elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

A small-scale creep test for calibrating an efficient lifetime model for high pressure turbine blades

Dresbach, Christian and Wischek, Janine and Bartsch, Marion and Kuntzagk, Stefan (2021) A small-scale creep test for calibrating an efficient lifetime model for high pressure turbine blades. ACEX2021 - 14th International Conference on Advanced Computational Engineering and Experimenting, 04-08.07.2021, hybrid, online und Intercontinental Malta, Malta.

Full text not available from this repository.

Abstract

Jet engines of airplanes are designed such that in some components damage occurs and grows in service without being critical up to a certain level of damage. Since maintenance, repair and component exchange are very cost-intensive, it is necessary to predict the component lifetime very well in an acceptable amount of time. To efficiently calculate the lifetime consumption with sufficient accuracy under operational conditions, we developed in a former investigation a hybrid approach where the lifetime consumption is calculated from interpolated stress and temperature distributions based on a DoE study with precise aerodynamic and structural mechanics simulations. Since the parameters of the former implemented lifetime models were only estimated from literature values of macroscopic medium- and long-time experiments, it was necessary to develop a special test setup, which allows the determination of the short time creep behavior, which is more relevant for the actual loading situation of real turbine blades. To consider also microstructural influences resulting from the manufacturing of thin-walled single crystal turbine blades, we developed a procedure to prepare small scale creep test samples out of real turbine blades and test them in short- and medium-time creep experiments. Based on the experimental results and the former used literature values, we were able to calibrate a modified creep model which describes the creep fracture behavior from short to long time loading and can now be used for the efficient prediction of the lifetime consumption of turbine blades under real loading conditions.

Item URL in elib:https://elib.dlr.de/148448/
Document Type:Conference or Workshop Item (Speech)
Title:A small-scale creep test for calibrating an efficient lifetime model for high pressure turbine blades
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Dresbach, ChristianHochschule Bonn-Rhein-Sieg (H-BRS)UNSPECIFIED
Wischek, Janinejanine.wischek (at) dlr.deUNSPECIFIED
Bartsch, Marionmarion.bartsch (at) dlr.dehttps://orcid.org/0000-0002-3952-2928
Kuntzagk, StefanLufthansa Technik AGUNSPECIFIED
Date:July 2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Creep test, superalloy, small scale test, lifetime modell, high pressure turbine blade, aero engine
Event Title:ACEX2021 - 14th International Conference on Advanced Computational Engineering and Experimenting
Event Location:hybrid, online und Intercontinental Malta, Malta
Event Type:international Conference
Event Dates:04-08.07.2021
Organizer:ICC – INTERNATIONAL CONFERENCES AND COURSES LIMITED
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Advanced Materials and New Manufacturing Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Materials Research > Experimental and Numerical Methods
Institute of Materials Research > Mechanical Testing of Materials
Deposited By: Bartsch, Dr.-Ing. Marion
Deposited On:24 Jan 2022 08:53
Last Modified:24 Jan 2022 08:53

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.