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TRIMIS

Novel Integration of Powerplant System Equipment

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€6 235 001
EU Contribution
€6 235 001
Project Acronym
NIPSE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-MG-2014_TwoStages
Link to CORDIS
Objectives

The main objectives of NIPSE are to provide technologies to:

  • reduce Integrated PowerPlant System development time of future aero engines by 10%
  • enable the 2 to 3% environmental related gains in fuel burn and reduction in emissions looked at by these new aero engine architectures (especially Ultra High Bypass Ratio and Open Rotor) through improved aero engine equipment solutions.

The objectives will be achieved through several elements. NIPSE will develop key equipment and capabilities, in particular:

  • multivariable optimisation methodologies,
  • more efficient heat exchangers,
  • smaller equipment, and
  • novel electrical and pneumatic interconnections to enable a means of developing better competitive solutions for future aero engine architectures in a shorter development time.

This will be performed taking into account line maintenance issues to ensure the improvements of aero engine architecture and associated equipment do not adversely impact the passenger experience.

 

This is relevant to the work programme in increasing competitiveness of European companies through development of technologies to achieve fast, best solution approaches for installation of aero engine equipment, allowing securement and enhancement of existing European workload for this equipment, and enhancing exports for Europe.

 

Development of key technology in equipment definition, installation and optimisation enables existing and future aero engine technologies to better achieve their goals, thus enhancing European competitiveness within aero engine market.

 

Without NIPSE, the true potential of the new aero engine architectures will not be achieved and societal gains will not be met.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.

Partners

Lead Organisation
Organisation
Safran Nacelles
Address
Route Du Pont Viii, 76700 Gonfreville L Orcher, France
EU Contribution
€946 413
Partner Organisations
Organisation
Compania Espanola De Sistemas Aeronauticos
Address
AVENIDA JOHN LENNON 4, 28906 MADRID (GETAFE), Spain
Organisation website
EU Contribution
€698 250
Organisation
Safran Aircraft Engines
Address
2 Bvd Du General Martial-Valin, 75724 Paris, France
EU Contribution
€514 250
Organisation
Stichting Centrum Voor De Ontwikkeling Van Transport En Logistiek In Europa
Address
Van Nelleweg 1, 3044 BC Rotterdam, Netherlands
Organisation website
EU Contribution
€595 000
Organisation
Thermocoax Sas
Address
USINE DE PLANQUIVON, 61430 ATHIS DE L ORNE, France
EU Contribution
€504 575
Organisation
Bae Systems (Operations) Limited
Address
Warwick House, Farnborough Aerospace Centre, FARNBOROUGH, HAMPSHIRE, GU14 6YU, United Kingdom
Organisation website
EU Contribution
€417 000
Organisation
Meggitt Advanced Composites Limited
Address
Atlantic House Aviation Park West Bournemouth International Airport, Christchurch Dorset, BH23 6EW, United Kingdom
Organisation website
EU Contribution
€972 014
Organisation
Arttic
Address
58A rue du Dessous des Berges, 75013 PARIS, France
Organisation website
EU Contribution
€345 000
Organisation
Archimhdhs Kentron Kainotomias Kaidimiourgias Archimedes Center For Innovation And Creation
Address
MPOYMPOULINAS 3, 17455 ALIMOS ATHINA, Greece
EU Contribution
€735 000
Organisation
Safran Electrical & Power
Address
1 Rue Louis Bleriot Parc Dactivite Andromede, 31702 Blagnac, France
EU Contribution
€507 500

Technologies

Technology Theme
Aircraft propulsion
Technology
Ultra-high bypass ratio jet engine
Development phase
Research/Invention

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