Difference between revisions of "Bee-Plane TRL 2"

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<li> EM Normandy : Partnership strategy
 
<li> EM Normandy : Partnership strategy
 
<li> SupMeca : [[Airport Studies]]<BR>
 
<li> SupMeca : [[Airport Studies]]<BR>
[[File:Supmeca Logistique 2013 Poster Bee-Plane.jpg ]]
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[[File:Supmeca Logistique 2013 Poster Bee-Plane.jpg|300px]]<BR>
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Revision as of 13:42, 19 January 2014

TRL 2 starts in 2013. It is planned to have a 2 years duration.
Projet and tasks are made according to Lesser Open Bee License 1.3

Bee-Plane TRL 1 Year 2012 : Aeronautical configuration to be studied in details is resulting from TRL1.

TRL2 Project Overview

Project description at beginning of TRL2 :



Additional documentation and numerical mock-up
All technical work done according to the open source paragraph of the Lesser Open Bee License 1-3 is available within a dedicated IT server. Access is provide on request.

Guidelines

Basket

  • Basket is design to be optimum for passengers frequent flight, then it is adapted to other usage (fret, hospitals...)
  • Basket with three pressure bubbles, Internal structure adapted to 3-3-3 seats configuration
  • Central luguage area for passenger basket (220 PAX full eco, 200 PAX in 2 classes), Only 1 central large main door on each side.
  • Basket with APU, 4 electric directional wheels, fuel tanks between bubble spaces
    Bee
  • Flat surface bellow bee with ISO standard dimensions (width 2,44m)
  • 1 pilot behind each other, or only 1, or even none.
  • Access between basket/bee is planned to be just before front attach system of the main wing.
  • 2 turbopropeller TP400 on main wings, 1 central turbofan (SAM 146) on the back, or even 2 on the back for military usage(Silvercrest * 2), and 4 propeller on main wing.
  • Variable inlet casing for rear turbofan, behind cockpit and wings, diameter of the turbofan = 1m.
    Landing Gears and wings
  • Bi-taildragger configuration, with lower rear wings that finish with vertical ends for each wheels.
  • Landing gear with external rotation. Wheels goes behind Turboprop engines
  • Upper rear wings that goes out at 45°, from the attach system point.

    Studies

    Studies will includes
    - Configuration definition - Aerodynamic - Mechanical - Accoustic


    Projects already finished (june 2013)

  • EM Normandy : Partnership strategy
  • SupMeca : Airport Studies
    Supmeca Logistique 2013 Poster Bee-Plane.jpg

  • SupMeca : overall design studies and Collaborative projet
  • SupMeca : landing gear definition
    File:File:Supmeca TP 2013 Poster.pdf
    File:Supmeca TP 2013 Rapport Final.pdf
    File:File:Supmeca TP 2013 Soutenance.pdf

  • Estaca Laval 4A : Rear wings
    File:Soutenance de projet Empennage Bee-Plane Tail 2013.pdf
    File:Rapport de projet Bee-Plane 14 01 2014 vFinal Tail 2013.pdf

    Projects started in september 2013
  • Ecole Centrale Paris : AAS Analysis for Aircraft Sizing tool, and implement lateral flight stability calculation.
  • Estaca : Cabin Layout for full eco passengers basket, Structural studies, Inboard Energies, certification
  • Supmeca : Coordination, main landing gear, airlines economical model
  • IFMA Clermont : Rear landing gear, airport, mechanical studies
  • Trinity College : Accoustic

    To be defined
  • INSA Rouen : Continue Engines parametric model (and apply to different future aircraft configuration, including BeePlane)
  • EM Normandy : Partnership strategy