Difference between revisions of "Bee-Plane TRL 2"

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<LI>Basket is design to be optimum for passengers frequent flight, then it is adapted to other usage (fret, hospitals...)
 
<LI>Basket is design to be optimum for passengers frequent flight, then it is adapted to other usage (fret, hospitals...)
 
<LI>Basket with three pressure bubbles, Internal structure adapted to 3-3-3 seats configuration
 
<LI>Basket with three pressure bubbles, Internal structure adapted to 3-3-3 seats configuration
−
<LI>Central luguage area for passenger basket (220 PAX full eco, 200 PAX in 2 classes), Only 1 central large main door on each side.
+
<LI>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.
−
<LI>Basket with APU, 4 electric directional wheels, fuel tanks between bubble spaces
+
<LI>Basket with APU on the back, 4 electric directional wheels, additional fuel tanks in the basket
−
<BR>
+
<BR><BR>
 
'''Bee'''<BR>
 
'''Bee'''<BR>
−
<LI>Flat surface bellow bee with ISO standard dimensions (width 2,44m)
+
<LI>Flat surface bellow bee with ISO standard dimensions (width 2,44m bellow wings)
−
<LI>1 pilot behind each other, or only 1, or even none.
+
<LI>1 pilot behind each other, or only 1 pilot, or even none.
−
<LI>Access between basket/bee is planned to be just before front attach system of the main wing.
+
<LI>Piot can not go from bee to basket (no internal ladder).
−
<LI>2 turbopropeller TP400 on main wings, 1 central turbofan (SAM 146) on the back,
+
<LI>2 turbopropeller TP400 bellow main wings, 1 central turbofan on the back.
−
    or even 2 on the back for military usage(Silvercrest * 2), and 4 propeller on main wing.
+
<LI>Variable inlet casing for rear turbofan, behind cockpit and bellow wings, diameter of the turbofan = 1m.<BR>
−
<LI>Variable inlet casing for rear turbofan, behind cockpit and wings, diameter of the turbofan = 1m.<BR>
 
 
'''Landing Gears and wings'''<BR>
 
'''Landing Gears and wings'''<BR>
−
<LI>Bi-taildragger configuration, with lower rear wings that finish with vertical ends for each wheels.
+
<LI>Bi-taildragger configuration<BR>
−
<LI>Landing gear with external rotation. Wheels goes behind Turboprop engines
+
<LI>Opposite "U" shape rear wings<BR>
−
<LI>Upper rear wings that goes out at 45°, from the attach system point.
+
<LI>Main landing gear with external rotation. Wheels goes behind Turboprop engines.<BR>
  
 
== Studies ==
 
== Studies ==

Revision as of 13:52, 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 :


  • Beeplane TRL2 v1.gif
  • Bee-Plane v12-3 trimoteur - basket séparé AR.jpg
  • Bee-Plane v12-3 trimoteur avec basket.jpg
  • Basket Hopital.jpg
  • En vol.jpg
  • Hangar.png
  • Image1.jpg
  • Image1.png
  • Image2.jpg
  • Image3 logistique.jpg
  • Image3.jpg
  • Vue de face.jpg
  • Beeplane modélisé.jpg


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
  • Flat surface bellow bee with ISO standard dimensions (width 2,44m bellow wings)
  • 1 pilot behind each other, or only 1 pilot, or even none.
  • Piot can not go from bee to basket (no internal ladder).
  • 2 turbopropeller TP400 bellow main wings, 1 central turbofan on the back.
  • Variable inlet casing for rear turbofan, behind cockpit and bellow wings, 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.

    Studies

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


    Projects already finished (june 2013)

  • EM Normandy : Partnership strategy
  • SupMeca : Airport Studies
    File:Rapport Projet Logistique.pdf
    File:Présentation Projet Logistique.pdf
    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
    • Retrieved from "https://wiki.collaborativebee.com//index.php?title=Bee-Plane_TRL_2&oldid=353"