Difference between revisions of "Bee-Plane TRL 2"

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TRL 2 starts in 2013. It is planned to have a 2 years duration.<BR>
 
TRL 2 starts in 2013. It is planned to have a 2 years duration.<BR>
−
Projet and tasks are made according to [http://www.bee-license.com Lesser Open Bee License 1.3]<BR>
+
Projet and tasks are achieved according to [http://www.bee-license.com Lesser Open Bee License 1.3]<BR>
 
<BR>
 
<BR>
 
[[Bee-Plane TRL 1 Year 2012]] : Aeronautical configuration to be studied in details is resulting from TRL1.<BR>
 
[[Bee-Plane TRL 1 Year 2012]] : Aeronautical configuration to be studied in details is resulting from TRL1.<BR>
Line 41: Line 41:
 
<BR><BR>
 
<BR><BR>
 
'''Bee'''<BR>
 
'''Bee'''<BR>
−
<LI>Flat surface bellow bee with ISO standard dimensions (width 2,44m bellow wings)
+
<LI>Flat surface bellow bee
 
<LI>1 pilot behind each other, or only 1 pilot, or even none.
 
<LI>1 pilot behind each other, or only 1 pilot, or even none.
 
<LI>Piot can not go from bee to basket (no internal ladder).
 
<LI>Piot can not go from bee to basket (no internal ladder).
 
<LI>2 turbopropeller TP400 bellow main wings, 1 central turbofan on the back.
 
<LI>2 turbopropeller TP400 bellow main wings, 1 central turbofan on the back.
−
<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, diameter of the turbofan = 1m.<BR>
 
'''Landing Gears and wings'''<BR>
 
'''Landing Gears and wings'''<BR>
 
<LI>Bi-taildragger configuration<BR>
 
<LI>Bi-taildragger configuration<BR>
 
<LI>Opposite "U" shape rear wings<BR>
 
<LI>Opposite "U" shape rear wings<BR>
 
<LI>Main landing gear with external rotation. Wheels goes behind Turboprop engines.<BR>
 
<LI>Main landing gear with external rotation. Wheels goes behind Turboprop engines.<BR>
−
 
+
<BR>
 
== Studies ==
 
== Studies ==
−
Studies will includes<BR>
+
Studies of the TRL2 includes<BR>
 
- Configuration definition
 
- Configuration definition
 
- Aerodynamic
 
- Aerodynamic
 
- Mechanical
 
- Mechanical
−
- Accoustic
+
- Accoustic diagnostic
 +
- Economical studies
 +
- Certification requierements
 
<BR>
 
<BR>
 
<BR>
 
<BR>
 
* [[Bee-Plane Passenger Floor Plan]]
 
* [[Bee-Plane Passenger Floor Plan]]
 
* [[Hospital basket]]<BR>
 
* [[Hospital basket]]<BR>
−
<BR>
+
<BR><BR>
−
'''Projects already finished (june 2013)'''<BR>
+
'''Projects already finished : june 2013'''<BR>
 
<li> EM Normandy : Partnership strategy
 
<li> EM Normandy : Partnership strategy
 
<li> SupMeca : [[Airport Studies]]<BR>
 
<li> SupMeca : [[Airport Studies]]<BR>
Line 69: Line 71:
 
[[File:Supmeca Logistique 2013 Poster Bee-Plane.jpg|300px]]<BR>
 
[[File:Supmeca Logistique 2013 Poster Bee-Plane.jpg|300px]]<BR>
 
<BR>
 
<BR>
 +
'''Projects already finished : February 2014'''<BR>
 +
<LI> Estaca Laval 4A : Rear wings<BR>
 +
[[File:Soutenance de projet Empennage Bee-Plane Tail 2013.pdf]]<BR>
 +
[[File:Rapport de projet Bee-Plane 14 01 2014 vFinal Tail 2013.pdf]]<BR>
 +
<BR>
 +
<li> Estaca Laval 5A : Cabin Layout for full eco passengers basket<BR>
 +
<li> Estaca Laval 5A : Inboard Energies and engines review<BR>
 +
<li> Estaca Laval 5A : certification Part 21<BR>
 +
<li> Estaca Levallois 5A : certification Part 145<BR>
  
  
 +
'''Projects in process : plan for march 2014'''<BR>
  
 
<LI> SupMeca : overall design studies and [[Collaborative projet]]
 
<LI> SupMeca : overall design studies and [[Collaborative projet]]
Line 78: Line 90:
 
[[File:File:Supmeca TP 2013 Soutenance.pdf]]<BR>
 
[[File:File:Supmeca TP 2013 Soutenance.pdf]]<BR>
 
<BR>
 
<BR>
−
<LI> Estaca Laval 4A : Rear wings<BR>
+
<LI> SupMeca : airline economical impact<BR>
−
[[File:Soutenance de projet Empennage Bee-Plane Tail 2013.pdf]]<BR>
+
 
−
[[File:Rapport de projet Bee-Plane 14 01 2014 vFinal Tail 2013.pdf]]<BR>
+
'''Project in process : plan for june 2014 '''
−
<BR>
 
−
'''Projects started in september 2013 '''
 
 
<li> Ecole Centrale Paris : [[AAS Analysis for Aircraft Sizing]] tool, and implement lateral flight stability calculation<BR>
 
<li> Ecole Centrale Paris : [[AAS Analysis for Aircraft Sizing]] tool, and implement lateral flight stability calculation<BR>
−
<li> Estaca : Cabin Layout for full eco passengers basket, Structural studies, Inboard Energies, certification<BR>
+
<li> IFMA Clermont : Rear landing gear,
−
<li> Supmeca : Coordination, main landing gear, airlines economical model<BR>
+
<li> IFMA Clermont : airport impact,  
−
<li> IFMA Clermont : Rear landing gear, airport, mechanical studies<BR>
+
<li> IFMA Clermont : attach system mechanical studies<BR>
−
<li> Trinity College : Accoustic<BR><BR>
+
<li> Trinity College : Accoustic<BR>
 
<BR>
 
<BR>
−
''' To be defined '''
 
−
<li> INSA Rouen : Continue Engines parametric model (and apply to different future aircraft configuration, including BeePlane)<BR>
 
−
<li> EM Normandy : Partnership strategy<BR>
 

Revision as of 12:05, 8 February 2014

TRL 2 starts in 2013. It is planned to have a 2 years duration.
Projet and tasks are achieved 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
  • 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, 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 of the TRL2 includes
    - Configuration definition - Aerodynamic - Mechanical - Accoustic diagnostic - Economical studies - Certification requierements



    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

    Projects already finished : 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
  • 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

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