Matches in SemOpenAlex for { <https://semopenalex.org/work/W2006992635> ?p ?o ?g. }
Showing items 1 to 68 of
68
with 100 items per page.
- W2006992635 endingPage "688" @default.
- W2006992635 startingPage "683" @default.
- W2006992635 abstract "Forging of high strength nickel base superalloys 720 and 718 for aircraft parts requires the usage of finite element simulations to ensure a proper thermo-mechanical treatment. Because of the strong mechanical requirements and narrow specifications of such parts not only a correct, defect free final geometry is necessary, but also a defined microstructure. The crucial point is therefore, to control all process parameters in a way to achieve the demanded properties. The typical forging processes like hydraulic, screw press and hammer forging imply a broad spectrum of strain rates. The influence of this different strain rates as well as forging temperature and strain on dynamic and post-dynamic recrystallization have been examined experimentally. Annealing tests at various temperatures and time periods have been performed, to investigate the grain growth behavior and dissolution processes in this before mentioned materials during heating periods. The obtained data was used to build phenomenological models, which were implemented into finite element code of a commercial special purpose finite element program. 2D and 3D Simulations of multiple step thermo-mechanical processes are compared with microstructure examinations of forged parts to show the usability and accuracy of such models as a tool to optimize complex forging processes of critical aircraft parts. In combination with systematic process data collection during production a stable processes and satisfactory mechanical product properties are guaranteed." @default.
- W2006992635 created "2016-06-24" @default.
- W2006992635 creator A5019008515 @default.
- W2006992635 creator A5091175238 @default.
- W2006992635 date "2004-10-01" @default.
- W2006992635 modified "2023-09-26" @default.
- W2006992635 title "Microstructure Modeling as a Tool to Optimize Forging of Critical Aircraft Parts" @default.
- W2006992635 cites W2005908092 @default.
- W2006992635 cites W2032233526 @default.
- W2006992635 cites W2039372184 @default.
- W2006992635 doi "https://doi.org/10.4028/www.scientific.net/msf.467-470.683" @default.
- W2006992635 hasPublicationYear "2004" @default.
- W2006992635 type Work @default.
- W2006992635 sameAs 2006992635 @default.
- W2006992635 citedByCount "4" @default.
- W2006992635 countsByYear W20069926352012 @default.
- W2006992635 countsByYear W20069926352023 @default.
- W2006992635 crossrefType "journal-article" @default.
- W2006992635 hasAuthorship W2006992635A5019008515 @default.
- W2006992635 hasAuthorship W2006992635A5091175238 @default.
- W2006992635 hasConcept C127413603 @default.
- W2006992635 hasConcept C135628077 @default.
- W2006992635 hasConcept C13655849 @default.
- W2006992635 hasConcept C139321929 @default.
- W2006992635 hasConcept C159985019 @default.
- W2006992635 hasConcept C169010117 @default.
- W2006992635 hasConcept C172658604 @default.
- W2006992635 hasConcept C191897082 @default.
- W2006992635 hasConcept C192562407 @default.
- W2006992635 hasConcept C207055975 @default.
- W2006992635 hasConcept C66938386 @default.
- W2006992635 hasConcept C78519656 @default.
- W2006992635 hasConcept C87976508 @default.
- W2006992635 hasConcept C96494537 @default.
- W2006992635 hasConceptScore W2006992635C127413603 @default.
- W2006992635 hasConceptScore W2006992635C135628077 @default.
- W2006992635 hasConceptScore W2006992635C13655849 @default.
- W2006992635 hasConceptScore W2006992635C139321929 @default.
- W2006992635 hasConceptScore W2006992635C159985019 @default.
- W2006992635 hasConceptScore W2006992635C169010117 @default.
- W2006992635 hasConceptScore W2006992635C172658604 @default.
- W2006992635 hasConceptScore W2006992635C191897082 @default.
- W2006992635 hasConceptScore W2006992635C192562407 @default.
- W2006992635 hasConceptScore W2006992635C207055975 @default.
- W2006992635 hasConceptScore W2006992635C66938386 @default.
- W2006992635 hasConceptScore W2006992635C78519656 @default.
- W2006992635 hasConceptScore W2006992635C87976508 @default.
- W2006992635 hasConceptScore W2006992635C96494537 @default.
- W2006992635 hasLocation W20069926351 @default.
- W2006992635 hasOpenAccess W2006992635 @default.
- W2006992635 hasPrimaryLocation W20069926351 @default.
- W2006992635 hasRelatedWork W2020660716 @default.
- W2006992635 hasRelatedWork W2067189140 @default.
- W2006992635 hasRelatedWork W2069451192 @default.
- W2006992635 hasRelatedWork W2078602358 @default.
- W2006992635 hasRelatedWork W2135357015 @default.
- W2006992635 hasRelatedWork W2160377190 @default.
- W2006992635 hasRelatedWork W2334042566 @default.
- W2006992635 hasRelatedWork W2776828477 @default.
- W2006992635 hasRelatedWork W2091096873 @default.
- W2006992635 hasRelatedWork W2594030139 @default.
- W2006992635 hasVolume "467-470" @default.
- W2006992635 isParatext "false" @default.
- W2006992635 isRetracted "false" @default.
- W2006992635 magId "2006992635" @default.
- W2006992635 workType "article" @default.