RELOAD | Regional turboprop loads control through active and passive technologies

Summary
A number of active and passive Loads Control and Alleviation concepts and technologies will be proposed, developed and evaluated. Aerodynamic design of an innovative spoiler will be undertaken, followed by a detailed aerodynamic characterisation of the spoiler and aileron capability for active loads control alleviation, conducted by means of CFD simulations and Wind Tunnel Tests. Novel passive loads alleviation concepts, such as passively morphing aerofoils using thickness and stiffness tailored skins or memory polymer skins and passively floating flaps, are going to be investigated and evaluated. A structural concept for an aeroelastic winglet for passive loads alleviation in manoeuvres and gusts will be developed.
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More information & hyperlinks
Web resources: https://cordis.europa.eu/project/id/686804
Start date: 01-12-2015
End date: 31-03-2019
Total budget - Public funding: 499 350,00 Euro - 499 350,00 Euro
Cordis data

Original description

A number of active and passive Loads Control and Alleviation concepts and technologies will be proposed, developed and evaluated. Aerodynamic design of an innovative spoiler will be undertaken, followed by a detailed aerodynamic characterisation of the spoiler and aileron capability for active loads control alleviation, conducted by means of CFD simulations and Wind Tunnel Tests. Novel passive loads alleviation concepts, such as passively morphing aerofoils using thickness and stiffness tailored skins or memory polymer skins and passively floating flaps, are going to be investigated and evaluated. A structural concept for an aeroelastic winglet for passive loads alleviation in manoeuvres and gusts will be developed.

Status

CLOSED

Call topic

JTI-CS2-2014-CFP01-REG-02-01

Update Date

27-10-2022
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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.3.4.5.2. IADP Regional Aircraft
H2020-CS2-CFP01-2014-01
JTI-CS2-2014-CFP01-REG-02-01 Aerodynamic characterization of control devices for wing loads control and aircraft response characterization of a regional turboprop aircraft