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HyPoGA

Feasibility study of a superefficient hybrid power train as a replacement unit for existing engines - Hybrid Power for General Aviation (HyPoGA)

Total Cost €

0

EC-Contrib. €

0

Partnership

0

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Project "HyPoGA" data sheet

The following table provides information about the project.

Coordinator
JOCKEL BERNHARD 

Organization address
address: GOETHESTRASSE 4A
city: DARMSTADT
postcode: 64285
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 Germany [DE]
 Project website http://www.hypoga.com
 Total cost 71˙429 €
 EC max contribution 50˙000 € (70%)
 Programme 1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
2. H2020-EU.2.3.1. (Mainstreaming SME support, especially through a dedicated instrument)
 Code Call H2020-SMEINST-1-2014
 Funding Scheme SME-1
 Starting year 2015
 Duration (year-month-day) from 2015-05-01   to  2015-10-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    JOCKEL BERNHARD DE (DARMSTADT) coordinator 50˙000.00
2    LIMBACH STEFAN DE (OSTRACH) participant 0.00

Map

 Project objective

Worldwide, over 280.000 General Aviation (GA) aircrafts are in use (28.000 in Europe) and most aircraft in this engine-power class (approx. 200 kW) are operated several hours per day in commercial services. The total operating costs are about 213 T€ per year. Combustion engines are designed for the maximum power needed for take-off and climbs (peak-loading), though in cruise flight only approx. 65 % of the power is required. The overall objective of the HyPoGA innovation project is to develop a superefficient, hybridized 200 kW aircraft engine by integration of a 140 kW combustion and a 60 kW electrical engine which will allow a fuel reduction of about 30% and a total cost reduction of 27% ~ 48 T€. This engine will be certified as a replacement unit according to EU and US aviation laws and regulations. The annual demand for replacement engines is ~3.000. The additional weight of the electrical components (electrical engine, batteries) is counter played by the weight reduction of a smaller combustion engine and the fuel savings. The innovative power train will contribute significantly to reduced costs of operations and a massive reduction of CO2 emission. Furthermore, the electrical engine constitutes a back-up increasing the safety of aircraft operations (two engines instead of one). These aspects create a unique selling point and competitive advantage for potential customers.

The objectives of the feasibility study are (i) a market research study and analysis (SWOT-Analysis), (ii) a technological feasibility (e.g. final design definition) and (iii) an economic and financial feasibility (including marketing strategy, certification, financial plan). The results will be elaborated in a business plan.

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The information about "HYPOGA" are provided by the European Opendata Portal: CORDIS opendata.

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