ACRONYM: FRIENDCOPTER
Integration of Technologies in Support of a Passenger and Environmentally Friendly Helicopter
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  General Information

Today's helicopters need to be improved further with respect to environmental and public acceptance. Helicopters generate external noise, cabin noise and vibration due to the complex nature of their dynamic systems and suffer from NOx emission like other transport systems. It is therefore very essential that the new generation rotorcraft addresses these issues to improve the situation, to make them environmentally friendly and acceptable to the general public. The modern society needs this indispensable system due to its ability to fly medical, rescue and law enforcement missions. These missions require flight profiles close to populated areas. Hence, a number of enhancements appears mandatory.

In detail, the following goals are envisaged:

  • External noise levels 10 dB below the current ICAO/JAA rules especially during approach.
  • A reduction of fuel consumption up to 20 % for high speed flights.
  • Cabin noise levels below 70 dBA similar to airliner cabins for normal cruise flight.
  • Cabin vibrations below 0,05 g corresponding to jet smooth ride comfort for the same flight regime.

Because of the large and fast rotating rotor, the non-symmetric rotor flow, the close vicinity of main gearbox and passenger position and the specific requests of engine performance, the targets mentioned above are highly challenging. In order to comply with the research objectives, an extreme high tech initiative is required, enabling European aeronautic industry to hold their own position against international competitors. In order to do so, short and long term objectives are planned targeting the following technology topics:

  • Short term objectives:
    Noise abatement flight procedures, cabin noise reduction, engine noise reduction
  • Long term objectives:
    Active blade control

The activities envisaged in FRIENDCOPTER are to provide a number of key deliverables. All of these will have undergone intense efficiency testing, mostly by flight tests.

  Project Data
Project Type: EU Project
Project Ref. No.: 502773
Duration: 1 March 2004 - 1 Sept. 2008
Main Contractor: VERTAIR EEIG
Contact Person: Valentin Kloeppel
  Email: valentin.kloeppel@eurocopter.com
Costs: 32,488,499 €
Project Homepage: www.friendcopter.org
  Partners (34)
AGUSTA S.P.A.  IT
AIRCELLE SAS  FR
ANOTEC CONSULTING S.L.  ES
CENTRO ITALIANO RICERCHE AEROSPAZIALI S.C.P.A.  IT
CRANFIELD UNIVERSITY  UK
DAHER LHOTELLIER AEROTECHNOLOGIES  FR
DEUTSCHES ZENTRUM FÜR LUFT- UND RAUMFAHRT E.V. - DLR  DE
EADS DEUTSCHLAND GMBH  DE
EUROCOPTER DEUTSCHLAND GMBH  DE
EUROCOPTER S.A.S.  FR
FORMTECH GMBH  DE
FREE FIELD TECHNOLOGIES S.A.  BE
GAMESA DESARROLLOS AERONAUTICOS S.A.  ES
INGENIERIA DE SISTEMAS PARA LA DEFENSA DE ESPAÑA, S.A.  ES
INGENIERIA Y ECONOMIA DEL TRANSPORTE S.A.  ES
INSTITUTO DE SOLDADURA E QUALIDADE  PT
INSTITUTO SUPERIOR TECNICO  PT
KUNGLIGA TEKNISKA HÖGSKOLAN STOCKHOLM  SE
LEUVEN MEASUREMENTS AND SYSTEMS INTERNATIONAL NV - LMS  BE
NATIONAAL LUCHT- EN RUIMTEVAART LABORATORIUM - NLR  NL
OFFICE NATIONAL D'ÉTUDES ET DE RECHERCHES AÉROSPATIALES - ONERA  FR
PAULSTRA S.N.C  FR
PIEZO TECH A/S (NOLIAC A/S)  DK
POLITECNICO DI MILANO  IT
RIGAS TEHNISKA UNIVERSITATE  LV
TURBOMECA SA  FR
UNIVERSITA DEGLI STUDI DI ROMA TRE  IT
UNIVERSITÄT OLDENBURG  DE
UNIVERSITY OF PATRAS  GR
VERTAIR EEIG  BE
VYZKUMNY A ZKUSEBNI LETECKY USTAV A.S.  CZ
WESTLAND HELICOPTERS LTD  UK
WYTWORNIA SPRZETU KOMUNIKACYJNEGO PZL-SWIDNIK "SA"  PL
ZF LUFTFAHRTTECHNIK GMBH  DE
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