People | Locations | Statistics |
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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Langkamp, Albert
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (42/42 displayed)
- 2025Hydrogen storage in a commuter aircraft: Combining classical engineering design process with model-based system engineering for CFRP pressure vessel integration
- 2024Modelling residual stresses and voids arising during resin polymerisation in fibre composites
- 2024Influence of toughness modification of high temperature thermosetting resins on fiber-reinforced composites strengths
- 2024Charakterisierung der Vernetzungsreaktion UV-härtender Endlosfaser-Kunststoff-Verbunde
- 2023Experimental analysis of the influence of thermoplastic veils doped with nanofillers on the thermal properties of fibre-reinforced composites
- 2023Interactive and model based development at the example of a structural and aerodynamic composite vane for a jet engine
- 2022Endless fibre-reinforced composite-metal impeller
- 2021Contribution to Digital Linked Development, Manufacturing and Quality Assurance Processes for Metal-Composite Lightweight Structurescitations
- 2021Experimental-numerical validation of the curing reaction of snap-cure polymer systems for component families of small batch sizes and high diversity
- 2021Effiziente und Robuste Entwicklung komplexer Faserverbund-Triebwerkstrukturen
- 2019Regionales Innovationskonzept "WIR!-DigiT" - Zentrum für vernetzte digitale Produktoptimierung durch Lebensphasen-übergreifende virtuelle Zwillinge
- 2018Experimental investigation of the curing behaviour of fibre composite structures with snap-cure polymer systemscitations
- 2018Endless fibre-reinforced composite-metal-impeller: material related design and dimensioning process for hybrid radial-fans
- 2018Elementary specific modelling of composite rotors with consideration of sequential damage processes
- 2017Novel engine-like test methods for the development of ultra-high ratio compressor components
- 2017Entwicklung faserverbundkeramischer Lüfterräder für effizientere Thermoprozesse
- 2017Influence of heat pretreatment on cross-linking behavior and thermal properties of thermoset semi-finished products with powder resin systems
- 2016Hybrid-Fügetechnologien für Leichtbauweisen bei Transportanwendungen (TransHybrid)
- 2016The networked car body – Function-integrated lightweight construction with hybrid yarn textile thermoplastic composites
- 2016Die vernetzte Karosserie – Funktionsintegrativer Leichtbau mit Hybridgarn-Textil-Thermoplast-Verbunden
- 2016Turbinenschaufel mit Beschichtung
- 2016Komplexe Leichtbau-Zwischengehäuse in Faserverbundbauweise für Turbo-Fantriebwerke neuer Generation
- 2015Development of active composite aerofoil for assessment of novel flow control concepts
- 2015Design of composite compressor blades with focus on the vibration behaviour
- 2014Gestaltung und Dimensionierung von Faserverbund-Antriebswellen in ultraleichter Mischbauweise
- 2014Zur Gestaltung und Dimensionierung von Pinverbindungen als Lasteinleitungssystem für Faserverbund-Antriebswellen
- 2011Thermoplastic last-stage blade
- 2011Turbine blade, especially rotor blade for a steam engine, and corresponding method of manufacture
- 2011Turbinenschaufel, Turbinenwelle, Turbinenanlage und Verfahren zur Montage der Turbinenschaufel
- 2010Turbinenschaufel, insbesondere Laufschaufel für eine Dampfturbine, sowie Herstellungsverfahren hierfür
- 2010Multifunktionale Mehrkomponentenwerkstoffe als Schlüssel zu Material- und Energieeffizienz - das Spitzentechnologiecluster ECEMP
- 2010Neuartige Ansätze für selbstdiagnostizierende und selbstregulierende Mehrkomponentenwerkstoffe in Leichtbauanwendungen
- 2010Turbinenschaufel mit Beschichtung
- 2010Verfahren zum Anbringen bzw. Herstellen eines geschlossenen Deckbandes für eine Laufbeschaufelung einer Turbinenstufe sowie Laufbeschaufelung einer Turbinenstufe für eine Turbine
- 2010Verfahren zum Anbringen bzw. Herstellen eines geschlossenen Deckbandes für eine Laufbeschaufelung einer Turbinenstufe sowie Laufbeschaufelung einer Turbinenstufe für eine Turbine
- 2007Advanced calculation methods for notched hybrid composites with textile-reinforced polymers
- 2007Erprobung des Werkstoffpotenzials von Faserkeramiken für hochdynamische, tribologisch belastete Fahrwerkskomponenten (KEFA)
- 2006Experimentelle Versagensanalyse von textilverstärkten Verbundwerkstoffen bei hochdynamischer Belastungcitations
- 2006Bruchmodebezogene Versagensmodelle für gewebeverstärkte Verbundwerkstoffe
- 2006Physically Based Failure Criteria for Long-Fibre Reinforced Ceramicscitations
- 20053D Textile Reinforcements for High-Performance Rotors
- 2004Contribution to the simulation of textile reinforced plastics under crash and impact loads
Places of action
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patent
Turbinenschaufel, Turbinenwelle, Turbinenanlage und Verfahren zur Montage der Turbinenschaufel
Abstract
The invention relates to a turbine blade (1), a turbine shaft (2) having such a turbine blade (1), a turbine system comprising a turbine shaft (2) having such a turbine blade (1), and a method for installing the turbine blade (1), resulting in that the turbine blade (1) is made of a fiber composite material and, at the same time, the bearing strength of the turbine blade (1) or the blade root (3) of the turbine blade (1) is increased relative to metal turbine blades by reducing stress concentrations at locations of the blade root (3) at which the blade root (3) is supported by corresponding wall segments (6) of a groove (4) of the turbine shaft (2), thus extending the service life of the turbine blade (1) and thus the turbine shaft (2) and the turbine system having such turbine blades (1). The aim is achieved by a particularly fine fit of the blade root (3) of the turbine blade (1) in the shape of the groove (4) of the turbine shaft (2), due to the effect of heating on the blade root (3) brought about by precautionary heating (8) during assembly to the turbine shaft (2), and consequently of auto-adaptation of the shape to the shape of the groove (4) of the turbine shaft (2).