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

HCF analysis of a prospective 3d-printed LRE turbine blade

Riccius, Jörg R. and Zametaev, Evgeny B. (2023) HCF analysis of a prospective 3d-printed LRE turbine blade. AIAA SciTech 2023 Forum, 23.-27. Jan. 2023, National Harbor, MD, USA & Online. doi: 10.2514/6.2023-1086.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/10.2514/6.2023-1086

Abstract

A HCF life analysis method for 3d printed turbine blades is suggested. This method comprises a stationary thermal 3d Finite Element analysis, a follow-on (one-way coupled) quasi stationary structural 3d Finite Element analysis (including four load steps) of a single and two half turbine blades and the related disk and rotor section and a (modified Goodman equation based) post-processing fatigue life analysis for the highest HCF-loaded point of the 3d printed turbine blade with as-built to machined surface HCF life correction. Finally, this approach is demonstrated by the numerical HCF analysis of a generic Hydrogen turbo pump (1st rotor row) turbine blade of a 1 MN thrust class gas generator LOX-LH2 Liquid Rocket Engine (LRE).

Item URL in elib:https://elib.dlr.de/59149/
Document Type:Conference or Workshop Item (Speech)
Title:HCF analysis of a prospective 3d-printed LRE turbine blade
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Riccius, Jörg R.UNSPECIFIEDhttps://orcid.org/0000-0002-5935-874XUNSPECIFIED
Zametaev, Evgeny B.UNSPECIFIEDhttps://orcid.org/0000-0003-0064-1396UNSPECIFIED
Date:19 January 2023
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.2514/6.2023-1086
Page Range:pp. 1-9
Status:Published
Keywords:LRE; HCF; FE; thermal analysis; structural analysis; mean stress; stress amplitude; creep; full admission; turbine blade; post-processing; Goodman; Inconel 718; 3d printing
Event Title:AIAA SciTech 2023 Forum
Event Location:National Harbor, MD, USA & Online
Event Type:international Conference
Event Dates:23.-27. Jan. 2023
Organizer:AIAA
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 TRANSIENT
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Riccius, Dr. Jörg
Deposited On:09 Feb 2023 15:24
Last Modified:09 Feb 2023 15:24

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.