contributor authorChilds, Dara W.
contributor authorArthur, Stephen
contributor authorMehta, Naitik J.
date accessioned2017-05-09T01:07:32Z
date available2017-05-09T01:07:32Z
date issued2014
identifier issn1528-8919
identifier othergtp_136_04_042501.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154684
description abstractTest results are presented for rotordynamic characteristics of holepatternstator annular gas seals at a 70 bar supply pressures with a running speed of 20,200 rpm. Leakage results are presented for these conditions and the additional speeds: 10,200 and 15,300 rpm. Holedepth is the principal test variable of interest. Most published annular test data for these seals have a hole diameter of 3.175 mm and a hole depth of 3.302 mm. For this work, with the 3.175 mm hole diameter, additional results are presented for shallow (1.905 mm) and deep (6.604 mm) hole depths. Test results show a pronounced dependence of leakage and rotordynamic behavior on hole depth. Test results show much better leakage performance for the shallowholedepth seal in both leakage and rotordynamic performance. Compressor manufacturers and users will need to decide whether this observed performance improvement is worth trying in real machines.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Impact of Hole Depth on the Rotordynamic and Leakage Characteristics of Hole Pattern Stator Gas Annular Seals
typeJournal Paper
journal volume136
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4025888
journal fristpage42501
journal lastpage42501
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 004
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record