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Thermal Management for the Hybrid Electric Regional Aircraft

Project description

Designing new hybrid aircraft thermal management solutions

Regional and short/medium-range aircraft with hybrid electric power and propulsion systems generate excess heat, making onboard thermal management important. In this context, the EU funded TheMa4HERA project will develop, design and test innovative technologies to address the challenge of handling heat dissipation in the range of 300 to 1 000 kW, compared to the current 35-50 kW capacity of thermal management systems. To simulate and optimise component-level requirements for any given aircraft architecture, the project will develop a full digital twin. It will validate and demonstrate its results in a full scale test facility, and dissemination activities will ensure stakeholder support.

Objective

The TheMa4HERA project takes on the huge challenge of on-board thermal management that comes with the introduction of hybrid electric power and propulsion systems in Regional and Short and Medium Range aircraft. This will be achieved through development, design and testing at TRL 5 of wide range of innovative technologies from Air Supply, to Air Conditioning, Systems Thermal Management to Cabin Air Distribution. Whereas today’s thermal management systems need to handle a heat dissipation of about 35-50kW, tomorrow’s hybrid electric regional aircraft will have to handle heat dissipation in the range of 300 to 1.000kW! With a consortium composed out of all key aerospace players in the market of thermal management, this project will address almost all currently known thermal management technologies. Multiple two-way interactions loops with TRA-01 will be established integration requirements and feedback constraints and validation results, to allow for further aircraft architecture optimization iterations. Through the development of a full digital twin, the project will be able to simulate and optimize component level requirements for any given aircraft architecture. This architecture will be taken from the EXACT project, adjusted and refined throughout the project, to eventually reflect the final Hybrid Electric Aircraft architecture. The project will validate and demonstrate its results in a full-scale demonstration test facility at Fraunhofer IBP. With the further refined models, that will be available by then, the project will also be able to calculate the achievements towards the Expected Outcomes, in particular the environmental footprint. The Communication, Dissemination and Exploitation actions will make sure that all necessary stakeholders will also be supportive to the EIS of the first Hybrid Electric Regional Aircraft relying on TheMa4HERA thermal management technologies.

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Programme(s)

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Topic(s)

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Funding Scheme

Funding scheme (or “Type of Action”) inside a programme with common features. It specifies: the scope of what is funded; the reimbursement rate; specific evaluation criteria to qualify for funding; and the use of simplified forms of costs like lump sums.

HORIZON-JU-IA - HORIZON JU Innovation Actions

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Call for proposal

Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.

(opens in new window) HORIZON-JU-Clean-Aviation-2022-01

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Coordinator

HONEYWELL INTERNATIONAL SRO
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 2 825 675,73
Address
V PARKU 2325/16 CHODOV
148 00 PRAHA
Czechia

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Region
Česko Praha Hlavní město Praha
Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
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Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 5 332 745,37

Participants (23)

Partners (5)

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