Pretražite po imenu i prezimenu autora, mentora, urednika, prevoditelja

Napredna pretraga

Pregled bibliografske jedinice broj: 1116264

Steady-State Creep of the Gas Turbine Disk - an Analytical Approach


Pustaić, Dragan
Steady-State Creep of the Gas Turbine Disk - an Analytical Approach // Proceedings of the 10th International Congress of Croatian Society of Mechanics (10th ICCSM 2022) / Skozrit, Ivica ; Sorić, Jurica ; Tonković, Zdenko (ur.).
Zagreb: Croatian Society of Mechanics (CSM), 2022. str. 223-224 (predavanje, međunarodna recenzija, kratko priopćenje, znanstveni)


CROSBI ID: 1116264 Za ispravke kontaktirajte CROSBI podršku putem web obrasca

Naslov
Steady-State Creep of the Gas Turbine Disk - an Analytical Approach

Autori
Pustaić, Dragan

Vrsta, podvrsta i kategorija rada
Sažeci sa skupova, kratko priopćenje, znanstveni

Izvornik
Proceedings of the 10th International Congress of Croatian Society of Mechanics (10th ICCSM 2022) / Skozrit, Ivica ; Sorić, Jurica ; Tonković, Zdenko - Zagreb : Croatian Society of Mechanics (CSM), 2022, 223-224

Skup
10th International Congress of Croatian Society of Mechanic (ICCSM 2022)

Mjesto i datum
Pula, Hrvatska, 28.09.2022. - 30.09.2022

Vrsta sudjelovanja
Predavanje

Vrsta recenzije
Međunarodna recenzija

Ključne riječi
Gas turbine disk ; stationary temperature field ; steady-state creep ; mechanical and thermal load of the disk ; stresses and the displacements in the disk in the steady-state creep conditions ; analytical methods.

Sažetak
The disk of the gas turbine rotor is usually performed as a disk of variable thickness. It is fixed by clamp connection on the turbine shaft or some other constructive solution is applied. At the stationary operation the disk is exposed to great mechanical and thermal loads. This primarily refers to the centrifugal forces of the disk´s own mass and the centrifugal forces of the blades, all at the speed of, for example, n = 7200 rpm. Regarding thermal loads, the disk is exposed to the stationary temperature field at the temperature of T = 600 0C. The creep of the disk will be especially expressed at so high temperatures and long duration of continuous operation. The creep of the disk will particularly influence disk´s displacements. In order to endure this high loads, the disk material has to be high strength alloyed steel as, for example, 45Cr14Ni14W2Mo, which in addition has a great elongation. The stresses and displacements at the stationary state which are the consequence of the creeping of a disk material are analyzed in this paper. The analysis was performed by analytical methods in the combination with contemporary mathematical tools. The software Wolfram Mathematica was used for the all numerical calculations.

Izvorni jezik
Engleski

Znanstvena područja
Brodogradnja, Strojarstvo, Zrakoplovstvo, raketna i svemirska tehnika

Napomena
Rad je izložen (PowerPoint Presentation) i
objavljen na 10th International Congress of
Croatian Society of Mechanics (10th ICCSM) koji je
održan u Puli, Hrvatska, od 28. do 30. rujna 2022.
godine.



POVEZANOST RADA


Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb

Profili:

Avatar Url Dragan Pustaić (autor)


Citiraj ovu publikaciju:

Pustaić, Dragan
Steady-State Creep of the Gas Turbine Disk - an Analytical Approach // Proceedings of the 10th International Congress of Croatian Society of Mechanics (10th ICCSM 2022) / Skozrit, Ivica ; Sorić, Jurica ; Tonković, Zdenko (ur.).
Zagreb: Croatian Society of Mechanics (CSM), 2022. str. 223-224 (predavanje, međunarodna recenzija, kratko priopćenje, znanstveni)
Pustaić, D. (2022) Steady-State Creep of the Gas Turbine Disk - an Analytical Approach. U: Skozrit, I., Sorić, J. & Tonković, Z. (ur.)Proceedings of the 10th International Congress of Croatian Society of Mechanics (10th ICCSM 2022).
@article{article, author = {Pustai\'{c}, Dragan}, year = {2022}, pages = {223-224}, keywords = {Gas turbine disk, stationary temperature field, steady-state creep, mechanical and thermal load of the disk, stresses and the displacements in the disk in the steady-state creep conditions, analytical methods.}, title = {Steady-State Creep of the Gas Turbine Disk - an Analytical Approach}, keyword = {Gas turbine disk, stationary temperature field, steady-state creep, mechanical and thermal load of the disk, stresses and the displacements in the disk in the steady-state creep conditions, analytical methods.}, publisher = {Croatian Society of Mechanics (CSM)}, publisherplace = {Pula, Hrvatska} }
@article{article, author = {Pustai\'{c}, Dragan}, year = {2022}, pages = {223-224}, keywords = {Gas turbine disk, stationary temperature field, steady-state creep, mechanical and thermal load of the disk, stresses and the displacements in the disk in the steady-state creep conditions, analytical methods.}, title = {Steady-State Creep of the Gas Turbine Disk - an Analytical Approach}, keyword = {Gas turbine disk, stationary temperature field, steady-state creep, mechanical and thermal load of the disk, stresses and the displacements in the disk in the steady-state creep conditions, analytical methods.}, publisher = {Croatian Society of Mechanics (CSM)}, publisherplace = {Pula, Hrvatska} }




Contrast
Increase Font
Decrease Font
Dyslexic Font