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Description
| - Production of new generation of aircraft gas turbine engines is based on designing new constructions and materials, which make it possible to operate under still more severe conditions. The key assembly of the engine is its turbine, whose materials and design determine the tolerable gas temperature. Increased inlet gas temperatures resulted in the shortening of the service life of the blades protected with diffusion coatings. New principles of coating deposition opened up new possibilities for purposive improvement of coating compositions and variation of their properties. Coatings protect the surface of turbine blades from damage caused by high-temperature corrosion and preserve the structural shape of blades and their mechanical properties for the required time [1, 2]. This paper deals with compare of microstructural features of two technological processes for deposition protective coatings for rotor turbine blades of aircraft DV2. The alternative deposition plasma spray was determined because of co
- Production of new generation of aircraft gas turbine engines is based on designing new constructions and materials, which make it possible to operate under still more severe conditions. The key assembly of the engine is its turbine, whose materials and design determine the tolerable gas temperature. Increased inlet gas temperatures resulted in the shortening of the service life of the blades protected with diffusion coatings. New principles of coating deposition opened up new possibilities for purposive improvement of coating compositions and variation of their properties. Coatings protect the surface of turbine blades from damage caused by high-temperature corrosion and preserve the structural shape of blades and their mechanical properties for the required time [1, 2]. This paper deals with compare of microstructural features of two technological processes for deposition protective coatings for rotor turbine blades of aircraft DV2. The alternative deposition plasma spray was determined because of co (en)
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Title
| - Study Of Protective Layers On Nickel-Base Superalloys
- Study Of Protective Layers On Nickel-Base Superalloys (en)
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skos:prefLabel
| - Study Of Protective Layers On Nickel-Base Superalloys
- Study Of Protective Layers On Nickel-Base Superalloys (en)
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skos:notation
| - RIV/00216305:26210/08:PU79830!RIV10-GA0-26210___
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
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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/00216305:26210/08:PU79830
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - Al-Si pack cementation process, plasma deposition, ZHS6K Al-Si pack cementation process, plasma deposition, ZHS6K (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
| - Trends in the Development of Machinery and Associated Technology
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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
| - Kianicová, Marta
- Podrábský, Tomáš
- Věchet, Stanislav
- Pospíšilová, Simona
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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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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http://localhost/t...ganizacniJednotka
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