Innovating Works
LC-MG-1-5-2019
LC-MG-1-5-2019: Advancements in aerodynamics and innovative propulsion systems for quieter and greener aircrafts
Specific Challenge:Significant progress has been done recently in terms of environmental emission (including noise) by the development of Ultra High Pressure Ratio and Ultra High By-Pass Ratio engines. Technology assessments based on the turbofan engine configuration are indicating that there is still remarkable potential inherent in the turbofan engine configuration to be realised to further reduce gaseous and noise emissions. However, as far as noise is considered it is necessary to address the interaction between engines and aerodynamics surface and the engines interaction in aircraft architecture for a better assessment of the gain in term of noise reduction. This is necessary for the above mentioned advanced engines soon available but even more for future aircraft architecture displaying distributed propulsion or closer engine/wing integration.
Sólo fondo perdido 0 €
European
This call is closed This line is already closed so you can't apply. It closed last day 16-01-2019.
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Presentation: Consortium Consortium: Esta ayuda está diseñada para aplicar a ella en formato consorcio.
Minimum number of participants.
This aid finances Proyectos: project objective:

Specific Challenge:Significant progress has been done recently in terms of environmental emission (including noise) by the development of Ultra High Pressure Ratio and Ultra High By-Pass Ratio engines. Technology assessments based on the turbofan engine configuration are indicating that there is still remarkable potential inherent in the turbofan engine configuration to be realised to further reduce gaseous and noise emissions. However, as far as noise is considered it is necessary to address the interaction between engines and aerodynamics surface and the engines interaction in aircraft architecture for a better assessment of the gain in term of noise reduction. This is necessary for the above mentioned advanced engines soon available but even more for future aircraft architecture displaying distributed propulsion or closer engine/wing integration.


Scope:In order to substantially decrease the noise and environmental impact of aviation, in parallel to advances in propulsion technologies, the quest for a full understanding of the noise source mechanism (for example associated with the laminar-to-turbulent flow transition, fully turbulent flow regime, high lift de... see more

Specific Challenge:Significant progress has been done recently in terms of environmental emission (including noise) by the development of Ultra High Pressure Ratio and Ultra High By-Pass Ratio engines. Technology assessments based on the turbofan engine configuration are indicating that there is still remarkable potential inherent in the turbofan engine configuration to be realised to further reduce gaseous and noise emissions. However, as far as noise is considered it is necessary to address the interaction between engines and aerodynamics surface and the engines interaction in aircraft architecture for a better assessment of the gain in term of noise reduction. This is necessary for the above mentioned advanced engines soon available but even more for future aircraft architecture displaying distributed propulsion or closer engine/wing integration.


Scope:In order to substantially decrease the noise and environmental impact of aviation, in parallel to advances in propulsion technologies, the quest for a full understanding of the noise source mechanism (for example associated with the laminar-to-turbulent flow transition, fully turbulent flow regime, high lift devices, landing gears, etc) remains open especially for future aircraft configurations adopting breakthrough technologies. Hence, proposals should address at least two of the following areas:

Compatibility between thrust effectors (fan/propeller electrically or mechanically driven) and higher degree of integration into disruptive airframe configurations (e.g. Boundary Layer Ingestion, wing distributed propulsion). A better understanding of the noise source mechanisms for high bypass ratio turbofan engines for evolutionary and disruptive aircraft architectures such as distributed propulsion or closer engine/wing integration. A better understanding of the noise source mechanism associated with the laminar-to-turbulent flow transition and fully turbulent flow regime. A better understanding of the leading/trailing edge noise generated at landing by high-lift devices and undercarriage, including new acoustic treatments on nacelle and aircraft structures. Innovative propulsion technologies to address the critical topics related to the further increase of overall pressure ratio and gas temperatures needed to drive efficiency such as: reducing fuel consumption by improving thermal and propulsion efficiency, reducing Particle Number (PN), CO2 and NOx emissions by advanced combustion technologies, reducing engine weight and dimensions gaining substantial benefits on aircraft level. The proposals are expected also to develop multi-physics modelling, numerical simulation and optimisation exploiting High Performing Computing capabilities, innovative flow control technologies, and experimental methodologies.

Proposals should ideally address TRLs ranging from 1 to 4. The Commission considers that proposals requesting a contribution from the EU between EUR 3 and 5 million would allow this specific challenge to be addressed appropriately. Nonetheless, this does not preclude submission and selection of proposals requesting other amounts.


Expected Impact:Results will contribute to ultra-efficient, more silent, regional, short-haul or long-haul commercial, transport aircraft that could result in demonstration activities in 2025. According to the Flightpath 2050 goals pursued by the ACARE SRIA, CO2 emissions per passenger kilometre have to be reduced by 75%, NOx by 90% and perceived noise by 65% by 2050, all relative to the year 2000. Recent achievements assessed by the CSA FORUM-AE and extrapolated at TRL6 in 2020 result in the following figures: CO2 emissions per passenger kilometre about 38% (aircraft, + engine + ATM), NOx at engine level reduced by about 60% and perceived noise reduced by about 50%. The proposals must demonstrate that their targets are going beyond these last and are approaching the ACARE 2050 goals. Proposals must substantially explain how and why their anticipated targets are realistic.


Cross-cutting Priorities:Blue Growth


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Temáticas Obligatorias del proyecto: Temática principal: TPA Turbomachinery / Propulsion Aerodynamics ABP Air-breathing propulsion CAC Computational Acoustics Blue Growth Propulsion PRO ACT Acoustic Measurements and Test Technology ENP External Noise prediction

Consortium characteristics

Scope European : The aid is European, you can apply to this line any company that is part of the European Community.
Tipo y tamaño de organizaciones: The necessary consortium design for the processing of this aid needs:

characteristics of the Proyecto

Requisitos de diseño: Duración:
Requisitos técnicos: Specific Challenge:Significant progress has been done recently in terms of environmental emission (including noise) by the development of Ultra High Pressure Ratio and Ultra High By-Pass Ratio engines. Technology assessments based on the turbofan engine configuration are indicating that there is still remarkable potential inherent in the turbofan engine configuration to be realised to further reduce gaseous and noise emissions. However, as far as noise is considered it is necessary to address the interaction between engines and aerodynamics surface and the engines interaction in aircraft architecture for a better assessment of the gain in term of noise reduction. This is necessary for the above mentioned advanced engines soon available but even more for future aircraft architecture displaying distributed propulsion or closer engine/wing integration. Specific Challenge:Significant progress has been done recently in terms of environmental emission (including noise) by the development of Ultra High Pressure Ratio and Ultra High By-Pass Ratio engines. Technology assessments based on the turbofan engine configuration are indicating that there is still remarkable potential inherent in the turbofan engine configuration to be realised to further reduce gaseous and noise emissions. However, as far as noise is considered it is necessary to address the interaction between engines and aerodynamics surface and the engines interaction in aircraft architecture for a better assessment of the gain in term of noise reduction. This is necessary for the above mentioned advanced engines soon available but even more for future aircraft architecture displaying distributed propulsion or closer engine/wing integration.
Do you want examples? Puedes consultar aquí los últimos proyectos conocidos financiados por esta línea, sus tecnologías, sus presupuestos y sus compañías.
Financial Chapters: The chapters of financing expenses for this line are:
Personnel costs.
Los costes de personal subvencionables cubren las horas de trabajo efectivo de las personas directamente dedicadas a la ejecución de la acción. Los propietarios de pequeñas y medianas empresas que no perciban salario y otras personas físicas que no perciban salario podrán imputar los costes de personal sobre la base de una escala de costes unitarios
Purchase costs.
Los otros costes directos se dividen en los siguientes apartados: Viajes, amortizaciones, equipamiento y otros bienes y servicios. Se financia la amortización de equipos, permitiendo incluir la amortización de equipos adquiridos antes del proyecto si se registra durante su ejecución. En el apartado de otros bienes y servicios se incluyen los diferentes bienes y servicios comprados por los beneficiarios a proveedores externos para poder llevar a cabo sus tareas
Subcontracting costs.
La subcontratación en ayudas europeas no debe tratarse del core de actividades de I+D del proyecto. El contratista debe ser seleccionado por el beneficiario de acuerdo con el principio de mejor relación calidad-precio bajo las condiciones de transparencia e igualdad (en ningún caso consistirá en solicitar menos de 3 ofertas). En el caso de entidades públicas, para la subcontratación se deberán de seguir las leyes que rijan en el país al que pertenezca el contratante
Amortizaciones.
Activos.
Otros Gastos.
Madurez tecnológica: The processing of this aid requires a minimum technological level in the project of TRL 5:. Los elementos básicos de la innovación son integrados de manera que la configuración final es similar a su aplicación final, es decir que está listo para ser usado en la simulación de un entorno real. Se mejoran los modelos tanto técnicos como económicos del diseño inicial, se ha identificado adicionalmente aspectos de seguridad, limitaciones ambiéntales y/o regulatorios entre otros. + info.
TRL esperado:

Characteristics of financing

Intensidad de la ayuda: Sólo fondo perdido + info
Lost Fund:
0% 25% 50% 75% 100%
1. Eligible countries: described in Annex A of the Work Programme.
A number of non-EU/non-Associated Countries that are not automatically eligible for funding have made specific provisions for making funding available for their participants in Horizon 2020 projects. See the information in the Online Manual.
 
2. Eligibility and admissibility conditions: described in Annex B and Annex C of the Work Programme. 
 
Proposal page limits and layout: please refer to Part B of the proposal template in the submission system below.
 
3. Evaluation:
Evaluation criteria, scoring and thresholds are described in Annex H of the Work Programme.  
Submission and evaluation processes are described in the Online Manual.
4. Indicative time for evaluation and grant agreements:    
Information on the outcome of evaluation (two-stage call):
For stage 1: maximum 3 months from the deadline for submission.
For stage 2: maximum 5 months from the deadline for submission.
Signature of grant agreements: maximum 8 months from the deadline for submission.
 
5. Proposal templates, evaluation forms and model grant agreements (MGA):
Research and Innovation Action:
Specific provisions and funding rates
Standard proposal template
Standard evaluation form
General MGA - Multi-Beneficiary
Annotated Grant A...
1. Eligible countries: described in Annex A of the Work Programme.
A number of non-EU/non-Associated Countries that are not automatically eligible for funding have made specific provisions for making funding available for their participants in Horizon 2020 projects. See the information in the Online Manual.
 
2. Eligibility and admissibility conditions: described in Annex B and Annex C of the Work Programme. 
 
Proposal page limits and layout: please refer to Part B of the proposal template in the submission system below.
 
3. Evaluation:
Evaluation criteria, scoring and thresholds are described in Annex H of the Work Programme.  
Submission and evaluation processes are described in the Online Manual.
4. Indicative time for evaluation and grant agreements:    
Information on the outcome of evaluation (two-stage call):
For stage 1: maximum 3 months from the deadline for submission.
For stage 2: maximum 5 months from the deadline for submission.
Signature of grant agreements: maximum 8 months from the deadline for submission.
 
5. Proposal templates, evaluation forms and model grant agreements (MGA):
Research and Innovation Action:
Specific provisions and funding rates
Standard proposal template
Standard evaluation form
General MGA - Multi-Beneficiary
Annotated Grant Agreement
 
6. Additional provisions:
Horizon 2020 budget flexibility
Classified information
Technology readiness levels (TRL) – where a topic description refers to TRL, these definitions apply
Members of consortium are required to conclude a consortium agreement, in principle prior to the signature of the grant agreement.
8. Additional documents:
1. Introduction WP 2018-20       
11. Smart, green and integrated transport WP 2018-20      
18. Dissemination, Exploitation and Evaluation WP 2018-20
General annexes to the Work Programme 2018-2020
Legal basis: Horizon 2020 Regulation of Establishment
Legal basis: Horizon 2020 Rules for Participation
Legal basis: Horizon 2020 Specific Programme
 
7. Open access must be granted to all scientific publications resulting from Horizon 2020 actions.
Where relevant, proposals should also provide information on how the participants will manage the research data generated and/or collected during the project, such as details on what types of data the project will generate, whether and how this data will be exploited or made accessible for verification and re-use, and how it will be curated and preserved.
Open access to research data
The Open Research Data Pilot has been extended to cover all Horizon 2020 topics for which the submission is opened on 26 July 2016 or later. Projects funded under this topic will therefore by default provide open access to the research data they generate, except if they decide to opt-out under the conditions described in Annex L of the Work Programme. Projects can opt-out at any stage, that is both before and after the grant signature.
Note that the evaluation phase proposals will not be evaluated more favourably because they plan to open or share their data, and will not be penalised for opting out.
Open research data sharing applies to the data needed to validate the results presented in scientific publications. Additionally, projects can choose to make other data available open access and need to describe their approach in a Data Management Plan.
Projects need to create a Data Management Plan (DMP), except if they opt-out of making their research data open access. A first version of the DMP must be provided as an early deliverable within six months of the project and should be updated during the project as appropriate. The Commission already provides guidance documents, including a template for DMPs. See the Online Manual.
Eligibility of costs: costs related to data management and data sharing are eligible for reimbursement during the project duration.
The legal requirements for projects participating in this pilot are in the article 29.3 of the Model Grant Agreement.
 
Guarantees:
does not require guarantees
No existen condiciones financieras para el beneficiario.

Additional information about the call

incentive effect: Esta ayuda tiene efecto incentivador, por lo que el proyecto no puede haberse iniciado antes de la presentación de la solicitud de ayuda. + info.
Respuesta Organismo: Se calcula que aproximadamente, la respuesta del organismo una vez tramitada la ayuda es de:
Meses de respuesta:
Muy Competitiva:
non -competitive competitive Very competitive
We do not know the total budget of the line
minimis: Esta línea de financiación NO considera una “ayuda de minimis”. You can consult the regulations here.

other advantages

SME seal: Tramitar esta ayuda con éxito permite conseguir el sello de calidad de “sello pyme innovadora”. Que permite ciertas ventajas fiscales.
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