HERRB

Helicopter Electric Regenerative Rotor Brake

 Coordinatore UNIVERSITY OF BRISTOL 

 Organization address address: TYNDALL AVENUE SENATE HOUSE
city: BRISTOL
postcode: BS8 1TH

contact info
Titolo: Dr.
Nome: David
Cognome: Drury
Email: send email
Telefono: +44 117 9545390

 Nazionalità Coordinatore United Kingdom [UK]
 Totale costo 698˙331 €
 EC contributo 523˙745 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2011-01
 Funding Scheme JTI-CS
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-10-01   -   2015-03-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    UNIVERSITY OF BRISTOL

 Organization address address: TYNDALL AVENUE SENATE HOUSE
city: BRISTOL
postcode: BS8 1TH

contact info
Titolo: Dr.
Nome: David
Cognome: Drury
Email: send email
Telefono: +44 117 9545390

UK (BRISTOL) coordinator 382˙990.00
2    Motor Design Ltd

 Organization address address: Scotland Street 4
city: Ellesmere
postcode: SY12 OEG

contact info
Titolo: Dr.
Nome: David
Cognome: Staton
Email: send email
Telefono: +44 1691 623305

UK (Ellesmere) participant 72˙093.00
3    ADAPTED SOLUTIONS GmbH

 Organization address address: Annaberger Strasse 240
city: CHEMNITZ
postcode: D-09125

contact info
Titolo: Dr.
Nome: Thomas
Cognome: Barucki
Email: send email
Telefono: 493715000000
Fax: 493715000000

DE (CHEMNITZ) participant 68˙662.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

rotor    electrical    aircraft    energy    power    hydraulic    coupled    benefits    exists   

 Obiettivo del progetto (Objective)

'The proposal outlines a design process coupled with a full evaluation and testing phase for a fully electric replacement for the current mechanical-hydraulic rotor brake system that exists on most large rotorcraft in production currently allow regenerative capture of the inertial energy stored in the aircraft drivetrain during deceleration.

The concept offers further potential alongside other similar projects to downsize and in the long term even remove the hydraulic circuit that exists on aircraft resulting such that the benefits of electrical systems becomes significant. Furthermore, once on the aircraft, installation of the equipment provides potential for several performance and system benefits as there would exist coupled to the rotor a bi-directional power flow controller within an independent energy store. Possible systems would include fast rotor start, auto-gyro assist for safe landing in the event of primary power failure and extra power on-board electrical power generation for redundancy during flight.'

Altri progetti dello stesso programma (FP7-JTI)

ECO-FAIRS (2011)

ECO-design and manufacturing of thermoplastic structural fairings for helicopters

Read More  

ALIAS (2013)

Acoustic Liners for air conditioning system

Read More  

ADHERO (2011)

Aerodynamic Design Optimisation of a Helicopter Fuselage including a Rotating Rotor Head

Read More