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contributor authorF. Caruel
contributor authorK. Harris
contributor authorG. L. Erickson
contributor authorS. Bourguignon
contributor authorB. Lallement
contributor authorJ. B. Wahl
contributor authorS. Fargeas
contributor authorA. DeBussac
date accessioned2017-05-08T23:56:39Z
date available2017-05-08T23:56:39Z
date copyrightJanuary, 1998
date issued1998
identifier issn1528-8919
identifier otherJETPEZ-26775#97_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120471
description abstractFrom a cost point of view SNECMA has found DS columnar grain manufacturing technology to be highly attractive compared to single crystal. CM 186 LC alloy exhibits enhanced mechanical and environmental properties and temperature capability compared to MAR M 200 Hf alloy; these properties are close to first-generation single crystal alloys up to 982°C (1800°F). The alloy is shown to be amenable to various coating and brazing high-temperature processes. The longer term creeprupture/phase stability data base on the alloy has now been extended out to 8300 hours at 1038°C (1900°F). Castings for engine test have been produced using CM 186 LC alloy.
publisherThe American Society of Mechanical Engineers (ASME)
titleSNECMA Experience With Cost-Effective DS Airfoil Technology Applied Using CM 186 LC® Alloy
typeJournal Paper
journal volume120
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2818093
journal fristpage97
journal lastpage104
identifier eissn0742-4795
keywordsAlloys
keywordsAirfoils
keywordsCrystals
keywordsCoating processes
keywordsCoatings
keywordsStability
keywordsTemperature
keywordsEngines
keywordsBrazing
keywordsManufacturing technology
keywordsDatabases AND High temperature
treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 001
contenttypeFulltext


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