Show simple item record

contributor authorMicio, Mirko
contributor authorBianchini, Cosimo
contributor authorMassini, Daniele
contributor authorFacchini, Bruno
contributor authorCeccherini, Alberto
contributor authorInnocenti, Luca
date accessioned2017-05-09T01:28:34Z
date available2017-05-09T01:28:34Z
date issued2016
identifier issn1528-8919
identifier othergtp_138_07_072505.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161118
description abstractAmong the various types of seals used in gas turbine secondary air system to guarantee sufficient confinement of the main gas path, honeycomb seals perform well in terms of enhanced stability and reduced leakage flow. Due to the large amount of honeycomb cells typically employed in real seals, it is generally convenient to treat the sealing effect of the honeycomb pack as an increased distributed friction factor on the plain top surface. That is why, this analysis is focused on a simple configuration composed by a honeycomb facing a flat plate. In order to evaluate the sealing performance of such honeycomb packs, an experimental campaign was carried out on a stationary test rig where the effects of shaft rotation are neglected. The test rig was designed to analyze different honeycomb geometries so that a large experimental database could be created to correlate the influence of each investigated parameter. Honeycomb seals were varied in terms of hexagonal cell dimension and depth in a range that represents well actual honeycomb packs employed in industrial compressors. For each geometry, seven different clearances were tested. This work reports the findings of such experimental campaign whose results were analyzed in order to guide actual seals design and effective estimates of shaft loads. Static pressure measurements reveal that the effects of investigated geometrical parameters on friction factor correlate well with a corrected Mach number based on the cell depth. The presence of acoustic effects in the seals was further investigated by means of hot wire anemometry. Acoustic forcing due to flow cavity interaction was found to be characterized by a constant Strouhal number based on cell geometry. Numerical simulations helped in the identification of system eigenmodes and eigenfrequencies providing an explanation to the friction factor enhancement triggered at a certain flow speed. Finally, the generated dataset was tested comparing the predicted leakage flow with experimental data of actual seals (with high pressure and high rotational speed) showing a very good agreement.
publisherThe American Society of Mechanical Engineers (ASME)
titleFlat Plate Honeycomb Seals Friction Factor Analysis
typeJournal Paper
journal volume138
journal issue7
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4031963
journal fristpage72505
journal lastpage72505
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 007
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record