HORIZON EUROPE
Cerrada
JTI-CS2-2019-CFP10-THT-07
JTI-CS2-2019-CFP10-THT-07:
Ultra-High Aspect ratio wings
Europeo
Specific Challenge:The most “easy” way to improve the aerodynamic efficiency and performance of an aircraft is to increase its aspect ratio of its wings. Increasing the aspect ratio has a direct effect on the induced drag. Increasing the aspect ratio while satisfying the design constraints that have to date limited aspect ratios of modern transport aircraft wings, such as aero-elasticity and buffeting; structural design and weight limitations; fuel capacity; and practical issues such as airport runway/taxiway and gate dimensions may yield a sizeable potential benefit in fuel burn and emissions. Long, slender wings may necessitate radically different structural and manufacturing concepts. Load control systems may prove essential to the feasibility of very high aspect ratio designs. Optimal wing span may lead to the need for folding outer wing sections. This topic aims to provide a preliminary design study involving the capture of the current state of the art, an analysis of potential gains through the use of very high aspect ratio wings in the various transport aircraft market segments [regional, short-medium and long range]. Different design concepts should be analysed, paying particular attention to design constraints such as those mentioned above. A proposed ‘best in class’ conceptual/preliminary design should be completed, starting from a selected reference aircraft for comparison in terms of performance. The estimated gains should be validated experimentally by scaled model wind tunnel tests, at least in terms of aerodynamic performance, possibly in terms of noise performance as well. Please refer to the full topic descriptions document published in this call.
Sólo fondo perdido
0 €
Europeo
Esta convocatoria está cerrada
Esta línea ya está cerrada por lo que no puedes aplicar. Cerró el pasado día 03-09-2019.
Se espera una próxima convocatoria para esta ayuda, aún no está clara la fecha exacta de inicio de convocatoria.
Por suerte, hemos conseguido la lista de proyectos financiados!
Presentación:
Consorcio
Consorcio:
Esta ayuda está diseñada para aplicar a ella en formato consorcio.
Número mínimo de participantes.
Esta ayuda financia
Proyectos:
Objetivo del proyecto:
Specific Challenge:The most “easy” way to improve the aerodynamic efficiency and performance of an aircraft is to increase its aspect ratio of its wings. Increasing the aspect ratio has a direct effect on the induced drag. Increasing the aspect ratio while satisfying the design constraints that have to date limited aspect ratios of modern transport aircraft wings, such as aero-elasticity and buffeting; structural design and weight limitations; fuel capacity; and practical issues such as airport runway/taxiway and gate dimensions may yield a sizeable potential benefit in fuel burn and emissions. Long, slender wings may necessitate radically different structural and manufacturing concepts. Load control systems may prove essential to the feasibility of very high aspect ratio designs. Optimal wing span may lead to the need for folding outer wing sections. This topic aims to provide a preliminary design study involving the capture of the current state of the art, an analysis of potential gains through the use of very high aspect ratio wings in the various transport aircraft market segments [regional, short-medium and long range]. Different design concepts should be analysed, paying part... ver más
Specific Challenge:The most “easy” way to improve the aerodynamic efficiency and performance of an aircraft is to increase its aspect ratio of its wings. Increasing the aspect ratio has a direct effect on the induced drag. Increasing the aspect ratio while satisfying the design constraints that have to date limited aspect ratios of modern transport aircraft wings, such as aero-elasticity and buffeting; structural design and weight limitations; fuel capacity; and practical issues such as airport runway/taxiway and gate dimensions may yield a sizeable potential benefit in fuel burn and emissions. Long, slender wings may necessitate radically different structural and manufacturing concepts. Load control systems may prove essential to the feasibility of very high aspect ratio designs. Optimal wing span may lead to the need for folding outer wing sections. This topic aims to provide a preliminary design study involving the capture of the current state of the art, an analysis of potential gains through the use of very high aspect ratio wings in the various transport aircraft market segments [regional, short-medium and long range]. Different design concepts should be analysed, paying particular attention to design constraints such as those mentioned above. A proposed ‘best in class’ conceptual/preliminary design should be completed, starting from a selected reference aircraft for comparison in terms of performance. The estimated gains should be validated experimentally by scaled model wind tunnel tests, at least in terms of aerodynamic performance, possibly in terms of noise performance as well. Please refer to the full topic descriptions document published in this call.
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Características del consorcio
Ámbito Europeo :
La ayuda es de ámbito europeo, puede aplicar a esta linea cualquier empresa que forme parte de la Comunidad Europea.
:
La ayuda es de ámbito europeo, puede aplicar a esta linea cualquier empresa que forme parte de la Comunidad Europea.
Tipo y tamaño de organizaciones:
El diseño de consorcio necesario para la tramitación de esta ayuda necesita de:
Características del Proyecto
Requisitos de diseño:
Duración:
Requisitos técnicos: Specific Challenge:The most “easy” way to improve the aerodynamic efficiency and performance of an aircraft is to increase its aspect ratio of its wings. Increasing the aspect ratio has a direct effect on the induced drag. Increasing the aspect ratio while satisfying the design constraints that have to date limited aspect ratios of modern transport aircraft wings, such as aero-elasticity and buffeting; structural design and weight limitations; fuel capacity; and practical issues such as airport runway/taxiway and gate dimensions may yield a sizeable potential benefit in fuel burn and emissions. Long, slender wings may necessitate radically different structural and manufacturing concepts. Load control systems may prove essential to the feasibility of very high aspect ratio designs. Optimal wing span may lead to the need for folding outer wing sections. This topic aims to provide a preliminary design study involving the capture of the current state of the art, an analysis of potential gains through the use of very high aspect ratio wings in the various transport aircraft market segments [regional, short-medium and long range]. Different design concepts should be analysed, paying particular attention to design constraints such as those mentioned above. A proposed ‘best in class’ conceptual/preliminary design should be completed, starting from a selected reference aircraft for comparison in terms of performance. The estimated gains should be validated experimentally by scaled mod...
Specific Challenge:The most “easy” way to improve the aerodynamic efficiency and performance of an aircraft is to increase its aspect ratio of its wings. Increasing the aspect ratio has a direct effect on the induced drag. Increasing the aspect ratio while satisfying the design constraints that have to date limited aspect ratios of modern transport aircraft wings, such as aero-elasticity and buffeting; structural design and weight limitations; fuel capacity; and practical issues such as airport runway/taxiway and gate dimensions may yield a sizeable potential benefit in fuel burn and emissions. Long, slender wings may necessitate radically different structural and manufacturing concepts. Load control systems may prove essential to the feasibility of very high aspect ratio designs. Optimal wing span may lead to the need for folding outer wing sections. This topic aims to provide a preliminary design study involving the capture of the current state of the art, an analysis of potential gains through the use of very high aspect ratio wings in the various transport aircraft market segments [regional, short-medium and long range]. Different design concepts should be analysed, paying particular attention to design constraints such as those mentioned above. A proposed ‘best in class’ conceptual/preliminary design should be completed, starting from a selected reference aircraft for comparison in terms of performance. The estimated gains should be validated experimentally by scaled model wind tunnel tests, at least in terms of aerodynamic performance, possibly in terms of noise performance as well. Please refer to the full topic descriptions document published in this call.
¿Quieres ejemplos? Puedes consultar aquí los últimos proyectos conocidos financiados por esta línea, sus tecnologías, sus presupuestos y sus compañías.
Capítulos financiables:
Los capítulos de gastos financiables para esta línea son:
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
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
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
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:
La tramitación de esta ayuda requiere de un nivel tecnológico mínimo en el proyecto de 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.
Características de la financiación
Intensidad de la ayuda:
Sólo fondo perdido
+ info
Fondo perdido:
1. Countries eligible for funding: described in Annex A of the Clean Sky 2 Work Plan.
2. Eligibility and admissibility conditions: described in Annex B & Annex C of the Clean Sky 2 Work Plan.
Proposal page limits and layout: Please refer to Part B of the proposal template in the submission tool below.
3. Evaluation
Evaluation criteria, scoring and thresholds: described in Annex F of the Clean Sky 2 Work Plan.
Submission and evaluation processes: described in the Clean Sky 2 Rules for submission, evaluation, selection, award and review procedures of calls for proposals.
4. Indicative time for evaluation and grant agreement: maximum 8 months from the date of closure of the call.
5. Proposal templates and model grant agreements (MGA):
Proposal templates are available after entering the submission tool below.
H2020 Clean Sky 2 JU MGA for Partners - Multi-Beneficiary
H2020 Clean Sky 2 JU MGA for Partners - Mono-Beneficiary
H2020 Annotated Grant Agreement
6. Additional provisions:
Clean Sky 2 Budget Flexibility: described in Annex G of the Clean Sky 2 JU Work Plan.
Members of consortium are required to conclude a consortium agreement prior to the signature of the grant agreement.
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... 1. Countries eligible for funding: described in Annex A of the Clean Sky 2 Work Plan.
2. Eligibility and admissibility conditions: described in Annex B & Annex C of the Clean Sky 2 Work Plan.
Proposal page limits and layout: Please refer to Part B of the proposal template in the submission tool below.
3. Evaluation
Evaluation criteria, scoring and thresholds: described in Annex F of the Clean Sky 2 Work Plan.
Submission and evaluation processes: described in the Clean Sky 2 Rules for submission, evaluation, selection, award and review procedures of calls for proposals.
4. Indicative time for evaluation and grant agreement: maximum 8 months from the date of closure of the call.
5. Proposal templates and model grant agreements (MGA):
Proposal templates are available after entering the submission tool below.
H2020 Clean Sky 2 JU MGA for Partners - Multi-Beneficiary
H2020 Clean Sky 2 JU MGA for Partners - Mono-Beneficiary
H2020 Annotated Grant Agreement
6. Additional provisions:
Clean Sky 2 Budget Flexibility: described in Annex G of the Clean Sky 2 JU Work Plan.
Members of consortium are required to conclude a consortium agreement prior to the signature of the grant agreement.
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 H2020 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.
8. Additional documents:
Clean Sky 2 Joint Technical Programme
Clean Sky 2 JU Financial Rules
Clean Sky 2 JU Regulation of Establishment
H2020 Regulation of Establishment
H2020 Rules for Participation
H2020 Specific Programme
2. Eligibility and admissibility conditions: described in Annex B & Annex C of the Clean Sky 2 Work Plan.
Proposal page limits and layout: Please refer to Part B of the proposal template in the submission tool below.
3. Evaluation
Evaluation criteria, scoring and thresholds: described in Annex F of the Clean Sky 2 Work Plan.
Submission and evaluation processes: described in the Clean Sky 2 Rules for submission, evaluation, selection, award and review procedures of calls for proposals.
4. Indicative time for evaluation and grant agreement: maximum 8 months from the date of closure of the call.
5. Proposal templates and model grant agreements (MGA):
Proposal templates are available after entering the submission tool below.
H2020 Clean Sky 2 JU MGA for Partners - Multi-Beneficiary
H2020 Clean Sky 2 JU MGA for Partners - Mono-Beneficiary
H2020 Annotated Grant Agreement
6. Additional provisions:
Clean Sky 2 Budget Flexibility: described in Annex G of the Clean Sky 2 JU Work Plan.
Members of consortium are required to conclude a consortium agreement prior to the signature of the grant agreement.
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... 1. Countries eligible for funding: described in Annex A of the Clean Sky 2 Work Plan.
2. Eligibility and admissibility conditions: described in Annex B & Annex C of the Clean Sky 2 Work Plan.
Proposal page limits and layout: Please refer to Part B of the proposal template in the submission tool below.
3. Evaluation
Evaluation criteria, scoring and thresholds: described in Annex F of the Clean Sky 2 Work Plan.
Submission and evaluation processes: described in the Clean Sky 2 Rules for submission, evaluation, selection, award and review procedures of calls for proposals.
4. Indicative time for evaluation and grant agreement: maximum 8 months from the date of closure of the call.
5. Proposal templates and model grant agreements (MGA):
Proposal templates are available after entering the submission tool below.
H2020 Clean Sky 2 JU MGA for Partners - Multi-Beneficiary
H2020 Clean Sky 2 JU MGA for Partners - Mono-Beneficiary
H2020 Annotated Grant Agreement
6. Additional provisions:
Clean Sky 2 Budget Flexibility: described in Annex G of the Clean Sky 2 JU Work Plan.
Members of consortium are required to conclude a consortium agreement prior to the signature of the grant agreement.
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 H2020 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.
8. Additional documents:
Clean Sky 2 Joint Technical Programme
Clean Sky 2 JU Financial Rules
Clean Sky 2 JU Regulation of Establishment
H2020 Regulation of Establishment
H2020 Rules for Participation
H2020 Specific Programme
Garantías:
No existen condiciones financieras para el beneficiario.
Información adicional de la convocatoria
Efecto incentivador:
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:
No conocemos el presupuesto total de la línea
Minimis:
Esta línea de financiación NO considera una “ayuda de minimis”.
Puedes consultar la normativa
aquí.
Otras ventajas
Sello PYME:
Tramitar esta ayuda con éxito permite conseguir el sello de calidad de “sello pyme innovadora”. Que permite ciertas ventajas fiscales.
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