Difference between revisions of "Bee-Plane TRL 2"

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<li> Estaca Laval 5A : Cabin Layout for full eco passengers basket<BR>
 
<li> Estaca Laval 5A : Cabin Layout for full eco passengers basket<BR>
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<BR>
 
<li> Estaca Laval 5A : Inboard Energies and engines review<BR>
 
<li> Estaca Laval 5A : Inboard Energies and engines review<BR>
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<BR>
 
<li> Estaca Laval 5A : certification Part 21<BR>
 
<li> Estaca Laval 5A : certification Part 21<BR>
 
[[File:File:Estaca 201402 Certif P21 CS 25.pdf]]<BR>
 
[[File:File:Estaca 201402 Certif P21 CS 25.pdf]]<BR>
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'''Projects in process : plan for march 2014'''<BR>
 
'''Projects in process : plan for march 2014'''<BR>
  
<LI> SupMeca : overall design studies and [[Collaborative projet]]
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<LI> SupMeca : overall design studies and [[Collaborative projet]]<BR>
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<LI> SupMeca : landing gear definition <BR>
 
<LI> SupMeca : landing gear definition <BR>
 
[[File:File:Supmeca TP 2013 Poster.pdf]]<BR>
 
[[File:File:Supmeca TP 2013 Poster.pdf]]<BR>

Revision as of 15:57, 8 February 2014

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

Bee-Plane TRL 1 : 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 for passengers on each side.
  • Basket with APU on the back, 4 electric directional wheels, additional fuel tanks in the basket
  • Bee-Plane Passenger Floor Plan
  • Hospital basket

    Bee
  • Flat surface bellow bee
  • New configuration : No pilot in the bee
  • 2 turbopropeller TP400 bellow main wings, 1 central turbofan on the back.
  • Variable inlet casing for rear turbofan, diameter of the turbofan = 1m.

    Landing Gears and wings
  • Bi-taildragger configuration
  • Opposite "U" shape rear wings
  • Main landing gear with external rotation. Wheels goes behind Turboprop engines.

    Partners

    Partners for TRL2 are :

  • SME (Fr) : Technoplane (Coordination)
  • University (Fr) : Ecole Centrale Paris (aero simulation)
  • University (Fr) : ESTACA (configuration, certification, energy...)
  • University (Fr) : Supméca (configuration, mechanical, logistic)
  • University (Fr) : IFMA (mechanical, airports)
  • University (Ir) : Trinity College (acoustics)
  • University (Fr) : EM Normandie (Partnership)

    Projects & Studies

    Projects finished in june 2013

  • SupMeca : Airport Studies
    File:Rapport Projet Logistique.pdf
    File:Présentation Projet Logistique.pdf


  • EM Normandy : Partnership strategy

    Projects finished in February 2014
  • 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

  • Estaca Laval 5A : Cabin Layout for full eco passengers basket

  • Estaca Laval 5A : Inboard Energies and engines review

  • Estaca Laval 5A : certification Part 21
    File:File:Estaca 201402 Certif P21 CS 25.pdf
    File:Estaca 201402 Certif P21 ppt soutenance.pdf
    File:Estaca 201402 Certif P21 rapport pré-certification Bee-Plane.pdf

  • Estaca Levallois 5A : certification Part 145


    Projects in process : plan for march 2014
  • 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

  • SupMeca : airline economical impact


    Project in process : plan for june 2014
  • Ecole Centrale Paris : AAS Analysis for Aircraft Sizing tool, and implement lateral flight stability calculation

  • IFMA Clermont : Rear landing gear,
  • IFMA Clermont : airport impact,
  • IFMA Clermont : attach system mechanical studies
  • Trinity College : Accoustic