Difference between revisions of "Bee-Plane TRL 2"
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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 3-4-3 seats configuration
Landing gear with external rotation. Wheels goes behind Turboprop engines
Flat surface bellow bee with ISO standard dimensions (width 2,44m)
1 pilot behind each other, or only 1, or even none.
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)
Variable inlet casing for rear turbofan, behind cockpit and wings, diameter of the turbofan = 1m.
Bi-taildragger configuration, with lower rear wings that finish with vertical ends for each wheels.
Central luguage area for passenger basket (200 PAX in 2 classes), Only 1 central main door on each side.
Access between basket/bee is planned to be just before front attach system of the main wing.
Basket with APU, 4 electric wheels, fuel tanks between bubble spaces
EM Normandy : Partnership strategy
SupMeca : Airport Studies
SupMeca : overall design studies and Collaborative projet
SupMeca : landing gear definition
Projects near completion :
None : "summer time"
Projects planned for september 2013 : Ecole Centrale Paris : Continue AAS Analysis for Aircraft Sizing tool, and implement lateral flight stability calculation.
Estaca : Cabin Layout, Structural studies, Inboard Energies, certification
INSA Rouen : Continue Engines parametric model (and apply to different future aircraft configuration, including BeePlane)
IPSA : wings studies
Trinity College : Accoustic
Potential projects within universities and engineering schools
EPFL : Impact on transport system
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<LI>Flat surface bellow bee with ISO standard dimensions (width 2,44m) | <LI>Flat surface bellow bee with ISO standard dimensions (width 2,44m) | ||
<LI>1 pilot behind each other, or only 1, or even none. | <LI>1 pilot behind each other, or only 1, or even none. | ||
− | <LI>2 turbopropeller TP400 on main wings, 1 central turbofan (SAM 146) on the back, or even 2 on the back (Silvercrest * 2) | + | <LI>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) |
<LI>Variable inlet casing for rear turbofan, behind cockpit and wings, diameter of the turbofan = 1m. | <LI>Variable inlet casing for rear turbofan, behind cockpit and wings, diameter of the turbofan = 1m. | ||
<LI>Bi-taildragger configuration, with lower rear wings that finish with vertical ends for each wheels. | <LI>Bi-taildragger configuration, with lower rear wings that finish with vertical ends for each wheels. |
Revision as of 01:24, 21 July 2013
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 : First aeronautical configuration to be studied in details is the one resulting from TRL1.
TRL2 Project Overview
Project description at beginning of TRL2 :
- Project overview : File:20130720 Bee-Plane - Description v3-2.pdf
- Light numerical mock-up : Bee-Plane Google Sketchup
- FP7 Submission file : File:BeePlane PartB Proposal v2.pdf will be presented again in Horizon 2020.
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
Studies
Studies will includes : - Configuration definition - Aerodynamic - Accoustic - Mechanical
Projects already finished:
Projects near completion :
None : "summer time"
Projects planned for september 2013 :
Potential projects within universities and engineering schools