National Repository of Grey Literature 16 records found  1 - 10next  jump to record: Search took 0.00 seconds. 
Machining of Ni80TiAl alloy detail
Kudrna, Miloš ; Novák, Zdeněk (referee) ; Humár, Anton (advisor)
The master`s thesis deal with analysis of machining technology of the bolt from the superalloy Ni80TiAl for the company Sanborn a.s. The aim of the thesis is the project of new technology by usage of new tool, indexable inserts and cutting conditions. The results are speedup of the roughing operation, reduction of the manufacturing cost and the product price.
Racionalization of production of components from nickel alloy
Bula, Tomáš ; Sedlák, Josef (referee) ; Zemčík, Oskar (advisor)
The Bachelor thesis deals with the racionalization of manufacturing Housing diffuser from Ni-base superalloy. The main emphasis is put on shortening production times of CNC turning, selecting appropriate tools and the development of the framework process and economic evaluation.
Manufacture and properties of heat resistant alloys
Majchrák, Aleš ; Myška, Martin (referee) ; Záděra, Antonín (advisor)
This bachelor thesis deals with heat resistant alloys, specifically with superalloys and high entropy alloys. The theoretical part includes distribution of those alloys by their chemical composition, description of their properties, microstructure and applications. Experimental part is devoted to cobalt alloy UmCo50. Aims of this part include metallurgy process description of this alloy, verification of vacuuming time influence on decarburization, microstructure observation and its conclusion.
Damage mechanisms in nickel-based superalloy René 41 subjected to fatigue
Babinský, Tomáš ; Pippan, Reinhard (referee) ; Růžička,, Milan (referee) ; Polák, Jaroslav (advisor)
Předkládaná práce se zabývá vznikem poškození ve tvářené niklové superslitině René 41, která je podrobena únavovému zatěžování za pokojové a zvýšené (800 °C) teploty. Slitina byla zkoumána ve dvou termodynamických stavech: po rozpouštěcím žíhání a po stárnutí. Jednoosé zkoušky nízkocyklové únavy byly prováděny symetricky vzhledem k řízené veličině, kterou byla celková podélná deformace. Za účelem studia mechanismů poškození a jejich souvislosti s plastickou deformací byly aplikovány techniky elektronové mikroskopie doplněné o analýzu cyklické odezvy ve formě hysterezních smyček statistickým přístupem. Navíc byly provedeny přerušované únavové zkoušky za účelem studia vývoje povrchového reliéfu ve vztahu k dislokační substruktuře, k čemuž bylo opět využito elektronové mikroskopie. Porušení za pokojové teploty bylo povětšinou transkrystalické, únavové trhliny iniciovaly především uvnitř zrn z povrchového reliéfu. Srovnáme-li dva zkoušené stavy, stárnutý materiál vykazoval vyšší hodnoty cyklického napětí a při srovnatelném napětí dosahoval vyšších životností. Cyklická deformace byla od prvního cyklu lokalizována do persistentních skluzových pásů. Bylo zjištěno, že většina skluzových pásů vzniká na začátku únavového života, kvůli čemuž jsou koherentní precipitáty ‘ významně deformovány pouze na začátku únavového života. Skluz v persistentních skluzových pásech vedl k vytvoření povrchového reliéfu ve formě skluzových schodů, extruzí a intruzí. Vznik povrchového reliéfu byl podrobně diskutován s existujícími modely. Vysokoteplotní expozice měla za následek oxidaci povrchu, zejména na oslabených hranicích zrn, kde iniciovaly a následně se šířily únavové trhliny. Výsledné poškození bylo tudíž interkrystalické.
Manufacture and properties of heat resistant alloys
Majchrák, Aleš ; Myška, Martin (referee) ; Záděra, Antonín (advisor)
This bachelor thesis deals with heat resistant alloys, specifically with superalloys and high entropy alloys. The theoretical part includes distribution of those alloys by their chemical composition, description of their properties, microstructure and applications. Experimental part is devoted to cobalt alloy UmCo50. Aims of this part include metallurgy process description of this alloy, verification of vacuuming time influence on decarburization, microstructure observation and its conclusion.
Interaction of Creep and High Cycle Fatigue of IN 713LC Superalloy
Horník, V. ; Šmíd, Miroslav ; Hutař, Pavel ; Kunz, Ludvík ; Hrbáček, K.
The study deals with the interaction of creep and high cycle fatigue of cast polycrystalline nickel-based superalloy IN 713LC at high temperatures. Previous works indicated that creep lifetime of superalloy structures was un-affected or even slightly increased in the cases with superimposed vibrations. The reason for this behaviour was not well described up to now. Therefore, set of fatigue tests was conducted at high mean stresses level to observe this phenomenon. The mean stress was kept constant while the stress amplitudes were selected in order to measure wide range of conditions from pure creep to pure fatigue. Fractographic analysis by scanning electron microscopy (SEM) was done with the aim to identify governing damage mechanisms for particular test conditions as a preliminary evaluation of conducted tests.
IN-SITU HIGH TEMPERATURE LOW CYCLE FATIGUE STUDY OF SURFACE TOPOGRAPHY EVOLUTION IN NICKEL SUPERALLOY
Petrenec, M. ; Polák, Jaroslav ; Šamořil, T. ; Dluhoš, J. ; Obrtlík, Karel
In-situ Low Cycle Fatigue test (LCF) at temperature 635 degrees C have been performed in Scanning Electron Microscope (SEM) equipped with Electron Backscatter Diffraction analysis (EBSD) on a small dog-bone-shaped specimen of cast Inconel 713LC superalloy. The aim of the work was to study early stage fatigue damage at high temperature by the observations of the characteristic surface relief evolution and crystallographic characterization changes by EBSD. The detail of slip bands shape was checked by FIB and AFM microscopes. The LCF test was conducted on GATAN stage with pre tilted position and constant stress amplitude of total cycle number of 20. The relief produced in the first cycle determines the other locations of the localized cyclic slip to the primary slip planes (111). The relief was modified in the next cycles but without forming additionally new slip traces in the primary system. Based on EBSD analysis before and after LCF, the orientation of two grains was changed which caused activation of second slip system. The damage mechanism evolution is closely connected with the cyclic strain localization to the persistent slip bands where the fatigue cracks were initiated.
Machining of Ni80TiAl alloy detail
Kudrna, Miloš ; Novák, Zdeněk (referee) ; Humár, Anton (advisor)
The master`s thesis deal with analysis of machining technology of the bolt from the superalloy Ni80TiAl for the company Sanborn a.s. The aim of the thesis is the project of new technology by usage of new tool, indexable inserts and cutting conditions. The results are speedup of the roughing operation, reduction of the manufacturing cost and the product price.
Racionalization of production of components from nickel alloy
Bula, Tomáš ; Sedlák, Josef (referee) ; Zemčík, Oskar (advisor)
The Bachelor thesis deals with the racionalization of manufacturing Housing diffuser from Ni-base superalloy. The main emphasis is put on shortening production times of CNC turning, selecting appropriate tools and the development of the framework process and economic evaluation.
IN-SITU HIGH TEMPERATURE LOW CYCLE FATIGUE STUDY
Petrenec, M. ; Polák, Jaroslav ; Šamořil, T. ; Dluhoš, J. ; Obrtlík, Karel
In-situ Low Cycle Fatigue test (LCF) at temperature 635 °C have been performed in Scanning Electron Microscope (SEM) equipped with Electron Backscatter Diffraction analysis (EBSD) on a small dog-bone-shaped specimen of cast Inconel 713LC superalloy. The aim of the work was to study early stage fatigue damage at high temperature by the observations of the characteristic surface relief evolution and crystallographic characterization changes by EBSD. The detail of slip bands shape was checked by FIB and AFM microscopes. The LCF test was conducted on GATAN stage with pre tilted position and constant stress amplitude of total cycle number of 20. The relief produced in the first cycle determines the other locations of the localized cyclic slip to the primary slip planes (111). The relief was modified in the next cycles but without forming additionally new slip traces in the primary system. Based on EBSD analysis before and after LCF, the orientation of two grains was changed which caused activation of second slip system. The damage mechanism evolution is closely connected with the cyclic strain localization to the persistent slip bands where the fatigue cracks were initiated.

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