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Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission Effects

Riccius, Jörg and Zametaev, Evgeny and Gulczynski, Mateusz T. and Dos Santos Hahn, Robson Henrique (2022) Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission Effects. European Space Agency. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR), 19-23 June 2022, Heilbronn.

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Official URL: https://atpi.eventsair.com/far2022/

Abstract

The prediction of the fatigue life of a turbine blade requires preliminary fluid dynamics analyses (which are not shown in this manuscript), a structural analysis and finally a HCF analysis. For the structural analysis, two different methods are described in this manuscript: A 0d analysis based on beam theory and a structural 3d Finite Element (FE) analysis. The suggested post-processing HCF analysis method for the structural analyses takes into account both, the pre-stressing of the turbine blade due to centrifugal forces and the vibrational stress, caused by transitions between the admission and the non-admission sections of a partial admission turbine. Finally, all of the abovementioned numerical analysis methods are exemplarily applied to a single turbine blade of the Methane Turbo Pump (TP) of the Liquid Upper Stage Demonstrator Engine (LUMEN).

Item URL in elib:https://elib.dlr.de/189488/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission Effects
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Riccius, JörgUNSPECIFIEDhttps://orcid.org/0000-0002-5935-874XUNSPECIFIED
Zametaev, EvgenyUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Gulczynski, Mateusz T.UNSPECIFIEDhttps://orcid.org/0000-0001-5932-8981UNSPECIFIED
Dos Santos Hahn, Robson HenriqueUNSPECIFIEDhttps://orcid.org/0000-0002-2389-2043UNSPECIFIED
Date:2022
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:European Space Agency
Status:Published
Keywords:HCF, turbine blade, LRE, FE analysis, LUMEN, TP
Event Title:2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR)
Event Location:Heilbronn
Event Type:international Conference
Event Dates:19-23 June 2022
Organizer:ESA, DLR, NASA, JAXA, CNES, ASI, UKSA, INTA, NOSA, ROSA, HyFAR-ARA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project LUMEN (Liquid Upper Stage Demonstrator Engine)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Engine Systems
Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Gulczynski, Mateusz T.
Deposited On:02 Nov 2022 07:50
Last Modified:01 Feb 2023 08:08

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