Revision history of "Nanostructural Coatings of Heat Barriers for Driving and Fixed Gas Turbines" (Q78465)

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18 October 2022

13 August 2022

  • curprev 16:2316:23, 13 August 2022DG Regio talk contribs 77,241 bytes +48,846 Changed label, description and/or aliases in et, lt, hr, el, sk, fi, hu, cs, lv, ga, sl, bg, mt, pt, da, ro, sv, nl, fr, de, it, es, and other parts: Adding translations: et, lt, hr, el, sk, fi, hu, cs, lv, ga, sl, bg, mt, pt, da, ro, sv,

19 January 2022

15 January 2022

16 December 2021

7 December 2021

30 November 2021

  • curprev 15:2315:23, 30 November 2021DG Regio talk contribs 17,225 bytes +2,762 Created claim: summary (P836): Couverture de barrière thermique („ revêtement de barrière thermique ” – À confirmer) en céramique à faible conductivité thermique sont actuellement utilisés pour assurer l’isolation thermique des composants métalliques provenant du flux de gaz chaud dans les moteurs à turbine à gaz utilisés pour la propulsion des aéronefs, la production d’énergie et la propulsion des navires. L’utilisation de TBC (épaisseur de 100 à 500 &m), a...
  • curprev 15:2315:23, 30 November 2021DG Regio talk contribs 14,463 bytes +168 Changed label, description and/or aliases in fr: translated_label

29 October 2020

14 October 2020

  • curprev 12:5012:50, 14 October 2020DG Regio talk contribs 14,735 bytes +134 Changed label, description and/or aliases in 1 language: translated_label
  • curprev 12:5012:50, 14 October 2020DG Regio talk contribs 14,601 bytes −124 Changed label, description and/or aliases in 1 language: remove_english_label
  • curprev 12:5012:50, 14 October 2020DG Regio talk contribs 14,725 bytes +2,328 Created claim: summary (P836): Thermal barrier coverage (thermal Barrier Coatingamp;bdquo; – TBC) made of low thermal conductivity ceramics are currently used to provide heat insulation of metal components from hot gas streams in turbo gas engines used for aircraft propulsion, electricity generation and marine propulsion. The use of TBC (thickness of 100 to 500 &m;m), together with the internal cooling of the base component produced from the superalloy, provides a signi...
  • curprev 12:5012:50, 14 October 2020DG Regio talk contribs 12,397 bytes −1,941 Removed claim: summary (P836): Treatment of thermal barriers (& bdnquo; thermal Barrier Coating & core;& ll;The tbc made of a low-conductivity ceramic is currently used to ensure the heat insulation of the metal components from the hot gas flow in gas turbine engines used for the propulsion of the aeroplane, for the generation of electrical energy and for the propulsion of vessels.The use of the TBC cover (with a thickness of 100 to 500 & m; m), together with the cooling of...

25 September 2020

23 September 2020

15 July 2020

9 June 2020

6 June 2020

26 March 2020

4 March 2020

  • curprev 09:1109:11, 4 March 2020DG Regio talk contribs 12,619 bytes +1,941 Created claim: summary (P836): Treatment of thermal barriers (& bdnquo; thermal Barrier Coating & core;& ll;The tbc made of a low-conductivity ceramic is currently used to ensure the heat insulation of the metal components from the hot gas flow in gas turbine engines used for the propulsion of the aeroplane, for the generation of electrical energy and for the propulsion of vessels.The use of the TBC cover (with a thickness of 100 to 500 & m; m), together with the cooling of t...

18 February 2020

8 February 2020

31 January 2020

13 January 2020