Show simple item record

contributor authorHahn, W.
contributor authorTasker, G.
contributor authorNaylor, E.
contributor authorKidd, M.
date accessioned2017-05-09T01:07:42Z
date available2017-05-09T01:07:42Z
date issued2014
identifier issn1528-8919
identifier othergtp_136_06_062504.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154729
description abstractThe impact of multiple erosion pits and crack initiation was investigated for a 500 megawatt (MW) steam turbine unit with three low pressure (LP) rotors on the steam end and generator end of the stage L0 blades. These units have been subjected to twoshifting operation and have been retrofitted with new high pressure (HP) turbine units over the life history of the turbines. Droplet erosion damage was exacerbated by operating conditions causing multiple crack initiation sites concentrated above the root platform. A method of accumulated damage was employed using pit counting and the number of cycles referenced back to turbine revolutions in line with the accumulated damage model developed from the damage function analysis and Palmgren–Miner approaches. The number of rotational cycles were calculated from the starts and running hours for preand postretrofit scenarios and compared and correlated to the number of pits formed during the completed cycles. The macro crack size represented the critical crack size or a damage number of one. It was found that there was a significant shift in the number of rotations before and after the HP turbine retrofit to achieve a damage rate of one. An accumulated damage model was developed for the post HP turbine retrofit and the LP turbine last stage blades fitted from new, based on the empirical evidence from the analysis. Assessments on the erosion distribution in the zoned areas revealed evidence of cracking, manifesting 18 mm away from the highest probability distribution with a standard deviation of 2 mm. The area where cracking first initiated on multiple samples was found to coincide with the mechanical change in the section blending in with the blade trailing edge. The damage model was implemented on a ive running plant and successfully applied over a period of two years using the most conservative approach, based on the lower bound values.
publisherThe American Society of Mechanical Engineers (ASME)
titleCrack Initiation in 14% Cr Low Pressure Turbine Blade Steel
typeJournal Paper
journal volume136
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4026453
journal fristpage62504
journal lastpage62504
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 006
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record