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MAHEPA SIGNED

Modular Approach to Hybrid Electric Propulsion Architecture

Total Cost €

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EC-Contrib. €

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Partnership

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Project "MAHEPA" data sheet

The following table provides information about the project.

Coordinator
PIPISTREL VERTICAL SOLUTIONS DOO PODJETJE ZA NAPREDNE LETALSKE RESITVE 

Organization address
address: VIPAVSKA CESTA 2
city: AJDOVSCINA
postcode: 5270
website: n.a.

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Slovenia [SI]
 Project website http://www.mahepa.eu
 Total cost 8˙979˙178 €
 EC max contribution 8˙979˙178 € (100%)
 Programme 1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
 Code Call H2020-MG-2016-Two-Stages
 Funding Scheme RIA
 Starting year 2017
 Duration (year-month-day) from 2017-05-01   to  2021-04-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    PIPISTREL VERTICAL SOLUTIONS DOO PODJETJE ZA NAPREDNE LETALSKE RESITVE SI (AJDOVSCINA) coordinator 3˙180˙754.00
2    COMPACT DYNAMICS GMBH DE (STARNBERG) participant 1˙808˙718.00
3    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 1˙409˙602.00
4    UNIVERSITAET ULM DE (ULM) participant 1˙234˙610.00
5    UNIVERZA V MARIBORU SI (MARIBOR) participant 477˙475.00
6    POLITECNICO DI MILANO IT (MILANO) participant 291˙875.00
7    TECHNISCHE UNIVERSITEIT DELFT NL (DELFT) participant 265˙625.00
8    H2FLY GMBH DE (STUTTGART) participant 205˙022.00
9    PIPISTREL DOO PODJETJE ZA PROIZVODNJO ZRACNIH PLOVIL SI (AJDOVSCINA) participant 105˙495.00

Map

 Project objective

The overall objective of MAHEPA is to bridge the gap between the research and product stage of a low emission propulsion technology to meet the environmental goals for aviation towards the year 2050. Two variants of a low emission, high efficiency, serial-hybrid-electric propulsion architecture will be advanced to TRL 6: the first uses a hydrocarbon fuelled internal combustion engine and an electric generator as primary power source, while in the second a hydrogen fuel cell is used to produce power showcasing the flexibility of the architecture. Common to both variants is the power control module, used to implement advanced power management methods to optimize mission, range and emissions of hybrid electric aircraft, and the new power electronic devices namely a highly efficient, airborne qualified electric propulsion motor and next-generation inverter technology. The modular approach is further demonstrated by integration and flight testing of each variant on a different small aircraft to showcase flexibility and scalability of the powertrain. A visionary implementation study towards commercial/transport category aircraft rounds up the project. The core value of MAHEPA is to build-up technological know-how and use flight test data to validate performance, efficiency and emission reduction capabilities of above technologies. This will allow to make conclusions about the suitability of these solutions towards megawatt-scale hydrocarbon driven hybrids and zero-emission hydrogen-powered solutions. For small aircraft this propulsion system development can be the door opener for a commercialized, new, low emission, highly efficient airplane category.

 Deliverables

List of deliverables.
Newsletters 2 Websites, patent fillings, videos etc. 2019-11-28 17:28:24
Ground infrastructure investment plan Documents, reports 2019-11-28 17:28:25
Project website Websites, patent fillings, videos etc. 2019-05-23 13:25:22
Certification basis composition report Documents, reports 2019-05-23 13:15:35
Newsletters 1 Websites, patent fillings, videos etc. 2019-05-23 13:25:22
Concept of Modular Architecture for Hybrid Electric Propulsion of Aircraft Documents, reports 2019-05-30 17:38:24

Take a look to the deliverables list in detail:  detailed list of MAHEPA deliverables.

 Publications

year authors and title journal last update
List of publications.
2020 Riboldi C. E. D., Mariani L., Trainelli L., Rolando A., Salucci F.
Assessing the Effect of Hybrid-Electric Power-Trains on Chemical and Acoustic Pollution
published pages: , ISSN: , DOI:
Aerospace Europe Conference February 25-28, 2020 2020-03-05
2020 Trainelli L., Bruglieri M., Salucci F., Gabrielli D.
Optimal Definition of a Short-Haul Air Transportation Network for Door-to-Door Mobility
published pages: , ISSN: , DOI:
Aerospace Europe Conference February 25-28, 2020 2020-03-05
2020 Salucci F., Riboldi C. E. D., Trainelli L., Rolando A.
Optimal Sizing and Operations of a Battery Recharging Infrastructure for a Regional Airport
published pages: , ISSN: , DOI:
Aerospace Europe Conference February 25-28, 2020 2020-03-05
2020 Rolando A., Salucci F., Trainelli L., Riboldi C. E. D., Khan Y. M.
On the Design of an Electric-Powered Micro-Feeder Aircraft
published pages: , ISSN: , DOI:
Aerospace Europe Conference February 25-28, 2020 2020-03-05
2020 Trainelli L., Riboldi C. E. D., Salucci F., Rolando A.
A General Preliminary Sizing Procedure for Pure-Electric and Hybrid-Electric Airplanes
published pages: , ISSN: , DOI:
Aerospace Europe Conference February 25-28, 2020 2020-03-05
2019 PRAPOTNIK BRDNIK, Anita, KAMNIK, Rok, MARKSEL, Maršenka, BOŽIČNIK, Stanislav.
Beginning steps of the electrification of commercial passenger aircraft transport
published pages: , ISSN: , DOI:
European Transport Conference 2019 October 9-11, 2019 2019-11-14
2019 Anita Prapotnik Brdnik, Rok Kamnik, Maršenka Marksel, Stanislav Božičnik
Market and Technological Perspectives for the New Generation of Regional Passenger Aircraft
published pages: 1864, ISSN: 1996-1073, DOI: 10.3390/en12101864
Energies 12/10 2019-10-15
2019 Trainelli L., Salucci F., Comincini D., Riboldi C. E. D., Rolando A.
Sizing and Performance of Hydrogen-Driven Airplanes
published pages: , ISSN: , DOI:
XXV Congresso Nazionale AIDAA September 9-12, 2019 2019-10-03
2019 Riboldi C. E. D., Bigoni F, Salucci F., Rolando A. , Trainelli L.
Switching to Electric Propulsion: Aero Club Fleet and Infrastructure Sizing
published pages: , ISSN: , DOI:
XXV Congresso Nazionale AIDAA September 9-12, 2019 2019-10-03
2019 Bruglieri M., Marchionni A. M., Trainelli L.
Optimization of the Demand Satisfied by a \'Micro-Feeder\' Hybrid-Electric Air Transport Service
published pages: , ISSN: , DOI:
XXV Congresso Nazionale AIDAA September 9-12, 2019 2019-10-03
2019 Salucci F., Trainelli L., Faranda R., Longo M.
An Optimization Model for Airport Infrastructures in Support to Electric Aircraft
published pages: , ISSN: , DOI:
2019-10-01
2019 Trainelli L., Salucci F., Rossi N., Riboldi C. E. D., Rolando A.
Preliminary Sizing and Energy Management of Serial Hybrid-Electric Airplanes
published pages: , ISSN: , DOI:
2019-10-01
2018 Bigoni F., Moreno-Perez A., Salucci F., Riboldi C. E. D., Rolando A., Trainelli L.
Design of Airport Infrastructures in Support of the Transition to a Hybrid-Electric Fleet
published pages: 10, ISSN: , DOI:
Advanced Aircraft Efficiency in a Global Air Transport System Conference (AEGATS 2018), Toulouse, France, October 23-25, 2018 October 23-25, 2018 2019-04-18

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