CORDIS provides links to public deliverables and publications of HORIZON projects.
Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .
Deliverables
Deliverable will develop a number of layouts to power the HTEP and evaluate the advantages and disadvantages of these layouts.
Risk Management and quality and innovation impact assessment strategy (opens in new window)Provide a risk management framework for the EFACA project, to ensure that adverse situations are properly managed along the evolution of the project. The document includes the processes, tools and procedures that will be used to manage and control those events that could have a negative impact. It exposes the proposed risk management approach of the project for managing and controlling all project risks. Moreover, this report will address the roles and responsibilities of the organization, the risk identification, as well as risk assessment and mitigation plans. (i) 1st version M8; (ii) 2nd version M20; (iii) 3rd version M32; (iv) 4th version M48
Specifications for Advisory Board (opens in new window)This document will describe the expected contribution of the Advisory Board, such as the revision of documents, participation in meetings, etc. It will be discussed in the Kick off meeting.
Shaping the GTE concept, selection of parameters and design scheme. Determination of GTE mass. Shaping the propeller concept, selection of parameters and design scheme. Determination of propeller mass (opens in new window)Deliverable will identify the parameters of the main engine components, the basic geometric parameters of the air-gas duct, the engine design diagram, developed a mathematical model of the engine, the choice of control laws and determined parameters in the main design points, selected design diagram of the engine, the evaluation of its mass and overall dimensions.Deliverable will also define the parameters of the propeller; the basic geometric parameters of the propeller; the method of controlling the propeller; the design scheme of the propeller, the evaluation of its mass and overall dimensions.
Requirements for HTEP elements (opens in new window)Deliverable will identify critical mass and size requirements (for all elements), required power and fuel consumption for the gas turbine engine, electric engine power and efficiency, required propeller parameters, and required FC performance parameters for HTEP elements.
Analysis of the Liquid hydrogen system for aero engine applications (opens in new window)The report describes the technical results of the process simulation of the systems comprising liquid hydrogen tank, cryogenic pump, and vaporizer for use in both gas turbines and fuel cells, which differ, among others, in the pressurization level. The results include also the main technical specification for the main equipment listed above. This deliverable refers to Task 3.1.
Report on the realization of the liquefaction, storage and vaporization test rig and on the update of the combustion test rig (opens in new window)This report describes the design criteria and the design work of the liquefaction, storage and vaporization test rig. Moreover, it describes the construction procedure, focusing on the issues encountered and the solutions adopted. This report refers to Task 3.3.
Report the promising technologies to reduce aviation noise exposure at airports around the EU and world (opens in new window)The currently investigated promising technologies (EU Clean Sky and Clean Aviation programs, USA FAA and NASA programs CLEEN and ASCENT) will be evaluated.
Results of aircraft emission inventory estimation for current fleet and projected trends of aviation neutrality by 2050 (opens in new window)Assessment of aircraft contribution to global emission for current fleet and updated fleet for the CAEP/EUROCONTROL mid-and long-term forecasting scenarios will be delivered. Inventory assessment will be provided for the classes of aircraft
Review of existing proposals in the field of creating hybrid turbo-electric propulsions for regional aircraft using fuel cells (opens in new window)Review and analysis of existing and currently developed hybrid propulsion systems for aviation applications, including fuel cells (FC). Technical problems of their production and operation. Advantages and disadvantages of existing and currently developed hybrid propulsion systems.
Results of aircraft noise assessment at aircraft, airport and fleet levels with complementarily analysis of their calculation and measuring tools (opens in new window)Assessment of aircraft noise exposure at airport level for current fleet and updated fleet for the CAEP/EUROCONTROL mid-and long-term forecasting scenarios will be delivered. Noise exposure assessment will be realised by calculations at airport level due to change in aircraft design and fleet transformation till 2050.
Types and roles of battery powered aircraft (opens in new window)This deliverable will analyse relevant technologies in detail, bearing in mind that they may be different for distinct classes of aircraft. It will also address other issues, gaps or risks factors precluding the proper and timely development and implementation of the market of electrical small short range aircrafts powered by batteries. It will be the outcome of task 6.2 Batteries production and disposal sustainable life cycle
Exploitation and IPR management Plan and reporting activities (opens in new window)Description of the overall exploitation strategy and follow-up activities reporting of the consortium and the actions to be carried out by each partner. Detailed outline of the actions until the end of the project and in the 2 years following the project’s end.Description of the guidelines for Intellectual Property Rights (IPR) management as derived from the EFACA Grant Agreement and Consortium Agreement. A procedure is presented covering identification of potential innovations, documentation, tracking and protection of Intellectual Property derived from the EFACA project.(i) 1st report: M6; (ii) 2nd report: M18; (iii) 3rd report: M36; (iv) 4th report: M48
Report the promising technologies to reduce global aviation emission (opens in new window)The currently investigated promising technologies for fuel burn and engine emission reduction (EU Clean Sky and Clean Aviation programs, USA FAA and NASA programs CLEEN and ASCENT) will be evaluated
Management and Coordination Handbook (opens in new window)This document will guide and support the management and implementation of EFACA, deploying all the relevantinformation and tools for this purpose.
Application of battery technologies to aircraft (opens in new window)This deliverable will study the current state, as well as the potential and limitations of the battery power for small short-range aircraft including UAM. It will be the outcome of task 6.1 Advances in battery technology
Technical and economic indicators of the systems. (opens in new window)Technical specifications and associated operating procedures and costs of acquisition and maintenance.
Preliminary shaping of the concept and typical flight profile of the aircraft with HTEP. Preliminary requirements for HTEP (opens in new window)Deliverable will tentatively conceptualize the aircraft, taking into account HTEP with fuel cells, forming preliminary requirements for HTEP with respect to safety issues and its operation when flying from sea level to cruising altitude
Shaping the FC concept of hydrocarbon fuel – electrical energy (opens in new window)Deliverable will define the basic parameters of FC, develop the FC design concept with an estimate of its mass and overall dimensions; form the conditions for FC placement in the aircraft design, taking into account the hydrogen feed scheme.
Rationale for the choice of design solutions in the development of liquid hydrogen in aircraft fuel systems. (opens in new window)Components of the liquid hydrogen system from storage tank to combustion chamber. Available technologies to meet cryogenic requirements of the liquid hydrogen.
Shaping the FC concept of hydrogen – electrical energy (opens in new window)Deliverable will define the basic parameters of FC, develop a FC design concept with an estimate of its mass and overall dimensions; form the conditions for FC placement in the aircraft design, taking into account the hydrogen feed scheme.
Shaping the vaporizer concept, determination of its mass (opens in new window)Deliverable will develop the concept of the evaporator, taking into account the possible design and layout, the type of hot coolant; investigate the features of the hydrogen boiling process using experimental data and CFD modeling; determine the design of the evaporator and its mass and dimensions.
Report on hydrogen-fired propulsion (opens in new window)The report describes the process simulation of pure-hydrogen fired gas turbines, touching also on the expected issues of flame stability and NOx formation. This deliverable refers to Task 3.2.
Data Management Plan (opens in new window)A DMP describes the data management life cycle for the data to be collected, processed and/or generated by EFACA project. Detailed information on the procedures that will be implemented by the EFACA complying with national and EU legislation will be provided.(i) 1st report: M6; (ii) 2nd report: M18; (iii) 3rd report: M36; (iv) 4th report: M48
Communication and Dissemination Plan (opens in new window)Definition of how, when and where to communicate the project’s activities and results to a wide range of target groups. Will include the general communication activities (common to the whole consortium) and the contribution of all partners, as each partner will complete a table with their planned dissemination events and their possibilities of “spreading the word” about the project. Communication materials: Project logo and identity, leaflet, poster, roll-up, templates will be developed.
Current pathways for SAF production (opens in new window)Description of the situation in Europe and worldwide about the production of SAF with emphasis on the new pathways approval and the perspectives on the emerging techniques (Task 9.1).
Selection of criteria for evaluating HTEP schemes (opens in new window)Deliverable will review existing comprehensive criteria for evaluating the effectiveness of a propulsion system as part of an aircraft. New criteria for evaluating HTEP efficiency are selected or proposed, with environmental friendliness in mind.
Recommendations to the project, safety instructions and environmental safety when using hydrogen. (opens in new window)Operating aspects of liquid hydrogen including volatility, flammability, venting, modes of operation and safety.
Publications
Author(s):
K.Kazhan, K. Synylo, O. Zaporozhets S. Karpenko
Published in:
International Journal Sustainable Aviation, 2023
Publisher:
N/A
DOI:
10.1504/IJSA.2023.127489
Author(s):
Boichenko S., Danilin O., Shkilniuk I., Yakovlieva A., Khotian A., Pavlovskyi M., Lysak Roksolana, Shamanskyi S., Kriuchkov A., Tarasiuk O.
Published in:
Eastern-European Journal of Enterprise Technologies, 2023
Publisher:
N/A
DOI:
10.15587/1729-4061.2023.280046
Author(s):
Synylo K.,Makarenko V., Krupko A., Tokarev V
Published in:
Eastern-European Journal of Enterprise Technologies, 2024
Publisher:
N/A
DOI:
10.15587/1729-4061.2024.302793
Author(s):
Horobtsov, I., Cherniak, L., Radomska, M., Tykhenko, O., & Synylo, K.
Published in:
Ecological Safety and Balanced Use of Resources Journal, 2023
Publisher:
N/A
DOI:
10.31471/2415-3184-2023-14(2)-09
Author(s):
Rosa Maria Arnaldo Valdés*, Victor Fernando Gómez Comendador, Maria Zamarreño, Suarez, Francisco Perez Moreno, and Raquel Delgado-Aguilera Jurado
Published in:
International Symposium on Electric Aircraft and Autonomous Systems, 2024, ISSN 0000-0000
Publisher:
IOP SCIENCE
DOI:
10.1088/1742-6596/2716/1/012012
Author(s):
T. Hikmet KARAKOÇ Oleksandr ZAPOROZHETS Andrzej LESKI Ali Haydar ERCAN Alper DALKIRAN
Published in:
International Symposium on Electric Aircraft and Autonomous Systems, 2023, ISSN 0000-0000
Publisher:
N/A
Author(s):
Sergii Fil, Dmytro Berbenets, Khaustov Andrii, Urban Oleksandra and Bondarchuk Oleksandr
Published in:
International Symposium on Electric Aircraft and Autonomous Systems (ISEAS-23), 2023, ISSN 0000-0000
Publisher:
N/A
Author(s):
Boichenko, Sergii Yakovlieva, Anna Zaporozhets Oleksandr
Published in:
2023, ISSN 0000-0000
Publisher:
N/A
DOI:
10.1007/978-3-031-34350-6
Author(s):
Ribun, V., Boichenko, S., Yakovlieva, A., Chelaydyn, L., Dubrovska, V., Shkyar, V., Wos, P.
Published in:
Systems, Decision and Control in Energy IV. Studies in Systems, Decision and Control, vol 454. Springer, Cham., 2023
Publisher:
SPRINGER NATURE
DOI:
10.1007/978-3-031-22464-5_19
Author(s):
Boichenko S., Zaporozhets A., Yakovlieva A., Shkilniuk I.
Published in:
Studies in Systems, Decision and Control, vol 510. Springer, Cham, 2024
Publisher:
N/A
DOI:
10.1007/978-3-031-44351-0
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