SAFRAN HELICOPTER ENGINES
- Country
- France
- Type
- Beneficiary
- Website
- www.turbomeca.com
- Grants received
- 32
Funding record
- 32 grants on record
- €49,399,308.08 awarded in total
- 2008–2023 span of the record
Grants recorded here are the ones our sources publish, and the total is the sum of those. It is not a statement of this organisation's total funding.
Programmes
- Seventh Framework Programme
- JTI
- Horizon 2020 Framework Programme
- Horizon Europe Framework Programme
- ARTEMIS
7 further grants are on record without a programme named by the source, or under a programme outside the largest shown here.
Frequent partners
Organisations this one has been funded alongside on two or more projects. A single shared consortium is not counted: the largest here has 195 members, and being on one list together is not a collaboration.
- SAFRAN AIRCRAFT ENGINES
- DEUTSCHES ZENTRUM FUR LUFT - UND RAUMFAHRT EV
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- CENTRE EUROPEEN DE RECHERCHE ET DEFORMATION AVANCEE EN CALCUL SCIENTIFIQUE
- GKN AEROSPACE SWEDEN AB
- INDUSTRIA DE TURBO PROPULSORES SA,SOCIEDAD UNIPERSONAL
- MTU AERO ENGINES AG
- GE AVIO SRL
Calls from this organisation
No published calls from this organisation.
Grants received
- Hybrid Electric propulsion system for regional AiRcrafT
- Research on AI- and Simulation-Based Engineering at Exascale
- H2020-IBA-CS2-GAMS-2020-2021
- Advanced Research Into Aeromechanical Solutions
- Annular Instabilities and Transient Phenomena in Gas Turbine Combustors
- Machine learning for Advanced Gas turbine Injection SysTems to Enhance combustoR performance.
- Validation of improved turbomachinery noise prediction models and development of novel design methods for fan stages with reduced broadband noise
- Soot Processes and Radiation in Aeronautical inNOvative combustors
- Engine ITD - GAM 2018
- Engine Module Validators
- Uncertainty Management for Robust Industrial Design in Aeronautics
- Research on Core Noise Reduction
- Engine Breakthrough Components and Subsystems
- Coupled Parallel Simulation of Gas Turbines
- Intelligent Design Methodologies for Low Pollutant Combustors for Aero-Engines
Data source
© European Union, 2026. Source: CORDIS. Reused under Commission Decision 2011/833/EU — CC BY 4.0.
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