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rdf:type
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Description
| - Aerospace industry often uses nickel superalloys for blades of jet engine turbines. The reason is that this material can satisfy numerous extreme requirements, such as e. g. strength even at very high temperatures, resistance to fatigue damage, resistance to fatigue effect of combustion gases, etc. The main requirement is assurance of high operational reliability and safety at exploitation under high temperatures. Long term service life and material reliability is directly linked to its microstructure, or with its stability at long-term exploitation. These materials are usually alloyed in a complex manner and they are very complicated from structural viewpoint (1,3,8). Superalloy was commercially produced ad was investigated by use of light microscope (LM) OLYMPUS IX 71, local chemical microanalysis and scanning electron microscope (SEM) JEOL 6490 LV. The optimum heat treatment (HT) was found. The reached results enabled to recommend the optimum heat treatment including heating on the 1240 °C with
- Aerospace industry often uses nickel superalloys for blades of jet engine turbines. The reason is that this material can satisfy numerous extreme requirements, such as e. g. strength even at very high temperatures, resistance to fatigue damage, resistance to fatigue effect of combustion gases, etc. The main requirement is assurance of high operational reliability and safety at exploitation under high temperatures. Long term service life and material reliability is directly linked to its microstructure, or with its stability at long-term exploitation. These materials are usually alloyed in a complex manner and they are very complicated from structural viewpoint (1,3,8). Superalloy was commercially produced ad was investigated by use of light microscope (LM) OLYMPUS IX 71, local chemical microanalysis and scanning electron microscope (SEM) JEOL 6490 LV. The optimum heat treatment (HT) was found. The reached results enabled to recommend the optimum heat treatment including heating on the 1240 °C with (en)
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Title
| - Effect of heat treatment on the structure of IN 713LC
- Effect of heat treatment on the structure of IN 713LC (en)
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skos:prefLabel
| - Effect of heat treatment on the structure of IN 713LC
- Effect of heat treatment on the structure of IN 713LC (en)
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skos:notation
| - RIV/00176109:_____/10:#0000008!RIV11-MPO-00176109
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
| - P(FI-IM5/001), P(FT-TA3/072), P(GA106/08/1243), Z(MSM6198910013)
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http://linked.open...vai/riv/dodaniDat
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http://linked.open...aciTvurceVysledku
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http://linked.open.../riv/druhVysledku
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http://linked.open...iv/duvernostUdaju
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http://linked.open...titaPredkladatele
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http://linked.open...dnocenehoVysledku
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http://linked.open...ai/riv/idVysledku
| - RIV/00176109:_____/10:#0000008
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - nickel superalloy; phase analysis; intermetallic y phase; heat treatment (en)
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http://linked.open.../riv/klicoveSlovo
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http://linked.open...ontrolniKodProRIV
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http://linked.open...v/mistoKonaniAkce
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http://linked.open...i/riv/mistoVydani
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http://linked.open...i/riv/nazevZdroje
| - METAL 2010 19. ročník mezinárodní konference metalurgie a materiálů
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http://linked.open...in/vavai/riv/obor
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http://linked.open...ichTvurcuVysledku
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http://linked.open...cetTvurcuVysledku
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http://linked.open...vavai/riv/projekt
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http://linked.open...UplatneniVysledku
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http://linked.open...iv/tvurceVysledku
| - Hrbáček, Karel
- Dobrovská, J.
- Jonšta, Z.
- Jonšta, P.
- Mazancová, E.
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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http://linked.open...n/vavai/riv/zamer
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number of pages
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http://purl.org/ne...btex#hasPublisher
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https://schema.org/isbn
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