ELECTRA | Efficient and Light Electrical Compressor for Tilt-Rotor Aircraft

Summary
The main objectives of the proposed ELECTRA project are:
1. The development of an optimal architecture for a bleedless cabin pressurization system (CPS)
2. The development, manufacturing, test and qualification of CPS hardware suitable for flight testing on the next-generation tiltrotor technology demonstrator

To achieve the objectives, ELECTRA will:
1. Set up a simulation platform
2. Perform system-level and equipment-level trade-off analyses
3. Develop equipment hardware: cabin pressure management system, electrical compressor, electronic control unit and its firmware, outflow valve and several other system components
4. Develop a test rig for hardware testing, emulating the cabin pressurization system, and test the developed hardware
5. Develop a prototype qualification unit and perform environmental qualification tests
6. Develop a prototype flight unit, cleared for flight on the next-generation tiltrotor technology demonstrator

ELECTRA contributes to task 1.6.3 of the Joint Technology Programme, “Pressurization and Environmental Control System Components Design, Manufacturing and Testing”, by contributing to these JTP objectives:
• Reduction of carbon emissions through improved energy efficiency
• Reduced cost of ownership
• European industrial leadership on ‘Smart, Green and Integrated Transport’
• Improving mobility through new mobility concepts (more flexible, resilient, effective and affordable)
• Spin-off from research innovation activities to other aircraft
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More information & hyperlinks
Web resources: https://cordis.europa.eu/project/id/831999
Start date: 01-02-2019
End date: 31-03-2023
Total budget - Public funding: 1 874 295,00 Euro - 1 200 000,00 Euro
Cordis data

Original description

The main objectives of the proposed ELECTRA project are:
1. The development of an optimal architecture for a bleedless cabin pressurization system (CPS)
2. The development, manufacturing, test and qualification of CPS hardware suitable for flight testing on the next-generation tiltrotor technology demonstrator

To achieve the objectives, ELECTRA will:
1. Set up a simulation platform
2. Perform system-level and equipment-level trade-off analyses
3. Develop equipment hardware: cabin pressure management system, electrical compressor, electronic control unit and its firmware, outflow valve and several other system components
4. Develop a test rig for hardware testing, emulating the cabin pressurization system, and test the developed hardware
5. Develop a prototype qualification unit and perform environmental qualification tests
6. Develop a prototype flight unit, cleared for flight on the next-generation tiltrotor technology demonstrator

ELECTRA contributes to task 1.6.3 of the Joint Technology Programme, “Pressurization and Environmental Control System Components Design, Manufacturing and Testing”, by contributing to these JTP objectives:
• Reduction of carbon emissions through improved energy efficiency
• Reduced cost of ownership
• European industrial leadership on ‘Smart, Green and Integrated Transport’
• Improving mobility through new mobility concepts (more flexible, resilient, effective and affordable)
• Spin-off from research innovation activities to other aircraft

Status

CLOSED

Call topic

JTI-CS2-2018-CfP08-FRC-01-24

Update Date

26-10-2022
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Horizon 2020
H2020-EU.3. SOCIETAL CHALLENGES
H2020-EU.3.4. SOCIETAL CHALLENGES - Smart, Green And Integrated Transport
H2020-EU.3.4.5. CLEANSKY2
H2020-EU.3.4.5.3. IADP Fast Rotorcraft
H2020-CS2-CFP08-2018-01
JTI-CS2-2018-CfP08-FRC-01-24 High efficiency full electrical low pressure Compartment Pressure Control System for tilt-rotor applications