000203240 001__ 203240
000203240 005__ 20230212173710.0
000203240 0247_ $$2CORDIS$$aG:(EU-Grant)754807$$d754807
000203240 0247_ $$2CORDIS$$aG:(EU-Call)H2020-CS2-CFP04-2016-02$$dH2020-CS2-CFP04-2016-02
000203240 0247_ $$2originalID$$acorda__h2020::754807
000203240 035__ $$aG:(EU-Grant)754807
000203240 150__ $$aSURFACE INTEGRITY CONSCIOUS HIGH-PERFORMANCE HYBRID MACHINING FOR SAFETY-CRITICAL SUPERALLOY AEROENGINE PARTS$$y2017-10-01 - 2021-09-30
000203240 371__ $$aFUNDACION TEKNIKER$$bTEKNIKER$$dSpain$$ehttp://www.tekniker.es$$vCORDIS
000203240 371__ $$aWATERJET AG$$bWATERJet$$dSwitzerland$$ehttp://www.waterjet.ch$$vCORDIS
000203240 371__ $$aSECO TOOLS AB$$dSweden$$ehttp://www.secotools.com$$vCORDIS
000203240 371__ $$aSYNOVA SA$$bSYNOVA$$dSwitzerland$$ehttp://www.synova.ch$$vCORDIS
000203240 371__ $$aNottingham Trent University$$bNTU$$dUnited Kingdom$$ehttp://www.ntu.ac.uk/$$vCORDIS
000203240 372__ $$aH2020-CS2-CFP04-2016-02$$s2017-10-01$$t2021-09-30
000203240 450__ $$aSTIMULANT$$wd$$y2017-10-01 - 2021-09-30
000203240 5101_ $$0I:(DE-588b)5098525-5$$2CORDIS$$aEuropean Union
000203240 680__ $$aSTIMULANT aims to develop and demonstrate “surface integrity conscious” hybridisation of machining processes for safety-critical aeroengine parts that is able to deliver a step-change in Material Removal Rates (MRR) and reduction in production costs. STIMULANT will take key knowledge at different levels of maturity that exists within Consortium, and progress it, via Standard Features (StdFs) methodology, to the demonstration on “engine-like” safety-critical parts. 
STIMULANT’s Objectives are scaled on 3 Phases:
Phase 1 – Standard features (StdF) identification 
- Decompose families of critical-safety aeroengine parts into classes of StdFs with technical, functional and economic characteristics to allow selection of single/multiple hybrid machining methods that minimise manufacturing costs. 

Phase 2 – Validation of individual hybrid machining processes  
- Develop and test a Spatially & Temporally Heat-Controlled Hybrid High Speed Machining for high MRR and cost efficiency and provide predictable properties of workpiece surface integrity and fatigue performance. 
- Develop and test a Dynamically Erosion-Controlled Hybrid Waterjet Machining for high productivity and geometrical accuracy of freeforms by controlled-depth, i.e. waterjet milling, and complex contours by waterjet through-cutting and demonstrate it as StdFs with high surface integrity and fatigue performance.
- Develop and test a Dynamically Material Removal Controlled Hybrid Laser Waterjet Guided for generating cost-efficient and high geometrical accuracy of complex geometry surfaces by controlled-depth milling and through-cutting and demonstrate it as StdFs with high surface integrity and fatigue performance. 

Phase 3 – Demonstration of hybridisation of machining processes and routes
- Demonstrate the hybrid machining methods validated on the Phase 2 on “engine-like” safety-critical parts and integrate them on hybridised processing routes for cost-effective machining of safety-critical aeroengine part.
000203240 909CO $$ooai:juser.fz-juelich.de:832017$$pauthority$$pauthority:GRANT
000203240 909CO $$ooai:juser.fz-juelich.de:832017
000203240 970__ $$aoai:dnet:corda__h2020::2ee0b23611e4af2e978d2291d7321c02
000203240 980__ $$aG
000203240 980__ $$aCORDIS
000203240 980__ $$aAUTHORITY