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TRIMIS

Transmissions in Aircraft on Unique Path Wires

Project

TAUPE - Transmissions in Aircraft on Unique Path Wires


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Project website:
Duration:
Start date: 01/09/2008,
End date: 01/02/2012

Status: Finished
Funding details:
Total cost:
€5 464 766
EU Contribution:
€3 630 186

Overview

Background & policy context:

Thanks to the European Union's Research Framework Programmes (FP5 and FP6), the technologies for power and data transmissions over a unique path wires are now strongly developed. The OPERA project made feasible the High Speed/High Voltage transmissions for Power Line Communication. The U-Broad project demonstrated that Fast Ethernet (100 Mb/s) can be provided over existing telephone network cabling.

The TAUPE project was an extension of the application of these technologies within aircraft environment. Indeed this extension requires innovating solutions to address aeronautic-specific severe constraints (weight, space allocations, routes segregation, electro-magnetic compatibility, more complex electrical architecture, airworthiness, ruggedized network, dispatch and safety).

From POA and MOET results, the All Electric Aircraft is replacing conventional systems (hydraulic and pneumatic) with electric systems. But it is currently facing a drastic issue: the increase of the number of wires (each electric system needs a power supply and communication networks) with impacts on systems weight and space allocation. An elegant solution to save weight and space, is to use a unique path wire to transmit power and data. But even though the related technologies are now mature, each technology has its own specifications and dedicated chipset/wires architecture and is not compliant with the aeronautical environment. The aeronautic sector now needs innovative solutions to merge the architectures into one full avionics-shared electrical and communication network.

Objectives:

To support the All Electric Aircraft, TAUPE defined a fully optimised avionic architecture for power and data transmission on unique path wires (mixing the aircraft (A/C) power and communication networks). From this fully optimised architecture, the related specifications were provided (harness wiring and network equipments) and requirements for systems qualification were delivered.

The TAUPE results addressed the ACARE SRA and the Work Programme (Cost Efficient Air Transport) thanks to:

  • Targeting minimum system weight
  • Easy and cost effective installation and retrofit
  • Cost effective maintenance

Methodology:

LABINAL coordinated the project, which was divided into eight Workpackages (WPs):

  • 5 Research Technology Development (RTD) WPs
  • 1 Management WP
  • 2 other WPs

During the project, two specific reference applications were considered and were tested for feasibility on two different benches. Another Laboratory test bench was designed for validation purposes.

The project partners actively participated in conferences and workshops relevant for TAUPE purposes. Such network activities avoid duplication of research activities and raise awareness about technological evolution.

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